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Miami International Field Office

2895 SW 145th Avenue Suite 221 Miramar, Florida 33027

July 20, 2017 Via email Mr. Carlos Parra Technical Manager, N.A. Avianca Airlines Certificate No. ANCF 173C Dear Mr. Parra: Please be advised that effective today, July 20, 2017, the documents submitted by Aerovias del Continente Americano S.A. (Avianca) for the A-318/319/320/321, Minimum Equipment List (MEL) Revision 36, dated 06/30/2017, based on the A-318/319/320/321 Master Minimum Equipment List (MMEL) Revision 26a, dated Sep 7, 2016 and Revision 26b, dated Nov 22, 2016, have been reviewed and approved. The pertinent Control Pages have been signed and delivered to your attention. It is the responsibility of Avianca Airlines to ensure their manuals contains safe policies and procedures that are in accordance with the U.S. Code of Federal Regulations (CFR), all applicable ICAO Standards, and other States Aviation Regulations. If you have any questions, please contact this office at (954) 641-6700. Sincerely,

Jose A. Pumares Aviation Safety Inspector Enclosure: 11 Control Pages

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST RECORD OF REVISION |

Upon receipt of revisions, insert revised pages in the manual and enter the revision Number, date, and abbreviated name of the individual responsible of the insertion. Revision Number 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36

Revision: 36 June 30, 2017

Revision Date July 30, 2008 October 01, 2008 October 31, 2008 July 05, 2009 August 18, 2009 December 11, 2009 April 09, 2010 August 09, 2010 November 22, 2010 January 28, 2011 March 01, 2011 March 22, 2011 April 18, 2011 May 19, 2011 July 05, 2011 August 24, 2011 September 23, 2011 October 14, 2011 December 09, 2011 February 17, 2012 April 13, 2012 May 22, 2012 Aug 15, 2012 November 16, 2012 February 8, 2013 April 09, 2013 January 31, 2014 May 20, 2014 July 01, 2014 October 23, 2014 February 26,2015 April 24, 2015 June 30, 2015 September 03, 2015 May 26, 2016 November 24, 2016 June 30, 2017

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Revision: 27 May 20, 2014

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Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST

TEMPORARY REVISION LIST Enter the temporary revision number in numerical order together with the temporary revision date in temporary revision list page. The temporary revision date is inserted followed by the filing person’s initials. When the temporary revision is cancelled and the related pages are removed, the removal date and pages involved must be logged and the responsible person’s initials included. Temporary Revision Number Date TR A32-36-01 Sep 15, 2017 TR A32-36-02 Sep.24,2017 TR A32-36-03 Sep.24,2017

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Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST TEMPORARY REVISION LIST Enter the temporary revision number in numerical order together with the temporary revision date in temporary revision list page. The temporary revision date is inserted followed by the filing person’s initials. When the temporary revision is cancelled and the related pages are removed, the removal date and pages involved must be logged and the responsible person’s initials included. Temporary Revision Number Date


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Revision: 30 February 26, 2015

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Avianca AIRBUS A318/A319/A320/321 MINIMUM EQUIPMENT LIST TABLE OF CONTENTS System No -------------------------21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 38 46 47 49 52 56 71 73 74 75 76 77 78 79 80 -------


System Cover Page Record of Revision Temporary Revision List Table of Contents Log of Revision Control Pages Highlights of Change Introduction Definitions and How to Use this Manual Preamble Manual Control Effectivity MEL Management Air Conditioning Auto Flight Communications Electrical Power Equipment/Furnishings Fire Protection Flight Controls Fuel Hydraulic Power Ice and Rain Protection Indicating/Recording System Landing Gear Lights Navigation Oxygen Pneumatic Water/Waste Information Systems Inert Gas System Airborne Auxiliary Power Doors Windows Power plant Engine Fuel & Control Ignition Bleed Air Engine Control Engine Indicating Engine Exhaust Engine Oil Starting Appendix CAT II/III Appendix PBN (RNAV-RNP) OPERATIONS ECAM WARNINGS / MEL ENTRY

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Page Numbers All pages RR-1, LR-1, CP-1 TO CP-10, HL-1, page 9 October 01, 2008 Effectivity., and 25.42 RR-1, LR-1, CP-1 TO CP-10, HL-1, page 9 October 31, 2008 Effectivity. RR-1, TC-1, LR-1, CP-1 TO CP-10, HL-1 to HL 8, page 1 to 5, 9 (effectivity)., 21.1, 21.4, 21.5, 21.9, 21.15, 21.19, 21.23, 21.28, 21.31, 21.41, 21.42,21.52,21.56, 21.59, 21.60, 21.61, 21.76, 21.80, 22.9, 22.10, 22.11, 22.14, 22.21, 22.22, 22.24, 22.25, 22.26, 22.28, 22.29, 22.30, 23.1, 23.12, 23.22, 23.23, 23.28, 23.36, 25.7, 25.9, 25.11, 25.12, 25.15, 25.23, 25.24, 25.25, 25.26 to 25.50, 26.4, 26.6, 26.8, 26.10, 26.11, 26.37, 27.10, 27.15, July 05, 2009 27.20, 27.43, 27.44, 27.46, 27.47, 27.51, 27.52, 27.53, 27.54, 27.71, 27.72, 28.2, 28.3, 28.4, 28.5, 28.6, 28.7, 28.8, 28.9, 28.10, 28.11 to 28.56, 29.1, 29.26, 30.23, 30.24, 30.25, 30.30, 31.1, 31.5, 31.7, 31.21, 32.1, 32.2, 32.10, 32.11, 32.16, 32.18, 32.54, 32.55, 33.1, 33.2, 33.4,to 33.24, 34.8, 34.46 to 34.48, 35.2, 35.4 to 35.20, 36.1 to 36.26, 52.7, 52.10, 52.11, 52.15, 52.16, 52.17, 52.20, 52.21, 56.1, 56.2, 56.3, 56.4, 71.1, 73.3, 73.15, 75.5, 75.6, 75.7, 75.8, 79.3 to 79.8 RR-1, LR-1, CP-1 to CP-10, HL-1, HL-2, page 9 August 18, 2009 (effectivity) RR-1, LR-1, CP-1 to CP-10, HL-1, HL-2, page 3, December 11, 2009 page 9 (effectivity), 25.46, 35.14, 80.1 RR-1, TC-1, LR-1, CP-1 to CP-10, HL-1, page 9, April 09, 2010 21.20 to 21.84, 25.22, 25.43 and 47.00 RR-1, TC-1, LR-1, HL-1, CP-1 to CP-10, 22.1, 22.2, 22.17, 22.23, 22.28, 22.29, 23.20, 27.47, 27.51, August 09, 2010 27.52, 27.53, 27.54, 31.21, 31.22, 34.3, 34.4, 34.5, 34.34, 34.37, 34.41, 34.47, 34.48, 36.14, 36.24, 52.2, PBN-1 and PBN-2. November 22, 2010 All pages RR-1, LR-1, CP-1 to CP-12, HL-1, HL-2, Page 9, January 28, 2011 47.1. RR-1, LR-1, CP-1 to CP-12, HL-1, HL-2, Page 3, 4, 5, 9 (effectivity), 21.1, 21.38, 21.39, 21.40, 21.41, 21.42, 21.43, 21.58, 22.16, 22.30, 23.3, 23.10, March 01, 2011 23.15, 23.20, 24.14, 24.15, 25.45. 25.47, 33.3, 33.18, 34.7, 34.22, 34.23, 34.25, 34.30, 34.41, 36.1, 36.2, 36.14, 36.23 and 36.24. RR-1, LR-1, CP-1 to CP-12, HL-1, HL-2, Page 32.35 March 22, 2011 and 32.36

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Page Numbers RR-1, LR-1, LR-2, CP-1 to CP-12, HL-1 and Page 9 April 18, 2011 (Effectivity). RR-1, TC-1, LR-2, CP-1 to CP-12, HL-1 to HL-4, Page 4, 21.1, 21.38, 21.39, 21.40, 21.41, 21.42, 21.43, 21.59, 21.62, 21.63 to 21.68, 21.76, 21.78, 21.79, 21.80, 21.81, 21.84, 22.16, 22.30, 23.3, 23.10, 23.28, 23.29, 23.31, 23.32, 23.33, 23.34, May 19, 2011 23.36 to 23.42, 24.14, 25.15, 25.36, 26.1, 26.13, 27.14, 28.6, 29.4, 29.5, 31.1, 32.18, 32.24, 32.35, 32.36, 32.48, 32.59, 33.3, 33.4, 33.18, 34.7, 34.9, 34.22, 34.23, 34.25, 34.28, 34.30, 34.41, 36.1, 36.2, 36.3, 34.14, 36.23 and 36.24. RR-1, LR-2, CP-1 to CP-12, HL-1 to HL-4, Page 9, 21.1, 21.38, 21.39, 21.40, 21.41, 21.42, 21.43, 21.59, 21.62, 21.63, 21.64, 21.66, 21.67, 21.76, 21.78, 21.79, 21.81, 21.84, 22.16, 22.30, 23.3, 23.5, 23.10, 23.28, 23.29, 23.31, 23.32, 23.33, 23.34, July 05, 2011 23.36, 23.38, 24.14, 25.12, 25.36, 26.1, 26.13, 27.14, 28.6, 29.4, 31.1, 32.18, 32.24, 32.35, 32.36, 32.48, 32.59, 33.3, 33.18, 34.7, 34.9, 34.22, 34.23, 34.25, 34.28, 34.30, 34.41, 35.15, 36.1, 36.2, 36.3, 34.14, 36.23, 36.24, 46.2 and 47.1. RR-1, LR-2, CP-1 to CP-12, HL-1 to HL-4, Page 9, 21.1, 21.38, 21.39, 21.40, 21.41, 21.42, 21.43, 21.59, 21.62, 21.63, 21.64, 21.66, 21.76, 21.78, 21.79, 21.81, 21.84, 22.16, 22.30, 23.3, 23.10, 23.15, 23.28, 23.29, 23.31, 23.32, 23.34, 23.36, August 24, 2011 23.38, 24.14, 25.36, 25.50, 26.1, 26.13, 27.14, 28.6, 29.4, 31.5, 31.6, 32.24, 32.48, 32.59, 33.3, 33.18, 34.7, 34.9, 34.22, 34.23, 34.25, 34.28, 34.30, 34.41, 36.1, 36.2, 36.3, 34.14, 36.23, 36.24, 47.1 and 52.18. RR-1, LR-2, CP-1 to CP-12, HL-1 to HL-2 and page September 23, 2011 34.46 RR-1, TC-1, LR-2, CP-1 to CP-12, HL-1, HL-2, page October 14, 2011 9, 21.38, 21.39, 21.40, 23.3, 24.4 to 24.30, 27.22, 27.23, 27.24, 34.41, 34.46 and PBN-2. RR-1, LR-2, CP-1 to CP-12, HL-1, HL-2, page 21.46, 21.74, 22.17, 22.26, 25.39, 25.47, 25.48, 26.8, 27.31, 27.34, 27.46, 27.65 to 27.70, 28.45, 28.50, December 09, 2011 31.2, 31.21, 31.23, 32.6, 32.9, 32.13, 34.4, 34.48, 35.5, 36.2, 36.24, 49.6, 52.1, 52.5, 52.12, 80.5, ECAM-3, ECAM-4 and ECAM 17.

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Page Numbers RR-1, TC-1, LR-2, LR-3, LR-4, CP-1 to CP-12, HL-1, February 17, 2012 HL-2, page 9, 21.38, 21.39, 21.40, 21.58, 23.3, 24.2, 24.3, 24.4, 24.5, 25.12, 32.58, 34.41 and 34.46 RR-1, LR-3, CP-1 to CP-12, HL-1, HL-2, page 9, April 13, 2012 21.38, 21.39, 21.40, 23.3, 23.28, 25.12, 34.41, 34.46 and 47.1 RR-1, LR-3, CP-1 to CP-12, HL-1, HL-2, page 9, May 22, 2012 26.41 and CAT-2. RR-1, TC-1, LR-3, CP-1 to CP-12, HL-1 thru HL-6, page 1 thru 5, 9, 21.1, 21.2, 21.4 thru 21.66, 22.16 thru 22.30, 23.23 thru 23.28, 23.42 thru 23.44, 24.2 thru 24.7, 24.29, 24.30, 25.17 thru 25.19, 25.21, 25.25, 25.26, 25.40, 25.44, 25.51 thru 25.54, 26.10 thru 26.40, 27.31 thru 27.36, 27.43 thru 27.72, 28.6, 28.25 thru 28.54, 30.2, 30.3, 30.11 thru 30.12, 30.29, Aug 15, 2012 31.5, 31.13, 31.15, 31.21 thru 31.28, 32.7, 32.11 thru 32.14, 32.16 thru 32.18, 32.35 thru 32.58, 33.1 thru 33.4, 33.9, 33.18, 33.24 thru 33.26, 34.3 thru 34.8, 34.29 thru 34.52, 35.5, 35.14, 35.19 thru 35.22, 36.1, 36.2, 36.16 thru 36.26, 52.7, 52.10, 52.11, 52.18, 52.20, 71.1, 71.2, 73.3, 73.8, 74.2, 76.1, 76.2, 79.4 and PBN-2. RR-1, TC-1, LR-3, CP-1 to CP-10, HL-1, HL-2, Page 9, 21.1, 21.26, 21.27, 21.28, 22.11 thru 22.28, 23.3, November 16, 2012 23.25, 24.2 thru 24.5, 25.1, 28.25, 31.1, 31.21 thru 31.25, 34.32, 34.44, 34.49, 34.52, 35.22 and 47.1. RR-1, TC-1, LR-3, CP-1 to CP-10, HL-1, HL-2, Page 9, 21.11, 23.3, 23.25, 24.5, 27.30 thru 27.76, 28.25, February 8, 2013 30.2 thru 30.4, 30.10, 30.12, 30.12.1, 30.12.2, 32.11, 32.14, 32.15, 32.19, 34.44, 34.49, 35.22, 47.1, 74.1 and CAT-2. RR-1, LR-3, CP-1 to CP-10, HL-1, HL-2, Page 9, April 09, 2013 21.26, 21.27, 21.28, 23.3, 23.25, 28.2, 28.25, 34.6, 34.44, 34.49, 35.22 and 47.1. RR-1, LR-3, CP-1 to CP-10, HL-1, HL-2, Page 9, 21.1, 21.26 thru 21.31, 21.43, 21.46 thru 21.48, 21.50, 21.57, 21.59, 21.62, 21.65, 22.27, 23.3, 23.10, 23.25, 23.27, 23.29, 23.31, 23.32, 23.34, 23.36, 23.38, 24.2 thru 24.5, 24.15, 25.12, 25.15, 25.36, 25.39, 25.12, 25.15, 25.36, 25.39, 26.1, 26.14, 26.40, 27.14, 27.36, 27.37, 27.38, 27.48, January 31, 2014 27.49, 28.7, 28.25, 30.2 thru 30.30, 31.1, 31.5, 31.23, 31.24, 32.13 thru 32.15, 32.24, 32.36, 32.37, 32.46, 32.56, 32.57, 33.1, 33.2, 33.4, 33.18, 33.25, 34.6 thru 34.9, 34.22, 34.23, 34.25, 34.28, 34.31, 34.32, 34.44, 34.49, 35.19, 35.20, 35.22, 36.1, 36.3, 36.14, 36.22, 36.23, 47.1, 73.8 thru 73.13, 74.1 thru 74.4, 78.3 thru 78.16, 79.1, 79.4, 79.7 and 80.1. May 20, 2014 All Pages

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Page Numbers Initials RR-1, TC-1, LR-4, CP-1 to CP-12, HL-1, Page 6, 7, July 01,2014 23.3, 23.25, 23.38, 23.39, 27.31, 27.66, 27.67, J.C.C.B 28.28, 30.3, 30.9, 30.10, 30.11, 34.49, 47.1 RR-1,TC-1, LR-4, CP-1 to CP-10, HL-1 to HL-6, Page 1 to 12, 21.20, 21.44, 21.47 thru 21.66, 22.27, 23.3, 23.6, 23.5, 23.20, 23.27 thru 23.46, 24.2, 24.3, 24.6, 24.15, 24.16, 24.23 thru 24.28, 25.1 thru 25.9, 25.14, 25.15, 25.18 thru 25.56, 26.5, 26.10, 26.11, 26.31, 26.32, 27.2 thru 27.70, 28.2 thru 28.52, 29.7 thru 29.20, 30.22, 30.23, 30.25, 31.1, 31.7, 31.11, October 23, 2014 J.C.C.B 31.14, 31.21, 31.22, 31.23, 32.3 thru 32.60, 33.1, 33.2, 33.9, 33.16, 33.17, 33.18, 33.23, 34.3 thru 34.54, 35.17, 36.5, 36.6 thru 36.22, 47.1, 47.2, 49.3 thru 49.10, 52.2, 52.7, 52.10, 52.14 thru 52.22, 71.1, 71.2, 73.9, 74.3, 75.1 thru 75.8, 77.1, CAT-2, CAT-3, ECAM-22, ECAM-23, ECAM-24, ECAM-25 and ECAM-26 RR-1, TRL-1, TRL-2, TC-1, LR-4, CP-1 to CP-10, HL-1 to HL-4-, Page 1 to 16, 23.3, 23.7, 23.12, 23.27, 23.28, 24.5, 25.14 thru 25.52, 26,40, 27.19, February 26, 2015 J.C.C.B 28.6, 28.8, 28.11, 28.34, 28.35, 28.36, 28.37, 32.24, 32,34 33.16, 33.18, 34.44, 35.15, 47.2, PBN-2, PBN4, PBN-6, PBN-7 and ECAM-21 RR-1, TRL-1, TC-1, LR-4, CP-1 thru CP-10, HL-1, HL-2, Page 21.49, 21.50, 23.3, 23.25, 23.27, 23.40, April 24, 2015 24.2, 27.2, 27.15, 27.25, 27.61, 27.62, 28.21, 31.21, J.C.C.B 31.22, 32.34, 32.35, 32.36, 33.5, 33.18, 33.20, 34.46, 34.51, 35.14, 35.22, 52.15, 52.22 and 71.1 RR-1, LR-4, CP-1 thru CP-10, HL-1, Page 9, 22.27, June 30, 2015 25.14, 25.15, 25.16, 25.48, 27.25, 27.26, 27.61, J.C.C.B 27.62, 31.1, 31.7, 31.11, 33.18, 33.24 and 34.46 RR-1, TRL-1, LR-4, CP-1 thru CP-10, HL-1, HL-2, 23.3, 23.25, 23.27, 24.2, 24.3, 27.25, 27.61, 27.62, September 03, 2015 28.21, 30.2, 30.3, 30.4, 30.7 30.8, 30.9, 30.10, J.C.C.B 31.21, 31.22, 32.9, 32.11, 32.12, 32.13, 34.51, 36.19, 36.20, 73.8 and 73.9 RR-1, TRL-1, TC-1, LR-4, LR-5, LR-6, CP-1 thru CP-12, HL-1 thru HL-8, Page 6, 8, 9, 15, 21.1, 21.26 thru 21.32, 21.42, 21.43, 21.46, 21.47, 21.48, 21.51, 21.52, 21.57, 21.59 thru 21.64, 22.7 thru 22.30, 23.3, 23.5, 23.10, 23.12, 23.25, 23.27, 23.29, 23.31 thru 23.44, 24.2, 24.3, 24.5, 24.7, 24.15, 24.26, 25.12, 25.14, 25.15, 25.18, 25.33, 25.36, 25.37, 25.41, May 26,2016 J.C.C.B 25.44, 25.45, 25.47, 25.51, 25.52, 26.1, 26.14, 26.40, 27.12, 27.25, 27.60, 27.61, 27.62, 28.3, 28.7, 28.21, 28.33, 28.39 thru 28.52, 29.4, 30.1, 30.7, 30.12, 30.13 thru 30.32, 31.1, 31.5, 31.21, 31.22, 31.23, 31.24, 32.5, 32.9, 32.21, 32.34, 32.35, 32.36, 32,45, 32.57, 32.58, 33.1, 33.2, 33.4, 33.8, 33.13, 33.17, 33.25, 34.1, 34.6, 34.9, 34.10, 34.16, (Continued) N Registration

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Page Numbers 34.23, 34.24, 34.26, 34.27, 34.29, 34.32, 34.34, 34.43, 34.46, 34.51, 35.5, 35.19 thru 35.22, 36.1 thru 36.26, 52.7, 52.15, 71.1, 71.3, 73.4, 73.8, 73.16 thru 73.24, 75.4 thru 75.10, 77.1, 78.1 thru 78.18, 79.3, 79.8 thru 79.12, 80.1, 80.4, CAT-2, CAT-3, PBN-2 thru PBN-8 RR-1, TRL-1, TC-1, LR-5, CP-1 thru CP-12, HL-1, HL-2, Page 23.3, 23.25, 23.27, 24.2, 27.19, 27.25, 27.61, 27.62, 28.5, 28.8 thru 28.54, 31.21, 31.22, November 24, 2016 32.5, 34.51, 35.21, 35.22, 36.1, 73.3, 73.16, 73.18, 73.20, 73.21, 73.22, 73.24, 73.25, 73.26, 74.1, 75.1, 78.1, 78.3, 78.4, 79.6, 79.8, 79.9, 79.10 and 79.11. RR-1, TRL-1, TC-1, LR-5, CP-1 thru CP-12, HL-1 thru HL-6, Pages 1, 4, 5, 7, 9, 13, 21.1, 21.5, 21.6, 21.8, 21.9 21.12, 21.19, 21.26, 21.27, 21.28, 21.29, 21.30, 21.31, 21.42, 21.46, 22.2, 22.7, 22.8, 22.10 thru 22.32, 23.2, 23.3, 23.6, 23.8, 23.10, 23.15, 23.16, 23.25, 23.27, 23.33, 23.34, 23.35, 23.37, 24.2, 24.7, 24.15, 24.16, 25.11, 25.12, 25.13, 25.14, 25.15, 25.35, 25.36, 25.44, 25.51, 25.52, 26.40, June 30, 2017 27.19 thru 27.72, 28.8, 28.22, 28.34, 28.37 thru 28.54, 29.4, 30.1, 30.3, 30.36, 31.1, 31.9, 31.21, 31.22, 32.5 thru 32.68, 33.1, 33.2, 33.4, 34.3, 34.4, 34.5, 34.9, 34.10, 34.23, 34.24, 34.26, 34.29, 34.33, 34.34, 34.46, 35.5 thru 35.24, 36.1 thru 36.36, 49.2, 49.3, 49.4, 71.1, 71.3, 73.8, 73.9, 73.16, 73.19, 73.20, 73.21, 73.22, 73.24, 73.26, 74.1 thru 74.6, 75.1, 77.1, 78.1, 78.3 thru 78.24, 79.8, 79.9, 79.10, 79.11, 79.12, ECAM-3 thru ECAM-24

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Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST HIGHLIGHTS OF CHANGE Airbus A318/A319/A320/A321 MEL Rev. 36 is based on FAA MMEL Revision 26b date November 22, 2016. This Revision were made to include four new aircrafts Airbus: 1. A321-253N 2. A321-253N 3. A320-251N 4. A320-251N

N759AV N761AV N764AV N765AV

and following changes as listed: ITEM Cover Page Record of Revision Temporary Revision Table of Contents Log of Revision Control Page Highlights of Change Introduction Definitions and How to Use this Manual Manual Control ATA 21 AIR CONDITIONING 21-00 21-26-01 21-26-02 21-26-05 21-26-10 21-28-01 21-28-02 21-28-03 21-28-04 21-28-05 21-28-06 21-43-02 21-51-06 ATA 22 AUTO FLIGHT 22-10-02 22-10-07 22-10-08 22-30-02 22-66-01 22-81-03 22-83-01 22-83-02 Pages 22,10 to 22,32 Revision: 36 June 30, 2017

MEL CHANGE Changed the effectivity manual. The Revision change to revision 36. Deleted the reference of temporary revision list. Updated according to revision 36. Updated to revision 36. Updated to revision 36 according with Highlights of Change. States the changes that includes the revision 36. The introduction was updated. The Definitions and How to Use this Manual was updated. The Manual Control was updated.

Deleted retired airplane N266CT Revised Op. Procedure Revised Op. Procedure Revised Op. Procedure Revised Op. Procedure Added new neo airplanes Added new neo airplanes Added new neo airplanes Deleted retired airplane N266CT Deleted retired airplane N266CT Deleted retired airplane N266CT Deleted retired airplane N266CT Revised Op. Procedure Revised Op. Procedure Pagination Change Added new neo airplanes Revised Op. Procedure Revised Op. Procedure Revised Op. Procedure Revised Op. Procedure Added new neo airplanes Pagination Change

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Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST HIGHLIGHTS OF CHANGE ITEM MEL CHANGE ATA 23 COMMUNICATIONS 23-10-01 Applicability revised 23-11-01 Added new neo airplanes 23-13-01 Applicability revised 23-28-01 Added new neo airplanes 23-31-02 Applicability revised 23-43-04 Applicability revised 23-44-01 Revised Op. Procedure 23-71-01 Added new neo airplanes 23-72-01 Added new neo airplanes 23-73-03 Added new neo airplanes 23-73-04 Added new neo airplanes 23-72-05 Added new neo airplanes 23-73-07 Added new neo airplanes ATA 24 ELECTRICAL POWER 24-20-01 Added new neo airplanes 24-20-07 Added new neo airplanes 24-30-01 Deleted retired airplane N266CT ATA 25 EQUIPMENT/FURNISHINGS 25-21-01 Added new neo airplanes 25-22-01 Added new neo airplanes 25-60-07 Added new neo airplanes 25-60-08 Added new neo airplanes 25-60-16 Added new neo airplanes 25-90-01 Added new neo airplanes ATA 26 FIRE PROTECTION 26-26-24 Deleted retired airplane N266CT ATA 27 FLIGHT CONTROLS 27-51-01 Added relief for neo airplanes. Op Proc updated 27-64-01 Added new neo airplanes and revised op procedures 27-92-02 Added new neo airplanes and revised op procedures 27-94-01 Added new neo airplanes and revised op procedures Pages 27,20 to 27,72 Pagination Change ATA 28 FUEL 28-21-02 Revised applicability 28-25-06 Added new airplanes N759AV, N761AV,N764AV and N765AV Added new airplanes N759AV, N761AV,N764AV and N765AV 28-40-02 28-40-05 Revised applicability 28-40-06 Revised applicability 28-40-07 Revised applicability Pages 28,38 to 28,54 Pagination Change ATA 29 HYDRAULIC POWER 29-10-03 Revised applicability for neo Airplanes ATA 30 ICE AND RAIN PROTECTION Added new airplanes N759AV, N761AV,N764AV and N765AV 30-00 Revision: 36 June 30, 2017

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Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST HIGHLIGHTS OF CHANGE ITEM MEL CHANGE 30-11-01 Revised to add neo airplanes and operational procedures 30-21-01 Revised to add neo airplanes and operational procedures 30-21-03 Revised to add neo airplanes and operational procedures Pages 30,6 to 30,36 Pagination Change ATA 31 INDICATING/RECORDING SYSTEM 31-00 ITEM (8) added A320 neo and A321 neo 31-30-05 Revised applicability Added new airplanes N759AV, N761AV,N764AV and N765AV 31-63-01 (Item 4 a) ATA 32 LANDING GEAR 32-31-01 Added provisos for neo airplanes 32-42-01 Updated for neo airplanes 32-44-02 Updated Operational Procedure 32-47-01 Revised applicability 32-48-01 Deleted N266CT and added N764AV and N765AV 32-48-02 Deleted N266CT and added N764AV and N765AV 32-48-03 Deleted N266CT and added N764AV and N765AV 32-51-03 Updated Op Procedure Pagination Change Pages 32,8 to 32,68 ATA 33 LIGHTS 33-10-01 Deleted item ( 2 ), applicable to N266CT only 33-20-01 Deleted N266CT in Item 1 and Item 2 ATA 34 NAVIGATION 34-10-01 Deleted N266CT from applicable Items 34-10-02 Deleted N266CT from applicable Items 34-10-03 Deleted N266CT from applicable Items 34-21-01 Deleted N266CT from applicable Item 34-21-02 Deleted N266CT from applicable Item 34-22-01 Deleted N266CT from applicable Item 34-22-03 Deleted N266CT from applicable Item 34-40-09 Revised to update applicability 34-41-01 Deleted N266CT from applicable Item 34-53-01 Deleted N266CT from applicable Item ATA 35 OXYGEN 35-13-01 Updated for neo airplanes and operational procedures revised 35-23-04 Deleted N266CT from applicable Item 35-23-05 Deleted N266CT from applicable Item 35-31-01 Updated for neo airplanes ( A320-251N only ) 35-32-01 Updated for neo airplanes Pages 35,6 to 35,24 Pagination Change ATA 36 PNEUMATIC 36-00 Deleted N266CT from applicable Item. 36-11-01 Updated for neo airplanes and operational procedures revised 36-11-02 Operational procedures revised 36-11-03 Updated for neo airplanes and operational procedures revised Revision: 36 June 30, 2017

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Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST HIGHLIGHTS OF CHANGE ITEM 36-11-08

MEL CHANGE Deleted N266CT from applicable Item and neo airplanes added Deleted N266CT from applicable Item and Neo airplanes item 36-22-15 revised 36-22-17 Updated for neo airplanes and operational procedures revised Pages 36,8 to 36,36 Pagination Change ATA 49 AIRBORNE AUXILIARY POWER Updated in accordance TR A32-36-03 and updated the operational 49-10-01 procedures 49-10-02 Updated in accordance TR A32-36-01 49-30-01 Updated in accordance TR A32-36-04 ATA 71 POWER PLANT 71-00 Deleted N266CT from applicable Item 71-10-01 Operational procedures revised ATA 73 ENGINE FUEL & CONTROL 73-20-03 New neo airplanes added in Op Procedure 73-20-11 Updated for new neo airplanes 73-30-04 Added placard instruction 73-30-05 Updated for new neo airplanes 73-30-06 Updated for new neo airplanes 73-30-07 Updated for new neo airplanes 73-30-09 Updated for new neo airplanes 73-30-10 Updated for new neo airplanes 73-30-11 Updated for new neo airplanes ATA 74 IGNITION 74-31-01 Revised op proc for LEAP-1A engines 74-31-02 Updated Op Procedure Pages 74,3 to 74,6 Pagination Change ATA 75 BLEED AIR 75-21-01 Updated for new neo airplanes ATA 77 ENGINE INDICATING 77-00-01 Updated for new neo airplanes ATA 78 ENGINE EXHAUST 78-11-09 Updated for new neo airplanes 78-30-01 Updated for neo airplanes and operational procedures revised 78-31-01 Updated for neo airplanes and operational procedures revised 78-31-02 Updated for new neo airplanes Pages 78,8 to 78,24 Pagination Change ATA 79 ENGINE OIL 79-35-02 Updated for new neo airplanes 79-35-03 Updated for new neo airplanes 79-35-04 Updated for new neo airplanes 79-35-05 Updated for new neo airplanes Pages 79,10 to 79,12 Pagination Change


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Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST HIGHLIGHTS OF CHANGE ITEM APPENDIX ECAM WARNINGS Pages ECAM-3 to ECAM-24


MEL CHANGE Revised applicability and format

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Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST HIGHLIGHTS OF CHANGE



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Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST INTRODUCTION This Minimum Equipment List Manual has been prepared in accordance with the FAA MMEL and reflects the items applicable to Airbus A318/A319/A320/A321 Avianca’s Fleet only to facilitate the MEL consult and deferring process and renumbering individual items within an ATA category to provide proper continuity. This manual explains the policies, techniques and procedures applicable to the Airline. The Airline operates within the approved Limitations, Operations Specifications, Regulations or any other Requirement that the FAA and UAEAC deems convenient. Every aircraft listed in the Limitations and Operations Specifications will be operated according to the specifications and/or requirements described in Airworthiness Certificate, Flight Manual and its Type Certificate and the MEL. The Airline will permit that the inspectors of the Aeronautical Authority audit the inspection system, records and general capacity at any time, as required. If the Aeronautical Authority requests it, the Airline will produce in a timely manner all the documents and requirements requested. It is the responsibility of the Engineering Director to ensure that all the information contained in this manual is correct and up to date. The responsible party for the quality in the distribution process and availability of volumes of the Minimum Equipment List Manuals is the Technical Publication Department Chief and boarding process on Airbus A318/A319/A320/A321 fleet is responsibility of CAD (Centro Administrativo Documentos), monitored by the Corporate Quality Assurance according to the procedures established in this manual. The procedures and instructions in this manual are based in the latest technical information. These have been established in order to plan and carry out commercial flights according to the policies of the Company. The Airline guarantees that all assigned personnel or the one who has a direct participation in the ground and flight operations, is properly instructed, has demonstrated their capacity in the company policies and procedures, in order to maintain the highest degree of safety. MEL Temporary Revisions Policy To expedite a revision requiring immediate implementation due to Aeronautical Authority (Airworthiness Directive or regulations), operational variations, policy changes or other related requirements, a temporary revision will be issued. The temporary revision shall be issued on yellow paper and recorded on a temporary revision list (refer to Temporary Revision List page to procedure details). All temporary revisions issued shall be included in the next MEL revision. All temporary revisions will be approved by the Avianca Quality Director and issued as a supplement to the approved MEL and the TR copy will send to UAEAC via e-mail. The temporary Airbus A318/A319/A320/A321 MEL revisions will be published by the Technical Publication Department to all manual holders. The temporary MEL revision will only be issued in the following cases: 1. Aircraft configuration mistakes. 2. Typographical error. 3. More restrictive requirement or changes from Manufacturer or Aeronautical Authority (Airworthiness Directive or regulations) related to (O) or (M) procedures. 4. SB incorporations that affects the MEL applicability. TR Consecutive TR A32Affected fleet: A32: Airbus A32S A33: Airbus A330 AT7: ATR 72 B78: Boeing 787 Revision: 36 June 30, 2017

-00-

-01

Current MEL revision number where the temporal revision is issued

Incremental Number

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Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST INTRODUCTION MEL Temporary Revision Layout (MEL-TR-001 Form Rev. 0)


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Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST INTRODUCTION


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Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST DEFINITIONS AND HOW TO USE THIS MANUAL 2. Administrative Control Item (ACI). An ACI is listed by the aircraft operator in the MEL for tracking and informational purposes. As an example, ACI may be used to track ETOPS accomplishment of required APU cold-soak, or in-flight verification starts. An ACI may be added to an aircraft operator’s MEL by approval of the POI provided no relief is granted, or provided conditions and limitations are contained in an approved document (e.g., Structural Repair Manual (SRM) or Airworthiness Directive (AD)). If relief other than that granted by an approved document is sought for an ACI, a request must be submitted to the Administrator. If the request results in review and approval by the FOEB, the item becomes an MMEL item rather than an ACI. Note: Avianca A318/A319/A320/A321 MEL manual is approval by the FAR and UAEAC although it does not cover the ECAM WARNING Appendix that is located at the end of the MEL manual; it is controlled by Avianca on the same control page and table of contents of Avianca A318/A319/A320/A321 MEL manual. ECAM WARNING appendix is a guide given by Airbus as a complement of the MEL, and it is used when fault message are showing on the ECAM display, it helps the technical personnel when are looking for an equivalent MEL item for an specific ECAM fault message. 3. ATA System Page. The ATA system page is divided into four (4) columns and contains: item and repair category; number installed; number required for dispatch; and remarks or exceptions. Standard ATA categories are used. Items are numbered sequentially. (Example) 3.1 ITEM

SUBJECT

22-10-01 Autopilot Systems

3.2 CAT

3.3 No INS

3.4 MIN REQ

B

2

0

3.5 REMARKS OR EXCEPTIONS

May be inoperative provided: 3.6 a) Approach minimums do not require their use, b) Enroute operations do not require their use, and c) Number of flight segments and segment duration is acceptable to flight crew. 3.7 NOTE 1: Any mode which operates normally may be used.

3.1. Item. This column depicts the equipment, system, component, or function listed in the “Item” column. 3.2. Repair Category. See definition #23. 3.3. Number Installed. This column depicts the number (quantity) of instrument and equipment items normally installed in the aircraft. This number represents the aircraft configuration considered in developing this MMEL. Should the number be a variable (e.g., fleet configuration differences, cockpit lighting items, cabin lighting items, cargo restraint components) a number is not required and the “-” symbol is used. 3.4. Number Required for Dispatch. This column depicts the minimum number (quantity) of instrument and equipment items required for operation provided the conditions specified in the “Remarks or Exceptions” column are met.


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3.8

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST DEFINITIONS AND HOW TO USE THIS MANUAL 3.5 Remarks or Exceptions. This column may include a statement(s) either prohibiting or permitting operation with a specific number of instrument and equipment items inoperative, provisos (conditions and limitations) for such operation, and appropriate notes. 3.6 Provisos. Provisos are indicated by a number or a lower case letter in “Remarks or Exceptions”. Provisos are conditions or limitations that must be complied with for operation with the listed instrument or equipment item inoperative. 3.7 Notes. Notes provide additional information for crewmember or maintenance consideration. Notes are used to identify applicable material, which is intended to assist with compliance, but do not relieve the aircraft operator of the responsibility for compliance with all applicable requirements. Additional notes may be amended, deleted, or added to the MEL by the aircraft operator, as appropriate. Notes are not a part of the provisos. 3.8 Vertical Bar (change bar). A vertical bar (change bar) in the margin indicates a change, addition or deletion in the adjacent text for the current revision of that page only. The change bar is dropped at the next revision of that page. This bar will not appear in the following revision at the same location as the bar only denotes changes done in the current revision of the manual not the previous ones. In addition, for the digital version of the manual these changes are also visualized in dark blue letter case for easy identification of the modified text. 4. Airplane Flight Manual (AFM). The FAA-approved AFM is the document approved by the responsible FAA Aircraft Certification Office (ACO) during type certification. The approved flight manual for the specific aircraft is listed on the applicable Type Certificate Data Sheet (TCDS). The approved flight manual is the source document for operational limitations and performance parameters for an aircraft. 5. Code of Federal Regulations (CFR) and Federal Aviation Regulations (FAR). CFR, the current term, and FAR both refer to the applicable portions of the Federal Aviation Act and Code of Federal Regulations. 5.1 “Reglamento Aeronáutico Colombiano” (RAC). Means the applicable portions of the Unidad Administrativa Especial de la Aeronáutica Civil (Autoridad Aeronáutica Colombiana) 6. Considered Inoperative. The phrase, “Considered Inoperative”, as used in the provisos, means that an instrument and equipment item must be treated for dispatch, taxi and flight purposes as though it were inoperative. The item will not be used or operated until the original deferred item is repaired. Additional actions include: documenting the item on the dispatch release (if applicable), placarding, and complying with all remarks, exceptions, and related MEL provisions, including any (M) and (O) procedures and observing the repair category. 7. Continuing Authorization – Single Extension. An aircraft operator who has the authorization to use an FAA-approved MEL may also have the authority to use a continuing authorization to approve a single (one-time) extension to the repair interval for category B or C items in accordance with Operations Specification D095. Continuing Authorization – Single Extension is not authorized for repair category A and D items. 8. Dash (-). Indicates a variable number (quantity) of the instrument and equipment items may be installed or required for dispatch. This is common when a fleet MEL is used since aircraft of the


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Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST DEFINITIONS AND HOW TO USE THIS MANUAL same make and model may have differing numbers of specific instrument and/or equipment items installed. 9. Day of Discovery. This is the calendar-day an equipment/instrument malfunction was recorded in the aircraft maintenance record/logbook. This day is excluded from the calendar-days or flightdays specified in the MEL for the repair interval of an inoperative instrument and/or equipment item. This provision is applicable to all MEL items; i.e., categories A, B, C, and D. 10. Deactivated and/or Secured. When the MEL refers to an instrument and/or equipment item as deactivated and/or secured, the specified component must be put into an acceptable condition for safe flight as specified on each item. 11. Deleted. "Deleted” in the remarks column after a sequence item indicates that the item was previously listed but is now required to be operative if installed in the aircraft. 12. Extended Range Operations (ER). ER refers to extended range operations (ETOPS) of an airplane with operational approval to conduct ETOPS in accordance with the applicable regulations. 13. Excess Items. Excess items are those instrument and equipment items that have been installed that are redundant to the requirements of the 14 CFR. 14. Flight Day. A flight-day is a 24-hour period based on Local Time (Bogotá, Colombia Time), during which at least one flight is initiated for the affected aircraft. 15. Heavy Maintenance Visit (HMV). HMV is a scheduled C-check/D-check or airworthiness maintenance program inspection where the aircraft is scheduled to be out of service for 4 or more days. 16. Icing Conditions. An atmospheric environment that may cause ice to form on the aircraft (structural) or in the engine(s) (induction). 17. Inoperative. A system and/or component malfunction to the extent that it does not accomplish its intended purpose and/or is not consistently functioning normally within its approved operating limit(s) and/or tolerance(s). 18. Inoperative Components of an Inoperative System. Inoperative instrument and equipment items, which are components of a system that is inoperative, are usually considered components directly associated with and having no other function than to support that system (warning/caution systems associated with the inoperative system must be operative unless relief is specifically authorized per the MEL). 19. Is Not Used. The phrase “Is Not Used” in the provisos, remarks or exceptions for an MEL instrument or equipment item may specify that another item in the MEL “is not used”. In such cases, crewmembers must not activate, actuate, or otherwise utilize that item under normal operations. It is not necessary for aircraft operators to accomplish the (M) procedure(s) associated with the item. However, operational requirements must be complied with, and an additional placard must be affixed, to the extent practical, adjacent to the control or indicator for the item that is not used. This informs crewmembers that an instrument or equipment item is not to be used under normal operations. 20. Nonessential Equipment and Furnishings (NEF). NEFs are those items installed on the aircraft as part of the original type certification, STC, or other form of alteration that have no effect on the safe operation of flight and would not be required by the applicable certification rules or operational rules. They are those items that, if inoperative, damaged, or missing, have no effect on the aircraft’s ability to be operated safely under all operational conditions. NEF items are not instrument and equipment items already identified in the MEL or CDL of the applicable aircraft. Revision: 34 May 26, 2016

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Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST DEFINITIONS AND HOW TO USE THIS MANUAL They do not include instrument and equipment items that are functionally required to meet the certification rule or for compliance with any operational rule. In accordance with FAA order 8900.1 Vol 4 Chapter 4, the Avianca NEF program is approved via MEL Chapter 25-22-03 and as consequence does not required a signature on NEF control page; Avianca will notify by email to FAA and UAEAC when a NEF program revision is issued for internal control and surveillance process only. 21. Operative. An operative system and/or component will accomplish its intended purpose and is consistently functioning normally within its design operating limit(s) and tolerance(s). When an MEL item specifies that an item of equipment must be operative, it does not mean that it’s operational status must be verified; it’s to be considered operative unless reported or known to be malfunctioning. When an MEL item specifies that an item of equipment must be verified operative, it means that it must be checked and confirmed operative at the interval(s) specified for that MEL item. When an MEL item specifies that an item of equipment must be verified but no interval is specified, verification is required only at the time of deferral. Other terminology sometimes used interchangeably with “operative” within the MEL is “operates normally”, "fully operative", and "considered operative”. 22. Placarding. Each inoperative instrument or equipment item must be placarded to inform and remind the crewmembers and maintenance personnel of the item condition. To the extent practical, placards should be located adjacent to the control or indicator for the item affected; however, unless otherwise specified (i.e. AFM), placard wording and location is establishing in each item MEL (as applicable). 23. Repair Category. All users of an MEL approved under parts 91K, 121, 125, 129, 135 and 142 must effect repairs of inoperative instrument and equipment items, deferred in accordance with the MEL, at or prior to the repair times established by the following letter designators: A. Repair Category A. This category item must be repaired within the time interval specified in the “Remarks or Exceptions” column of the aircraft operator’s approved MEL. For time intervals specified in “calendar days” or “flight days”, the day the malfunction was recorded in the aircraft maintenance record/logbook is excluded. For all other time intervals (i.e., flights, flight legs, cycles, hours, etc.), repair tracking begins at the point when the malfunction is deferred in accordance with the operator’s approved MEL. B. Repair Category B. This category item must be repaired within 3 consecutive calendar-days (72 hours) excluding the day the malfunction was recorded in the aircraft maintenance record/logbook. For example, if it were recorded at 10 a.m. on January 26th, the 3-day interval would begin at midnight the 26th and end at midnight the 29th. C. Repair Category C. This category item must be repaired within 10 consecutive calendar-days (240 hours) excluding the day the malfunction was recorded in the aircraft maintenance record/logbook. For example, if it were recorded at 10 a.m. on January 26th, the 10-day interval would begin at midnight the 26th and end at midnight February 5th. D. Repair Category D. This category item must be repaired within 120 consecutive calendar-days (2880 hours) excluding the day the malfunction was recorded in the aircraft maintenance record/logbook. 24. Takeoff. Takeoff is the act of beginning a flight in which an aircraft is accelerated from a state of rest to that of flight. For the purposes of MEL relief, this translates to the point at which the pilot physically begins to apply power for the purpose of taking flight.


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Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST DEFINITIONS AND HOW TO USE THIS MANUAL 25. Visible Moisture. An atmospheric environment containing water, in any form, that can be seen in natural or artificial light; for example, clouds, fog, rain, sleet, hail, or snow. 26. Visual Flight Rules (VFR). VFR is as defined in 14 CFR Part 91. This precludes a pilot from filing an Instrument Flight Rules (IFR) flight plan. 27. Visual Meteorological Conditions (VMC). VMC means the atmospheric environment is such that would allow a flight to proceed under the visual flight rules applicable to the flight. This does not preclude operating under Instrument Flight Rules. 28. (M). This symbol indicates a requirement for a specific maintenance procedure which must be accomplished prior to operation with the listed item inoperative. Normally, these procedures are accomplished by maintenance personnel; however, other personnel may be qualified and authorized to perform certain functions. Procedures requiring specialized knowledge or skill, or requiring the use of tools or test equipment, should be accomplished by maintenance personnel. The satisfactory accomplishment of all maintenance procedures, regardless of who performs them, is the responsibility of the aircraft operator. Appropriate procedures are required to be produced as part of the aircraft operator’s manual or MEL. NOTE: During every corrective action to close DMIs, the required maintenance actions (M) must be consulted in applicable MEL or Maintenance Manual. These maintenance actions must be brought back by returning the affected systems to their normal, original condition and an entry of this procedure must be also included as part of the corrective action. 29. (O). This symbol indicates a requirement for a specific operations procedure which must be accomplished in planning for and/or operating with the listed item inoperative. Normally, these procedures are accomplished by the flightcrew; however, other personnel may be qualified and authorized to perform certain functions. The satisfactory accomplishment of all procedures, regardless of who performs them, is the responsibility of the aircraft operator. Appropriate procedures are required to be produced as a part of the aircraft operator’s manual or MEL. 30. Electronic Fault Alerting System. New generation aircraft display system fault indications to the flight crew by use of computerized display systems. Aircraft manufacturers incorporate individual design philosophies when determining the data that is represented. The following are customized definitions (specific to each manufacturer) to help determine the level of messages affecting the aircraft's dispatch status. AIRBUS (A318/A319/A320/A321) Airbus aircraft equipped with Electronic Centralized Aircraft Monitoring (ECAM) provide different levels of system condition messages (WARNING (Red), CAUTION (amber)). On A318/A319/A320/A321 the ECAM STATUS page also provides MAINTENANCE STATUS messages. Any message that affects airplane dispatch is displayed at the WARNING or CAUTION level. For A318/A319/A320/A321, MAINTENANCE STATUS messages may also affect airplane dispatch. System faults that result only in messages on the Centralized Fault Display System (CFDS) do not affected airplane dispatch and do not require action other c as addressed within the operator’s standard maintenance program. 31. Extended overwater flight. A Flight operated over water at a distance of more than 93 Km (50 NM) or 30 minutes at normal cruising speed, whichever is the lesser, away from land suitable for making an emergency landing (refer to OACI Annex 6 parts II)


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Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST DEFINITIONS AND HOW TO USE THIS MANUAL 32. Equipment Relief without Passengers. The FAR requires specific items of equipment to be onboard airplanes for passenger carrying operations, the MMEL provides relief for these items allows operators the ability to position aircraft to another location and still carry cargo, crew members and other authorized persons. The following persons, but no others, may be carried aboard an airplane without complying with the passenger carrying airplane requirements: 1- A crewmember. 2- A company employee. 3- An FAA air carrier inspector, a DOD commercial air carrier evaluator, or an authorized representative of the National Transportation Safety Board, who is performing official duties 4- A person necessary for: 4.1 The safety of the flight; 4.2 The safe handling of animals; 4.3 The safe handling of hazardous materials whose carriage is governed by regulations in 49 CFR part 175; 4.4 The security of valuable or confidential cargo; 4.5 The preservation of fragile or perishable cargo; 4.6 Experiments on, or testing of, cargo containers or cargo handling devices; 4.7 The operation of special equipment for loading or unloading cargo; and 4.8 The loading or unloading of outsize cargo. The pilot in command may authorize a person previously listed to be admitted to the crew compartment of the airplane.

NOTE 1: When an item MEL has no category and the quantity installed is equal to the quantity required for Dispatch, the item is considered as NO GO item. NOTE 2: When an item MEL has category and the quantity installed is equal to the quantity required for Dispatch is considered a degradation of the related item.

Notes applicable to Items MEL from CEO (Current Engine Option) and/or NEO (New Engine Option): 1- When an item MEL has no the acronym “CEO” or “NEO” is applicable to all aircraft of the fleet or model. 2- When an item MEL has acronym “NEO” is only applicable to the NEO´s Aircraft. 3- When an item MEL has acronym “CEO” is only applicable to the CEO´s Aircraft.


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Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST DEFINITIONS AND HOW TO USE THIS MANUAL



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Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST PREAMBLE

(Effective 6/14/89) The following is applicable for authorized certificate holders operating under Title 14 Code of Federal Regulations (14 CFR) Parts 121, 125, 129, 135: 14 CFR require that all equipment installed on an aircraft in compliance with the Airworthiness Standards and the Operating Rules must be operative. However, the Rules also permit the publication of a Minimum Equipment List (MEL) where compliance with certain equipment requirements is not necessary in the interests of safety under all operating conditions. Experience has shown that with the various levels of redundancy designed into aircraft, operation of every system or installed component may not be necessary when the remaining operative equipment can provide an acceptable level of safety. A Master Minimum Equipment List (MMEL) is developed by the FAA, with participation by the aviation industry, to improve aircraft utilization and thereby provide more convenient and economic air transportation for the public. The FAA approved MMEL includes those items of equipment related to airworthiness and operating regulations and other items of equipment which the Administrator finds may be inoperative and yet maintain an acceptable level of safety by appropriate conditions and limitations; it does not contain obviously required items such as wings, flaps, and rudders. The MMEL is the basis for development of individual operator MELs which take into consideration the operator's particular aircraft equipment configuration and operational conditions. Operator MELs, for administrative control, may include items not contained in the MMEL; however, relief for administrative control items must be approved by the Administrator. An operator's MEL may differ in format from the MMEL, but cannot be less restrictive than the MMEL. The individual operator's MEL, when approved and authorized, permits operation of the aircraft with inoperative equipment. Equipment not required by the operation being conducted and equipment in excess of 14 CFR requirements are included in the MEL with appropriate conditions and limitations. The MEL must not deviate from the Aircraft Flight Manual Limitations, Emergency Procedures or with Airworthiness Directives. It is important to remember that all equipment related to the airworthiness and the operating regulations of the aircraft not listed on the MMEL must be operative. Suitable conditions and limitations in the form of placards, maintenance procedures, crew operating procedures and other restrictions as necessary are specified in the MEL to ensure that an acceptable level of safety is maintained. The MEL is intended to permit operation with inoperative items of equipment for a period of time until repairs can be accomplished. It is important that repairs be accomplished at the earliest opportunity. In order to maintain an acceptable level of safety and reliability the MMEL establishes limitations on the duration of and conditions for operation with inoperative equipment. The MEL provides for release of the aircraft for flight with inoperative equipment. When an item of equipment is discovered to be inoperative, it is reported by making an entry in the Aircraft Maintenance Record/Logbook as prescribed by 14 CFR. The item is then either repaired or may be deferred per the MEL or other approved means acceptable to the Administrator prior to further operation. MEL conditions and limitations, do not relieve the operator from determining that the aircraft is in condition for safe operation with items of equipment inoperative. When these requirements are met, an Airworthiness Release, Aircraft Maintenance Record/Logbook entry, or other approved documentation is issued as prescribed by 14 CFR. Such documentation is required prior to operation with any item of equipment inoperative.


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Page: 11

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST PREAMBLE

Operators are responsible for exercising the necessary operational control to ensure that an acceptable level of safety is maintained. When operating with multiple inoperative items, the interrelationships between those items and the effect on aircraft operation and crew workload will be considered. Operators are to establish a controlled and sound repair program including the parts, personnel, facilities, procedures and schedules to ensure timely repair. WHEN USING THE MEL, COMPLIANCE WITH THE STATED INTENT OF THE PREAMBLE, DEFINITIONS, AND THE CONDITIONS AND LIMITATIONS SPECIFIED IN THE MEL IS REQUIRED.


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Page: 12

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST MANUAL CONTROL

Technical Publications publishes on the network MEL Manual for access to all Technical Vicepresidency personnel and Third Parties. In case that the access is not granted by Third Parties a hard copy will be send. Upon receipt of a revision, each manual holder will be responsible for updating the manual according to the list of effective pages for each new revision.


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Page: 13

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST EFFECTIVITY

This Manual is applicable to Avianca A318, A319, A320 and A321 aircraft, a listing of individual aircraft registration and serial numbers along with the MEL and MMEL revision status is contained in FAA Operations Specifications Paragraph D095. A listing of individual aircraft registration and serial numbers are including in Colombian Operations Specifications Section A.12.


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Page: 14

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST MEL MANAGEMENT SYSTEM 1 DEFINITION: Deferred defects are defined as those defects reported in operational service, which are deferred for later rectification. When maintenance personnel are reviewing technical log defects and ECAM1 messages, the technician approved for such action, when making decisions whether to defer a discrepancy from the technical log to the DMI2 log, must strictly comply the following procedures: NOTE: THE AVIANCA INFORMATION REMAINS INCLUDED IN THE AVIANCA GENERAL MAINTENANCE MANUAL CHAPTER 8 FOR DEFERRED REPORTS AND CHAPTER 11 FOR MAINTENANCE LOGBOOK HANDLING. 2

ISSUING OF THE DMI

The maintenance personnel will follow the next items: Thoroughly understand the pilot write up / ECAM message; if illegible or can not be easily interpreted, immediately contact the crew responsible to have a clear understanding of the defect, i.e. aircraft configuration when first noticed, attitude, speed, height, and aircraft position in operation sector. Evaluate the defect rectification for trade category, if spares required are available on site and, if able to rectify during the scheduled turnaround / downtime. Consult the aircraft Minimum Equipment List (MEL) to determine if the particular defect is deferrable, according to the policies and intervals described in that document. Write down in the technical logbook the action column by quoting MEL reference, MEL category and deferred defect item number. Write down in the Deferred Maintenance Log, which has been developing to record the maintenance information related to the Items deferred. The technician responsible for deferring the report must transcribe and record all the information to the Log. Inform to the Flight Crew the item Deferred. Create the AMOS3 Order in order to control this specific item trough the Avianca`s control system. Advise of operations dispatch office and MCC4 Department about defect and MEL reference. NOTE: DMI CONTROL IS MANAGING TROUGH THE INTERNAL AVIANCA AMOS CONTROL SYSTEM. Reliability Department should use this information to issue the Reliability monthly report, to control the repetitive and deferred Items. Each inoperative item must be placarded to inform and remind the crewmembers and maintenance personnel of the equipment condition. NOTE:TO THE EXTENT PRACTICAL, PLACARDS SHOULD BE LOCATED ADJACENT TO THE CONTROL OR INDICATOR FOR THE ITEM AFFECTED; HOWEVER, UNLESS OTHERWISE SPECIFIED, PLACARD WORDING AND LOCATION WILL BE DETERMINED BY THE OPERATOR. 3 CORRECTION OF THE DMI Any DMI correction has to be registered in the maintenance logbook (AVIANCA´s answer has to be included in the DMI log) to comply with and X1 has to be issued transcribing literally the report from the DMI log and including the actions taken to solve the discrepancy.

1

ECAM (Electronic Centralized Aircraft Monitoring) DMI (Deferred Maintenance Item) 3 AMOS (Avianca data base platform) 4 MCC (Maintenance Control Center) 2


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Page: 15

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST MEL MANAGEMENT SYSTEM

4 DMI DAILY CONTROL: Daily meeting will carry out to control the DMI items assuring that the materials, itinerary, manpower and additional resources will available before the limit dated. The personnel or its delegate identified below will conduct the daily DMI meeting: 5 DUTIES AND RESPONSIBILITIES: Quality Control Chief; who is responsible for ensuring that every DMI is accomplished within the specified interval of time, with the required tools and material and, in general, to ensure that every item is corrected according to AVIANCA’s policies established. Additionally, he/she is responsible for establishing a procedure to control extensions to DMI as approved by Aeronautical Authorities according to the registration of the aircraft. Extensions given are kept on board while the Deferred Item is finally completed. Quality Control Chief is responsible for keeping record of those extensions approved. He/she during daily meeting must request additional information to support the status of DMI items. Outstations and Maintenance Control Center Chief who is responsible to coordinate the availability of personnel and logistic when any item is to be corrected in any outstation. In addition, through the MCC controllers permanent surveillance of the DMIs will be performed and it will be documented to the whole organization in the daily morning inform, which is sent by internal net, including the responsible for corrective actions and status. Fleet Department Chiefs who are responsible for the availability of personnel when an item is to be corrected at EDR facilities. Planning / Production Control Chief, who is responsible for establishing the date when, and the location where every item is to be corrected according to category of the item, availability of personnel, material, tooling. He is also responsible to ensure that date and location agreed are the must proper according to the Maintenance Program of the aircraft affected. Material Fleet Coordinator, who is responsible to ensure the availability of material required to accomplish every Deferred Maintenance item discussed in the meeting. 6. DMI ADDITIONAL EXTENSIONS Avianca is authorized to use a continuing authorization to approve extensions to the maximum repair interval for category B and C items up to one time per item, as specified in the approval MEL, provided the responsible Flight Standar District Office if notified within 24 hours of any extension approval. The Foreign air carrier is not authorized to approve any extensions to the maximun repair interval for category A and D items as specified in the approval MEL. The Flight Standards District Office may be deny the use of this continuing authorization is abuse is evident. NOTE: After any DMI issuing or correction, Avianca´s authorized personnal will sign off the Airworthiness Release or Maintenance Release (Certificated of Release to Service) in the Aircraft Maintenance Log, according to the criteria specified in the approved Avianca General Maintenance Manual Chapter 8 and 11


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Page: 16

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 21 AIR CONDITIONING ITEM

21-00

SUBJECT

CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS

CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) Fault(s) Indicated by PACK 1 (2) (Without Mod 30626)

Not applicable to Avianca. Avianca fleet has incorporated Mod.30626

2) Fault(s) Indicated by ZONE CONT (Without Mod 30626)


3) Fault(s) Indicated by AFT CRG HEAT

Not applicable to Avianca.

4) Fault(s) Indicated by TEMP CTL 1(2) (With Mod 30626)

C

Applicable to A318, A319, A320 and A321

NOTE 1: Dispatch with any of the above maintenance status messages displayed on ECAM is permitted without CFDS interrogation. NOTE 2: The systems are designed to be fault tolerant for a period of time given on the category column in accordance with MEL preamble information. Quantities are not required for this item while the idea is to allow these fault indication.


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Page21.1


SUBJECT

21-21-01 Cabin Fans

CAT

No INS

MIN REQ

C

2

1


PLACARD Install 21-21-01 INOP placard adjacent to the cabin fan switch on overhead panel.


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Page21.2


SUBJECT

CAT

No INS

MIN REQ

C

1

0


21-21-02 CAB FAN p.b. Switch 1) OFF Light PLACARD Install 21-21-02 INOP placard adjacent to the affected cabin fan switch on overhead panel.


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Page21.3


SUBJECT

CAT

No INS

MIN REQ


21-23-01 Lavatory and Galley Extraction Fan 1) Aircraft Without Mod. 22561/MP K2335 2) Aircraft With Mod. 22561/MP K2335

Not applicable to Avianca Avianca fleet has incorporated Mod. 22561/MP K2335 C

1

0

(M) May be inoperative provided: a) Cabin duct temperatures are available on ECAM COND Page, and b) GSM ON BOARD system (if installed by Mod. 36790/MP K10889) is deactivated. (Not applicable to Avianca Fleet, Mod. 36790/MP K10889 GSM ON BOARD system not incorporated).

PLACARD Install 21-23-01 “Lavatory and Galley Extraction Fan-INOP” placard adjacent to the ventilation control panel. MAINTENANCE (M) 21-23-01 To deactivate Lavatory and Galley Extraction Fan refer to Aircraft Maintenance Manual (AMM) Task 2123-00-040-001.


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Page21.4


SUBJECT

21-26-01 Blower Fan

CAT

No INS

MIN REQ


C

1

0

(O) May be inoperative provided: a) Extract fan operates normally, b) BLOWER p.b switch is set to OVRD, c) Both packs are operative, d) VENT AVNCS SYS FAULT ECAM caution is not present, and e) FL 270 is not exceeded on airplanes with Mod. 20056. (Restriction not applicable to Avianca fleet, Modification not installed)

C

1

0

(M)(O) May be inoperative provided: a) Extract fan operates normally, b) BLOWER p.b switch is set to OVRD, c) Both packs are operative, d) Air conditioning inlet valve is verified open prior to each flight, and e) FL 270 is not exceeded on airplanes with Mod. 20056. (Restriction not applicable to Avianca fleet, Modification not installed)

C

1

0

(M)(O) May be inoperative provided: a) Extract fan operates normally, b) BLOWER p.b switch is set to OVRD, c) Both packs are operative, d) Air conditioning inlet valve is secured open, e) FL 270 is not exceeded on airplanes with Mod. 20056 (Restriction not applicable to Avianca fleet, Modification not installed), and f) AEVC test is performed before each flight.

PLACARD Install 21-26-01 INOP placard adjacent to Blower p.b. switch on the ventilation control panel OPERATIONS (O) 21-26-01 First Proviso Blower Fan (VENT AVNCS SYS FAULT Alert not displayed) DURING COCKPIT PREPARATION ‐ Supply the aircraft electrical network. ‐ Check that the air conditioning correctly operates with both air conditioning packs set to on. ‐ BLOWER pb-sw...................................................................................................................OVRD - AVNCS VENT/BLOWER/FAN (123VU AD10) C/B ……………………………………………Pull ‐ Check that the VENT AVNCS SYS FAULT and VENT EXTRACT FAULT alerts are not displayed on the EWD. NOTE: If the VENT EXTRACT FAULT alert is displayed on the EWD, the blower fan may be seized. In that case: ‐ Contact the maintenance personnel to exchange the blower fan and the extract fan. Only the VENT EXTRACT FAULT alert must then be displayed on the EWD. ‐ When the blower and extract fans are exchanged, Refer to Item MEL 21-26-02 Extract Fan. (Continued) Revision: 36 June 30, 2017

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Page21.5


SUBJECT

21-26-01

Blower Fan (Continued)

CAT

No INS

MIN REQ


Second Proviso Blower Fan (Air conditioning inlet valve checked open before each flight) DURING COCKPIT PREPARATION ‐ Supply the aircraft electrical network. ‐ Check that the air conditioning correctly operates with both air conditioning packs set to on. ‐ BLOWER pb-sw...................................................................................................................OVRD - AVNCS VENT/BLOWER/FAN (123VU AD10) C/B ……………………………………………Pull ‐ Check that the VENT EXTRACT FAULT alert is not displayed on the EWD NOTE: If the VENT EXTRACT FAULT alert is displayed on the EWD, the blower fan may be seized. In that case: ‐ Contact the maintenance personnel to exchange the blower fan and the extract fan. Only the VENT EXTRACT FAULT alert must then be displayed on the EWD. ‐ When the blower and extract fans are exchanged, Refer to Item MEL 21-26-02 Extract Fan. Third Proviso Blower Fan (Avionics ventilation system checked before each flight) DURING COCKPIT PREPARATION ‐ Supply the aircraft electrical network. ‐ Check that air the conditioning correctly operates with both air conditioning packs set to on. ‐ BLOWER pb-sw...................................................................................................................OVRD - AVNCS VENT/BLOWER/FAN (123VU AD10) C/B ……………………………………………Pull ‐ Check that the VENT EXTRACT FAULT alert is not displayed on the EWD After application of the maintenance procedure: Clear the VENT AVNCS SYS FAULT alert using the CLR p.b. The VENT AVNCS SYS FAULT alert will be displayed after landing NOTE: If the VENT EXTRACT FAULT alert is displayed on the EWD, the blower fan may be seized. In that case: ‐ Contact the maintenance personnel to exchange the blower fan and the extract fan. Only the VENT EXTRACT FAULT alert must then be displayed on the EWD. ‐ When the blower and extract fans are exchanged, Refer to Item MEL 21-26-02 Extract Fan. MAINTENANCE (M) 21-26-01 Second Proviso Blower Fan (Air conditioning inlet valve checked open before each flight) To Blower Fan Inoperative - Check that the Air Conditioned Inlet Valve is Open refer to Aircraft Maintenance Manual (AMM) task 21-26-00-040-006. Third Proviso Blower Fan (Avionics ventilation system checked before each flight) To Deactivation of the Conditioned-Air Inlet Valve when the Blower Fan is Inoperative refer to Aircraft Maintenance Manual (AMM) task 21-26-00-040-013.


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Page21.6


SUBJECT

21-26-02 Extract Fan

CAT

No INS

MIN REQ


C

1

0

(O) May be inoperative provided: a) Blower fan operates normally, b) EXTRACT p.b. sw. is set at OVRD, c) Both packs are operative, d) VENT AVNCS SYS FAULT ECAM caution is not present, and e) Outside air temperature (OAT) and time on ground with electrical power on are limited as follows: OAT < 38 degrees C - No limit OAT 39-45 degrees C - 3 hours OAT 46-50 degrees C - 2 hours OAT 51-54 degrees C - 35 min.

C

1

0

(M)(O) May be inoperative provided: a) Blower fan operates normally, b) EXTRACT p.b. sw. is set at OVRD, c) Both packs are operative, d) Air conditioning inlet valve is verified open prior to each flight, and e) Outside air temperature (OAT) and time on ground with electrical power on are limited as follows: OAT < 38 degrees C - No limit OAT 39-45 degrees C - 3 hours OAT 46-50 degrees C - 2 hours OAT 51-54 degrees C - 35 min.

C

1

0

(M)(O) May be inoperative provided: a) Blower fan operates normally, b) EXTRACT p.b. sw. is set at OVRD, c) Both packs are operative, d) Air conditioning inlet valve is secured open, e) Outside air temperature (OAT) and time on ground with electrical power on are limited as follows: OAT < 38 degrees C - No limit OAT 39-45 degrees C - 3 hours OAT 46-50 degrees C - 2 hours OAT 51-54 degrees C - 35 min, and f) AEVC test is performed before each flight.

PLACARD Install 21-26-02 INOP placard adjacent to Extract p.b. switch on the ventilation control panel (Continued) Revision: 27 May 20, 2014

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Page21.7


SUBJECT

21-26-02

Extract Fan (Continued)

CAT

No INS

MIN REQ


OPERATIONS (O) 21-26-02 First proviso Avionics Extract Fan (VENT AVNCS SYS FAULT Alert not displayed) FLIGHT PREPARATION/LIMITATIONS Time limitation on ground with electrical network supplied:

DURING COCKPIT PREPARATION ‐ Supply the aircraft electrical network. ‐ Check that the air conditioning correctly operates with both air conditioning packs set to on. ‐ EXTRACT pb-sw..................................................................................................................OVRD ‐ Clear the VENT EXTRACT FAULT alert using the CLR p.b. Applicable to A318/A319/A320: ‐ AVNCS VENT/EXTC/FAN (123VU AE2) C/B.......................................................................Pull ‐ Check that the VENT AVNCS SYS FAULT alert is not displayed on the EWD. Applicable to A321, A320NEO and A321 NEO: ‐ AVNCS VENT/EXTC/FAN (123VU AC4) C/B.......................................................................Pull ‐ Check that the VENT AVNCS SYS FAULT alert is not displayed on the EWD. Applicable to all aircraft: NOTE: If the ground horn sounds: EIS/HORN/SPLY (121VU P09) C/B...........................................................................Pull The C/B must be closed again after first engine start If the ground horn sounds after landing when engines are off, it can be silenced again. In this case, the ADIRS must be set to OFF before leaving the aircraft. Second Proviso Avionics Extract Fan (Air conditioning inlet valve checked open before each flight) FLIGHT PREPARATION/LIMITATIONS Time limitation on ground with electrical network supplied:

DURING COCKPIT PREPARATION ‐ Supply the aircraft electrical network. ‐ Check that the air conditioning correctly operates with both air conditioning packs set to on. ‐ EXTRACT pb-sw..................................................................................................................OVRD ‐ Clear the VENT EXTRACT FAULT alert using the CLR p.b. Applicable to A318/A319/A320: ‐ AVNCS VENT/EXTC/FAN (123VU AE2) C/B........................................................................Pull Applicable to A321, A320NEO and A321NEO: ‐ AVNCS VENT/EXTC/FAN (123VU AC4) C/B........................................................................Pull (Continued)


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Page21.8


SUBJECT

21-26-02

Extract Fan (Continued)

CAT

No INS

MIN REQ


Applicable to all aircraft: NOTE: If the ground horn sounds: EIS/HORN/SPLY (121VU P09) C/B............................................................................Pull The C/B must be closed again after first engine start If the ground horn sounds after landing when engines are off, it can be silenced again. In this case, the ADIRS must be set to OFF before leaving the aircraft. Third Proviso Avionics Extract Fan (Avionics ventilation system checked before each flight) FLIGHT PREPARATION/LIMITATIONS Time limitation on ground with electrical network supplied:

DURING COCKPIT PREPARATION ‐ Supply the aircraft electrical network. ‐ Check that the air conditioning correctly operates with both air conditioning packs set to on. ‐ EXTRACT pb-sw..................................................................................................................OVRD ‐ Clear the VENT EXTRACT FAULT alert using the CLR p.b. Applicable to A318/A319/A320: ‐ AVNCS VENT/EXTC/FAN (123VU AE2) C/B.......................................................................Pull Applicable to A321, A320NEO and A321NEO: ‐ AVNCS VENT/EXTC/FAN (123VU AC4) C/B.......................................................................Pull Applicable to all aircraft: After application of the maintenance procedure: Clear the VENT AVNCS SYS FAULT alert using the CLR p.b. The VENT AVNCS SYS FAULT alert will be displayed after landing. NOTE: If the ground horn sounds: EIS/HORN/SPLY (121VU P09) C/B............................................................................Pull The C/B must be closed again after first engine start If the ground horn sounds after landing when engines are off, it can be silenced again. In this case, the ADIRS must be set to OFF before leaving the aircraft. MAINTENANCE (M) 21-26-02 Second Proviso Avionics Extract Fan (Air conditioning inlet valve checked open before each flight) To Extract Fan Inoperative - Check of Conditioned-Air Inlet Valve Open refer to Aircraft Maintenance Manual (AMM) task 21-26-00-040-007. Third Proviso Avionics Extract Fan (Avionics ventilation system checked before each flight) To Extract Fan Inoperative - Do the Deactivation of the Conditioned-Air Inlet Valve refer to Aircraft Maintenance Manual (AMM) task 21-26-00-040-015.


N Registration

Page21.9


SUBJECT

21-26-03 Skin Exchanger Inlet Bypass Valve

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS (M)(O) May be inoperative provided: a) Valve is manually secured closed, and b) AEVC test is performed before each flight.

PLACARD Install 21-26-03 INOP placard adjacent to lower ECAM display OPERATIONS (O) 21-26-03 ON GROUND After application of the maintenance procedure: Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR p.b. The VENT AVNCS SYS FAULT alert will be displayed after landing. If the VENT SKIN VALVE FAULT alert is displayed on the EWD: Apply the ECAM procedure. MAINTENANCE (M) 21-26-03 To Deactivation of the Skin Exchanger Inlet Bypass Valve refer to Aircraft Maintenance Manual (AMM) 2126-00-040-001.


N Registration

Page21.10


SUBJECT

21-26-04 Skin Air Outlet Valve

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS (M)(O) May be inoperative in closed position provided: a) Internal flap (Auxiliary Flap) is manually secured to open position, b) Extract valve (skin air outlet valve) is displayed in partially open position (amber or green) on ECAM CAB PRESS page, c) Both packs are operative, d) Skin exchanger isolation valve is secured open, and e) AEVC test is performed before each flight.

PLACARD Install 21-26-04 INOP placard adjacent to lower ECAM display OPERATIONS (O) 21-26-04 ON GROUND After application of the maintenance procedure: Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR p.b. The VENT AVNCS SYS FAULT alert will be dis played after landing. If the VENT SKIN VALVE FAULT alert is displayed on the EWD: Apply the ECAM procedure. NOTE: Avionics smoke may be not perceptible from the cockpit due to the opening of the internal flap of the valve. In the case of AVIONICS SMOKE alert: Apply the ECAM procedure even if the smoke is not perceptible. MAINTENANCE (M) 21-26-04 WARNING: OPEN ONLY THE AUXILIARY FLAP. THE MAIN FLAP MUST STAY FULLY CLOSED. IF THE MAIN FLAP IS NOT FULLY CLOSED, THE AIRCRAFT WILL NOT PRESSURIZE. To Deactivation of the Skin Air Outlet Valve in the Closed Position with the Auxiliary Flap in the Open Position refer to Aircraft Maintenance Manual (AMM) 21-26-00-040-002.


N Registration

Page21.11


SUBJECT

21-26-05 Skin Air Inlet Valve

CAT

No INS

MIN REQ

C

1

0

(M)(O) May be inoperative provided: a) Valve is secured closed, b) Air conditioning inlet valve is verified open before each flight, c) Both packs are operative, and. d) AEVC test is performed before each flight

C

1

0

(M)(O) May be inoperative provided: a) Valve is secured closed, b) Air conditioning inlet valve is secured open, c) Both packs are operative, and d) AEVC test is performed before each flight.


PLACARD Install 21-26-05 INOP placard adjacent to lower ECAM display OPERATIONS (O) 21-26-05 First proviso Skin Air Inlet Valve (Air conditioning inlet valve is verified open before each flight): DURING COCKPIT PREPARATION ‐ Supply the aircraft electrical network. ‐ Check that the air conditioning is operating with one or two air conditioning packs set to on. ‐ EXTRACT pb-sw...................................................................................................................OVRD ‐ Check that the skin air inlet valve is closed on the CAB PRESS SD page. ‐ Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR p.b. NOTE: With only one air conditioning pack operative, operating time on ground is limited to 1 h. AFTER TAKEOFF EXTRACT pb-sw......................................................................................................................AUTO AFTER LANDING EXTRACT pb-sw......................................................................................................................OVRD Second proviso Skin Air Inlet Valve (Air conditioning inlet valve is secured open): DURING COCKPIT PREPARATION ‐ Supply the aircraft electrical network. ‐ Check that the air conditioning is operating with one or two air conditioning packs set to on. ‐ EXTRACT pb-sw....................................................................................................................OVRD After application of the maintenance procedure: Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR p.b. The VENT AVNCS SYS FAULT alert will be displayed after landing. NOTE: With only one air conditioning pack operative, operating time on ground is limited to 1 h. (Continued)


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Page21.12

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 21 AIR CONDITIONING ITEM 21-26-05

SUBJECT

CAT

No INS

MIN REQ


Skin Air Inlet Valve (Continued)

AFTER TAKEOFF EXTRACT pb-sw.......................................................................................................................AUTO AFTER LANDING EXTRACT pb-sw...................................................................................................................... OVRD MAINTENANCE (O) 21-26-05 First proviso Skin Air Inlet Valve (Air conditioning inlet valve is verified open before each flight): To Deactivation of the Skin Air Inlet Valve refer to Aircraft Maintenance Manual (AMM) 21-26-00-040-004. Second proviso Skin Air Inlet Valve (Air conditioning inlet valve is secured open): To Skin Air-Inlet Valve Inoperative - Do the Deactivation of the Conditioned-Air Inlet Valve refer to Aircraft Maintenance Manual (AMM) 21-26-00-040-014.


N Registration

Page21.13


SUBJECT

21-26-06 Skin Exchanger Isolation valve

CAT

No INS

MIN REQ

C

1

0

(M)(O) May be inoperative in open position provided AEVC test is performed before each flight.

C

1

0

(M)(O) May be inoperative provided a) Valve is secured open, and b) AEVC test is performed before each flight.


PLACARD Install 21-26-06 INOP placard adjacent to lower ECAM display OPERATIONAL (O) 21-26-06 First and Second Proviso After application of the maintenance procedure: Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR p.b. MAINTENANCE (M) 21-26-06 First Proviso Valve inoperative in the open position To Skin-Exchanger Isolation Valve Inoperative - Check of the Open Position of the Valve refer to Aircraft Maintenance Manual (AMM) 21-26-00-040-008. Second Proviso Valve secured open To Deactivation of the Skin-Exchanger Isolation Valve refer to Aircraft Maintenance Manual (AMM) 21-2600-040-016.


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Page21.14

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 21 AIR CONDITIONING SUBJECT

CAT

No INS

21-26-07 Skin Exchanger Outlet Bypass Valve

C

1

ITEM

MIN REQ

0


PLACARD Install 21-26-07 INOP placard adjacent to lower ECAM display


N Registration

Page21.15


SUBJECT

21-26-08 Air Conditioning Inlet Valve

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS (M)(O) May be inoperative provided: a) Valve is manually secured open, b) Both packs are operative, and c) AEVC test is performed before each flight.

PLACARD Install 21-26-08 INOP placard adjacent to lower ECAM display OPERATIONS (O) 21-26-08 ON GROUND After application of the maintenance procedure: Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR p.b. MAINTENANCE (M) 21-26-08 To Deactivation of the Conditioned-Air Inlet Valve refer to Aircraft Maintenance Manual (AMM) 21-26-00040-003.


N Registration

Page21.16


SUBJECT

21-26-09 Ventilation Filters

CAT

No INS

MIN REQ


C

1

0

(O) May be inoperative provided: a) Blower and extract fans operate normally, b) EXTRACT p.b. switch is set at OVRD, c) Both packs are operative, and d) VENT AVNCS SYS FAULT ECAM caution is not present.

C

1

0

(M)(O) May be inoperative provided: a) Blower and extract fans operate normally, b) EXTRACT p.b. switch is set at OVRD, c) Both packs are operative, and d) Air conditioning inlet valve is verified open prior to each flight.

C

1

0

(M)(O) May be inoperative provided: a) Blower and extract fans operate normally, b) EXTRACT p.b. switch is set at OVRD, c) Both packs are operative, d) Air conditioning inlet valve is secured open, and e) AEVC test is performed before each flight.

PLACARD Install 21-26-09 INOP placard adjacent to lower ECAM display OPERATIONS (O) 21-26-09 First Proviso VENT AVNCS SYS FAULT not displayed DURING COCKPIT PREPARATION ‐ Supply the aircraft electrical network. ‐ Check that the air conditioning is operating with both air conditioning packs set to on. ‐ EXTRACT pb-sw..................................................................................................................OVRD ‐ Check that the VENT AVNCS SYS FAULT alert is not displayed on the EWD. Second Proviso Air conditioning inlet valve is verified open DURING COCKPIT PREPARATION ‐ Supply the aircraft electrical network. ‐ Check that the air conditioning is operating with both air conditioning packs set to on. ‐ EXTRACT pb-sw..................................................................................................................OVRD (Continued) Revision: 27 May 20, 2014

N Registration

Page21.17

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 21 AIR CONDITIONING ITEM 21-26-09

SUBJECT

CAT

No INS

MIN REQ


Ventilation Filters (Continued)

Third Proviso Air conditioning inlet valve is secured open: DURING COCKPIT PREPARATION ‐ Supply the aircraft electrical network. ‐ Check that the air conditioning is operating with both air conditioning packs set to on. ‐ EXTRACT pb-sw..................................................................................................................OVRD After application of the maintenance procedure: Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR p.b. The VENT AVNCS SYS FAULT alert will be displayed after landing. MAINTENANCE (M) 21-26-09 Second Proviso Air conditioning inlet valve is verified open To Deactivation of the Avionics Ventilation Filter refer to Aircraft Maintenance Manual (AMM) 21-26-00040-009. Third Proviso Air conditioning inlet valve is secured open: To Avionics Ventilation Filter Inoperative - Do the Deactivation of the Conditioned-Air Inlet Valve refer to Aircraft Maintenance Manual (AMM) 21-26-00-040-017.


N Registration

Page21.18


CAT

No INS

21-26-10 Avionic Equipment Ventilation Computer (AEVC)

C

1

ITEM

MIN REQ


0

(M)(O) May be inoperative provided: a) Extract fan is verified to operate normally prior to each flight, b) BLOWER and EXTRACT p.b switches are set at OVRD, c) Air conditioning inlet valve and extract valve (skin air outlet valve) are verified in the proper position prior to each flight, d) Both packs are operative, and e) Skin air inlet valve is secured closed.

PLACARD Install 21-26-10 INOP placard (AEVC is deactivated) adjacent to lower ECAM display OPERATIONS (O) 21-26-10 DURING COCKPIT PREPARATION ‐ Supply the aircraft electrical network. ‐ Check that the conditioning is operating with both air conditioning packs set to on. ‐ BLOWER pb-sw...................................................................................................................OVRD ‐ EXTRACT pb-sw..................................................................................................................OVRD NOTE: If the ground horn sounds: EIS/HORN/SPLY (121VU P09) C/B...........................................................................Pull The C/B must be closed again after first engine start If the ground horn sounds after landing when engines are off, it can be silenced again. In this case, the ADIRS must be set to OFF before leaving the aircraft. NOTE: In the case of a low pressure in the avionics compartment ventilation ducts, the weather radar image may not be displayed on the ND on ground. Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR p.b IN FLIGHT In the case of an air conditioning pack failure: ‐ The cabin altitude may reach about 9 700 ft (3 000 m), and ‐ The CAB PR EXCESS CAB ALT alert may be displayed on the EWD. MAINTENANCE (M) 21-26-10 To Avionics Equipment Ventilation Computer Inoperative (AEVC) - Check of the Ventilation System refer to Aircraft Maintenance Manual (AMM) 21-26-00-040-005.


N Registration

Page21.19


SUBJECT

21-26-11 BLOWER FAULT Caution on ECAM

CAT

No INS

MIN REQ

C

1

0

(M) May be inoperative provided: a) Blower fan is verified operative prior to each flight, b) VENT AVNCS SYS FAULT caution is available on ECAM, and c) EXTRACT FAULT caution is not present on ECAM

C

1

0

May be inoperative provided blower fan is considered inoperative.


NOTE: Refer to item 21-26-01 Blower Fan.

PLACARD (First Proviso): Install 21-26-11 INOP placard (BLOWER FAULT warning is not serviceable) adjacent to lower ECAM display MAINTENANCE (M) 21-26-11 To Blower Fault Warning - Check of the Blower Fan and AVNCS SYS FAULT Warning refer to Aircraft Maintenance Manual (AMM) 21-26-00-040-010.

Revision: 29 October 23, 2014

N Registration

Page21.20


SUBJECT

21-26-12 EXTRACT FAULT Caution on ECAM

CAT

No INS

MIN REQ


C

1

0

(M) May be inoperative provided: a) Extract fan is verified to operate normally before each flight, b) VENT AVNCS SYS FAULT caution is available on ECAM, and c) BLOWER FAULT caution is not present on ECAM.

C

1

0

May be inoperative provided extract fan is considered inoperative. NOTE: Refer to item 21-26-02 Extract Fan.

PLACARD (First Proviso): Install 21-26-12 INOP placard (EXTRACT FAULT warning is not serviceable) adjacent to lower ECAM display MAINTENANCE (M) 21-26-12 To Extract Fault Warning - Check of the Extract Fan and AVNCS SYS FAULT Warning refer to Aircraft Maintenance Manual (AMM) 21-26-00-040-011.


N Registration

Page21.21


SUBJECT

CAT

No INS

MIN REQ

C

1

0


21-26-13 BLOWER p.b. Switch 1) FAULT Light PLACARD Install 21-26-13 INOP placard adjacent to the BLOWER p.b. switch


N Registration

Page21.22


SUBJECT

CAT

No INS

MIN REQ

C

1

0


21-26-14 EXTRACT p.b. Switch 1) FAULT Light PLACARD Install 21-26-14 INOP placard adjacent to the EXTRACT p.b. switch


N Registration

Page21.23


SUBJECT

21-26-15 ECAM CAB PRESS Indications

CAT

No INS

MIN REQ

C

2

0

REMARKS OR EXCEPTIONS INLET and EXTRACT indications may be inoperative.

PLACARD Install 21-26-15 INOP placard adjacent to the lower ECAM display


N Registration

Page21.24


SUBJECT

21-27-01 Avionics Equipment Ground Cooling System (Mod 20056/MP P0073)


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable to Avianca Avianca fleet does not have incorporated Mod 20056/MP P0073.

N Registration

Page21.25


SUBJECT

CAT

No INS

MIN REQ

D

1

0

21-28-01 Forward Cargo Extraction Fan

REMARKS OR EXCEPTIONS (O) Applicable to all A319, A320, A321 aircraft only. Except for Aircraft N195AV, N519AV, N536AV, N557AV, N789AV, N821AV, N862AV and N939AV.

PLACARD Install 21-28-01 INOP placard adjacent to the Cargo Vent Panel. OPERATIONS (O) 21-28-01 FLIGHT PREPARATION/LIMITATIONS For livestock transportation, refer to livestock transportation manual and/or Airbus Live Animal Transportation Calculation Tool and notify Dispatch.


N Registration

Page21.26


SUBJECT

21-28-02 Forward Cargo Isolation Valves

CAT

No INS

MIN REQ

D

2

0

REMARKS OR EXCEPTIONS Applicable to all A319, A320, A321 aircraft only. Except for Aircraft N195AV, N519AV, N536AV, N557AV, N789AV, N821AV, N862AV and N939AV. (O) May be inoperative provided: a) Both valves are closed, and b) FWD ISOL VALVE FAULT Light operates normally.

D

2

0

(M) May be inoperative provided both valves are secured closed.

PLACARD Install 21-28-02 INOP placard adjacent to the Cargo Vent Panel. OPERATIONS (O) 21-28-02 FLIGHT PREPARATION/LIMITATIONS For livestock transportation, refer to livestock transportation manual and/or Airbus Live Animal Transportation Calculation Tool and notify Dispatch. DURING COCKPIT PREPARATION ‐ ANN LT selector.....................................................................................................................TEST ‐ Check that the FWD ISOL VALVE pb-sw FAULT light comes on ‐ ANN LT selector.....................................................................................................................BRT or DIM ‐ FWD ISOL VALVE pb-sw.......................................................................................................OFF ‐ Check that the FWD ISOL VALVE pb-sw FAULT light does not come on. NOTE: If the FWD ISOL VALVE pb-sw FAULT light comes on: The FWD cargo isolation valve must be secured in the closed position. MAINTENANCE (M) 21-28-02 To Deactivation of the Fwd Cargo-Compartment Ventilation Isolation-Valves 4HN, 5HN refer to Aircraft Maintenance Manual (AMM) Task Number 21-28-00-040-001.


N Registration

Page21.27


SUBJECT

21-28-03 FWD ISOL VALVE Fault light

CAT

No INS

MIN REQ

D

1

0

REMARKS OR EXCEPTIONS Applicable to all A319, A320, A321 aircraft only. Except for Aircraft N195AV, N519AV, N536AV, N557AV, N789AV, N821AV, N862AV and N939AV.

PLACARD Install 21-28-03 INOP placard adjacent FWD ISOL VALVE p.b. switch.


N Registration

Page21.28


SUBJECT

CAT

No INS

MIN REQ


D

1

0

Applicable to A318 aircraft with ventilation system in the AFT cargo compartment embodied.

21-28-04 Aft Cargo Extraction Fan

(O) May be inoperative provided alternate procedures are established and used. PLACARD Install 21-28-04 INOP placard adjacent to the Cargo Vent Panel. OPERATIONS (O) 21-28-04 FLIGHT PREPARATION/LIMITATIONS For livestock transportation, refer to livestock transportation manual and/or Airbus Live Animal Transportation Calculation Tool and notify Dispatch.


N Registration

Page21.29


SUBJECT

CAT

No INS

MIN REQ


D

2

0


21-28-05 Aft Cargo Isolation Valves

(O) May be inoperative provided: a) Both valves are closed, and b) AFT ISOL VALVE FAULT Light operates normally. D

2

0

Applicable to A318 aircraft with ventilation system in the AFT cargo compartment embodied. (M) May be inoperative provided both valves are secured closed.

PLACARD Install 21-28-05 INOP placard adjacent to the Cargo Vent Panel. OPERATIONS (O) 21-28-05 FLIGHT PREPARATION/LIMITATIONS For livestock transportation, refer to livestock transportation manual and/or Airbus Live Animal Transportation Calculation Tool and notify Dispatch. DURING COCKPIT PREPARATION - ANN LT Selector……………………………………………………………………………….. TEST - Check that the FWD ISOL VALVE p.b-sw FAULT light comes on - ANN LT Selector………………………………………………………………………………. BRT or DIM - FWD ISOL VALVE p.b-sw…………………………………………………………………….. OFF - Check that the FWD ISOL VALVE p.b-sw FAULT light does not come on. NOTE: If the AFT ISOL VALVE p.b-sw FAULT light comes on: The AFT cargo isolation valve must be secured in the closed position. MAINTENANCE (M) 21-28-05 To Deactivation of the Aft Cargo-Compartment Ventilation Isolation-Valves 33HN, 34HN refer to Aircraft Maintenance Manual (AMM) Task Number 21-28-00-040-002.


N Registration

Page 21.30


SUBJECT

21-28-06 Aft Cargo AFT ISOL VALVE Fault Light

CAT

No INS

MIN REQ


D

1

0


PLACARD Install 21-28-06 INOP placard adjacent to the AFT ISOL VALVE p.b. switch.


N Registration

Page 21.31


CAT

No INS

MIN REQ

C

2

0

(O) May be inoperative provided: a) Flight is conducted in an unpressurized configuration, and b) Extended overwater flight is prohibited.

1) System 1

A

1

0

(M)(O) Except for ER operations, may be inoperative provided: a) CPC 1 is deactivated, b) Manual mode is verified to operate normally, c) Cabin pressure indications are available on ECAM CAB PRESS Page in manual mode, d) Both FCU channels operate normally, e) System 2 operates normally, and f) Repairs are made within three flight days.

2) System 2

C

1

0

(M)(O) May be inoperative provided: a) CPC 2 is deactivated, b) Manual mode is verified to operate normally, c) Cabin pressure indications are available on ECAM CAB PRESS Page in manual mode, d) Both FCU channels operate normally, and e) System 1 operates normally.

SUBJECT

21-31-01 Automatic Cabin Pressure Control Systems(CPC, outflow valve AUTO channels)


PLACARD Install 21-31-01 INOP Placard adjacent to pressure system control panel. OPERATIONS (O) 21-31-01 (Both automatic CPCs inoperative) The flight is not pressurized; refer to FCOM/PRO-SPO-20 Flight Without Cabin Pressurization. OPERATIONS (O) 21-31-01 1) 2) (Automatic CPC 1 inoperative or Automatic CPC 2 inoperative) DURING COCKPIT PREPARATION If CPC 1 is affected: AIR COND/CAB/PRESS/CTL 1 (49VU D09) C/B....................................................................Pull If CPC 2 is affected: AIR COND/CAB/PRESS/CTL 2 (122VU Y22) C/B...................................................................Pull ‐ RPCU (122VU X23) C/B (If installed).....................................................................................Pull ‐ MODE SEL pb-sw..................................................................................................................MAN (Continued)


N Registration

Page 21.32


SUBJECT

CAT

No INS

MIN REQ


21-31-01 Automatic Cabin Pressure Control Systems(CPC, outflow valve AUTO channels) (Continued) ‐ On the CAB PRESS SD page, check that the cabin differential pressure, the cabin vertical speed, the cabin altitude, and the outflow valve position are available. ‐ MAN V/S CTL sw......................................................................................................................DN ‐ On the CAB PRESS SD page, check outflow valve movement. ‐ RPCU (122VU X23) C/B (If installed).......................................................................................Push ‐ MODE SEL pb-sw....................................................................................................................AUTO MAINTENANCE (M) 21-31-01 1) To deactivate of the CPC1 refer to Aircraft Maintenance Manual (AMM) Task Number 21-31-00-040-007. MAINTENANCE (M) 21-31-01 2) To deactivate of the CPC2 refer to Aircraft Maintenance Manual (AMM) Task Number 21-31-00-040-006.


N Registration

Page 21.33


SUBJECT

21-31-02 Manual Cabin Pressure Control System

CAT

No INS

MIN REQ


C

1

0

(M) May be inoperative provided both auto cabin pressure control systems are verified to operate normally before each flight

C

1

0

(O) May be inoperative provided: a) Flight is conducted in an unpressurized configuration, b) Extended overwater flight is prohibited, and c) Avionics equipment ventilation system operates normally

PLACARD Install 21-31-02 INOP Placard adjacent to pressure system control panel. OPERATIONS (O) 21-31-02 The flight is not pressurized; refer to FCOM/PRO-SPO-20 Flight Without Cabin Pressurization. MAINTENANCE (M) 21-31-02 To Verification Test of the Automatic Cabin-Pressure Control-Systems refer to Aircraft Maintenance Manual (AMM) 21-31-00-040-002.


N Registration

Page 21.34


SUBJECT

CAT

No INS

MIN REQ


21-31-03 Outflow Valve 1) Auto Motor 2


Deleted, REV 20. Move to MMEL items 21-31-01 and 21-31-02

N Registration

Page 21.35


SUBJECT

21-31-04 Safety Valves

CAT

No INS

MIN REQ

C

2

1

REMARKS OR EXCEPTIONS (M) One may be inoperative closed provided: a) Both automatic cabin pressure control systems operate normally, and b) The three outflow valve motors operate normally.

PLACARD Install 21-31-04 INOP Placard adjacent to lower ECAM display. MAINTENANCE (M) 21-31-04 To Verification Test (Safety Valves and Outflow Valve) refer to Aircraft Maintenance Manual (AMM) 21-3100-040-001.


N Registration

Page21.36


SUBJECT

CAT

No INS

MIN REQ

C

1

0


21-31-05 Landing Elevation Selection System 1) AUTO Function

(O) May be inoperative provided LDG ELEV is set to destination field elevation altitude.

PLACARD Install 21-31-05 INOP placard adjacent to LDG ELEV knob (pressure system control panel). OPERATIONS (O) 21-31-05 BEFORE TAKEOFF ‐ Set the LDG ELEV selector on the CABIN PRESS panel at the destination airport altitude. ‐ On the CAB PRESS SD page, check that the LDG ELEV MAN message is displayed.


N Registration

Page21.37


SUBJECT

21-31-06 MODE SEL FAULT Light

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS (O) May be inoperative provided SYS 1 and SYS 2 indications on ECAM CAB PRESS page are available.

PLACARD Install 21-31-06 INOP Placard adjacent to MODE SEL p.b. switch. OPERATIONS (O) 21-31-06 Check on ECAM PRESS PAGE SYS 1 and SYS 2 are operative.


N Registration

Page21.38


SUBJECT

21-31-07 Safety Valves Position Indication on ECAM CAB PRESS page

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS (M) May be inoperative provided both safety valves are visually verified closed.

PLACARD Install 21-31-07 INOP Placard adjacent to lower ECAM display. MAINTENANCE (M) 21-31-07 To Verification Test of the Safety Valves (6HL, 7HL) (Position Indication on ECAM CAB PRESS Page) refer to Aircraft Maintenance Manual (AMM) 21-31-00-040-004.


N Registration

Page21.39


SUBJECT

21-31-08 SAFETY VALVE OPEN Caution on ECAM

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS (M) May be inoperative provided both safety valves are visually verified closed.

PLACARD Install 21-31-08 INOP Placard adjacent to lower ECAM display MAINTENANCE (M) 21-31-08 To Verification Test of the Safety Valves (6HL, 7HL) (OPEN Caution on ECAM) refer to Aircraft Maintenance Manual (AMM) 21-31-00-040-005.


N Registration

Page21.40


SUBJECT

21-43-01 Fwd Cargo Compartment Heating System


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable to Avianca. Avianca fleet does not have installed this system

N Registration

Page21.41


SUBJECT

21-43-02 Aft Cargo Compartment Heating System


CAT

No INS

MIN REQ


N Registration

Page21.42


SUBJECT

CAT

No INS

MIN REQ


21-51-01 Pack Flow Control Valves 1) (Aircraft Without Mod 30626/MP K6443) 2) (Aircraft with Mod 30626/MP K6443)

Not applicable to Avianca. Avianca fleet has incorporated Mod.30626 C

2

1

Except for ER operations, one may be inoperative provided associated air conditioning pack is considered inoperative.

C

2

0

(M)(O) Except for ER operations, may be inoperative provided: a) Flight is conducted in an unpressurized configuration, b) Avionics equipment ventilation system operates normally, c) Outside air temperature (OAT) is less than 38 degrees C, and d) Both packs are switched OFF and both flow control valves are secured closed.

PLACARD Install 21-51-01 INOP placard adjacent to associated PACK p.b. switch. OPERATIONS (O) 21-51-01 The flight is not pressurized refer to FCOM/PRO-SPO-20 Flight Without Cabin Pressurization PACK 1 pb.sw and PACK 2 pb.sw........................................................................................OFF Notify to Dispatch. MAINTENANCE (M) 21-51-01 To deactivate Pack Flow Control Valves refer to Aircraft Maintenance Manual (AMM) Task Number 21-51-00-040-001.


N Registration

Page21.43


CAT

No INS

MIN REQ

1) A319/A320

C

3

1

LO and/or NORM may be inoperative.

2) A321

C

2

1

ECON FLOW may be inoperative.

3) A318

C

2

1

HI may be inoperative

SUBJECT


21-51-02 Pack Flow Selections

PLACARD Install 21-51-02 INOP placard adjacent to affected Pack flow selector switch.


N Registration

Page21.44


CAT

No INS

MIN REQ

1) FAULT Lights

C

2

0

2) OFF Lights

C

2

0

SUBJECT


21-51-03 PACK p.b. Switch

PLACARD Install 21-51-03 INOP placard adjacent to PACK p.b. Switch affected.


N Registration

Page21.45


SUBJECT

21-51-06 Pack Flow Sensor (Aircraft with Mod. 30626)

CAT

No INS

MIN REQ

C

2

1

REMARKS OR EXCEPTIONS (O) One may be inoperative provided the HOT AIR p.b. switch is selected OFF. NOTE: For aircraft equipped with forward cargo compartment heating (Mod. 20082) refer to Livestock Transportation Manual (Not applicable to Avianca fleet).

PLACARD Install 21-51-06 INOP placard adjacent to appropriate PACK p.b. Switch. OPERATIONAL (O) 21-51-06 GENERAL INFORMATION The hot air pressure regulating valve automatically closes. The Flow Control Valve on the affected side operates in pneumatic backup mode. FLIGHT PREPARATION/LIMITATIONS  If the FWD cargo heating is installed: For live animal transportation, use the Live Animal Transportation Calculation Tool. DURING COCKPIT PREPARATION AIR COND HOT AIR pb-sw........................................................................................................ OFF Note: - Unequal passengers distribution may cause high temperature in the rear cabin when the hot air pressure regulating valve is closed. - The temperature in the cockpit may be low when the hot air pressure regulating valve is closed combined with single pack operation.


N Registration

Page21.46


SUBJECT

CAT

No INS

MIN REQ


C

2

0

(O) Except for ER operations, may be inoperative provided: a) Flight is conducted in an unpressurized configuration, b) Avionics equipment ventilation system operates normally, and c) Outside air temperature (OAT) is less than 38 degrees.

21-52-01 Packs

1) A319/A320 without Mod 31283/MP P7125 (FWC H2-F1 Stnd) and without Mod 30626/MP K6443 (Enhanced ECS)


2) A321 without Mod.31283/MP P7125 (FWC H2-F1 Stnd) and without Mod. 30626/MP K6443 (Enhanced ECS)


3) A319 with Mod.31283/MP P7125 (FWC H2-F1 Stnd) and without Mod. 30626/MP K6443 (Enhanced ECS)


4) A320 with Mod.31283/MP P7125 (FWC H2-F1 Stnd) and without Mod. 30626/MP K6443 (Enhanced ECS)

Not applicable to Avianca

5) A321 with Mod.31283/MP P7125 (FWC H2-F1 Stnd) and without Mod. 30626/MP K6443 (Enhanced ECS


(Continued)


N Registration

Page21.47


SUBJECT

CAT

No INS

MIN REQ


C

2

1

(M) Except for ER operations, one may be inoperative provided: a) Airplane remains at or below FL 310, b) AIR PACK 1(2) REGUL FAULT, AIR COND CTL 1(2)-A FAULT, and AIR COND CTL 1(2)-B FAULT cautions associated with the operative side are not displayed on ECAM, c) Affected pack p.b. sw is set to OFF, d) HI FLOW p.b. sw is set to ON, e) Avionics equipment ventilation system operates normally, and f) Pack flow control valve is secured closed.

C

2

1

(M) Except for ER operations, one may be inoperative provided: a) Airplane remains at or below FL 350, b) AIR PACK 1(2) REGUL FAULT, AIR COND CTL 1(2)-A FAULT, and AIR COND CTL 1(2)-B FAULT cautions associated with the operative side are not displayed on ECAM, c) Affected pack p.b. sw is set to OFF, d) HI FLOW p.b. sw is set to ON, e) Avionics equipment ventilation system operates normally, f) Speedbrakes operate normally, and g) Pack flow control valve is secured closed.

C

2

1

(M) Except for ER operations, one may be inoperative provided:

21-52-01 Packs (Continued) 6) A318

7) A319 With Mod 31283/MP P7125 (FWC H2-F1 Stnd) and with Mod. 30626/MP K6443 (Enhanced ECS)

a) Airplane remains at or below FL 310, b) AIR PACK 1(2) REGUL FAULT, AIR COND CTL 1(2)-A FAULT, and AIR COND CTL 1(2)-B FAULT cautions associated with the operative side are not displayed on ECAM, c) Affected pack p.b. sw is set to OFF, d) PACK FLOW selector is set to HI, e) Avionics equipment ventilation system operates normally, and f) Pack flow control valve is secured closed. (Continued)


N Registration

Page21.48


SUBJECT

CAT

No INS

MIN REQ

C

2

1


21-52-01 Packs (Continued) 7) A319 With Mod 31283/MP P7125 (FWC H2-F1 Stand) and with Mod. 30626/MP K6443 (Enhanced ECS) (Continued) (M) Except for ER operations, one may be inoperative provided: a) Airplane remains at or below FL 370, b) AIR PACK 1(2) REGUL FAULT, AIR COND CTL 1(2)-A FAULT, and AIR COND CTL 1(2)-B FAULT cautions associated with the operative side are not displayed on ECAM, c) Affected pack p.b. sw is set to OFF, d) PACK FLOW selector is set to HI, e) Avionics equipment ventilation system operates normally, f) Speedbrakes operate normally, and g) Pack flow control valve is secured closed. 8) A320 With Mod 31283/MP P7125 (FWC H2-F1 Stnd) and with Mod. 30626/MP K6443 (Enhanced ECS)

C

2

1

(M) Except for ER operations, one may be inoperative provided:

a) Airplane remains at or below FL 310, b) AIR PACK 1(2) REGUL FAULT, AIR COND CTL 1(2)-A FAULT, and AIR COND CTL 1(2)-B FAULT cautions associated with the operative side are not displayed on ECAM, c) Affected pack p.b. sw is set to OFF, d) PACK FLOW selector is set to HI, e) Avionics equipment ventilation system operates normally, and f) Pack flow control valve is secured closed. (Continued)

Revision: 31 April 24, 2015

N Registration

Page21.49


SUBJECT

CAT

No INS

MIN REQ


C

2

1

(M) Except for ER operations, one may be inoperative provided: a) AIR PACK 1(2) REGUL FAULT, AIR COND CTL 1(2)-A FAULT, and AIR COND CTL 1(2)-B FAULT cautions associated with the operative side are not displayed on ECAM, b) Affected pack p.b. sw is set to OFF, c) PACK FLOW selector is set to HI, d) Avionics equipment ventilation system operates normally, e) Speedbrakes operate normally, and f) Pack flow control valve is secured closed.

C

2

1

(M) Except for ER operations one may be inoperative provided: a) Airplane remains at or below FL 310, b) AIR PACK 1(2) REGUL FAULT, AIR COND CTL 1(2)-A FAULT, and AIR COND CTL 1(2)-B FAULT cautions associated with the operative side are not displayed on ECAM, c) Affected pack p.b. sw is set to OFF, d) ECON FLOW p.b. sw is set to OFF, e) Avionics equipment ventilation system operates normally, and f) Pack flow control valve is secured closed.

C

2

1

(M) Except for ER operations one may be inoperative provided: a) AIR PACK 1(2) REGUL FAULT, AIR COND CTL 1(2)-A FAULT, and AIR COND CTL 1(2)-B FAULT cautions associated with the operative side are not displayed on ECAM, b) Affected pack p.b. sw is set to OFF, c) ECON FLOW p.b. sw is set to OFF, d) Avionics equipment ventilation system operates normally, e) Speedbrakes operate normally, and f) Pack flow control valve is secured closed.

21-52-01 Packs (Continued) 8) A320 With Mod 31283/MP P7125 (FWC H2-F1 Stnd) and with Mod. 30626/MP K6443 (Enhanced ECS) (Continued)

9) A321 With Mod 31283/MP P7125 (FWC H2-F1 Stnd) and with Mod. 30626/MP K6443 (Enhanced ECS)

(Continued) Revision: 31 April 24, 2015

N Registration

Page21.50


SUBJECT

CAT

No INS

MIN REQ


C

2

0

(O) Except for ER operations, may be inoperative provided: a) Flight is conducted in an unpressurized configuration, b) Avionics equipment ventilation system operates normally, and c) Outside air temperature (OAT) is less than 38 degrees C.

21-52-01 Packs (Continued) 10) Air Cycle Machine (ACM)

a) A319/A320/A321 without Mod 30626/MP K6443 (Enhanced ECS)


b) A318, A319, A320, C

2

A321 with Mod. 30626/MP K6443 (Enhanced ECS)

1

(O) One pack may be operated on heat exchanger cooling only provided: a) Affected pack's compressor outlet temperature indication is available on ECAM BLEED page, b) TAT indication is available, c) AIR COND CTL 1(2)-A FAULT and AIR COND CTL 1(2)-B FAULT cautions associated with the operative side are not displayed on ECAM, d) Affected pack is not used until airborne, e) TAT is at or below 12 degrees C, and f) Avionics equipment ventilation system operates normally. NOTE: FL 310 or below must be maintained if normal operating pack fails.

PLACARD Install 21-52-01 INOP placard adjacent to appropriate PACK pb-sw affected. OPERATIONS (O) 21-52-01 ALL PROVISOS Both may be inoperative provided that the flight is not pressurized. Refer to FCOM/PRO-SPO-20 Flight Without Cabin Pressurization NOTE: When the aircraft is dispatched with both packs inoperative, the unpressurized flight must now be performed with no passengers. (Continued)


N Registration

Page21.51


SUBJECT

CAT

No INS

MIN REQ


21-52-01 Packs (Continued) OPERATIONS (O) 21-52-01 DURING COCKPIT PREPARATION PACK 1(2) pb.sw in "heat exchanger cooling only"..................................................................OFF IN FLIGHT When the TAT is equal to or less than 12°C: PACK 1(2) pb.sw in "heat exchanger cooling only"..................................................................ON If the non affected air conditioning pack fails: Maximum flight altitude.............................................................................................................31 500 ft (9 600 m) DURING DESCENT If the TAT is above 12°C: PACK 1(2) pb.sw in "heat exchanger cooling only"...................................................................OFF AT THE END OF THE DESCENT, BEFORE LANDING PACK 1(2) pb.sw in "heat exchanger cooling only"...................................................................OFF

MAINTENANCE (M) 21-52-01 ALL PROVISOS To Deactivation of the Air Conditioning Pack refer to Aircraft Maintenance Manual (AMM) 21-51-00-040002.


N Registration

Page21.52


SUBJECT

CAT

No INS

MIN REQ


21-52-02 Air Cond Pack Ram Air Inlet Flaps (Without Mod 24371) (With Mod 24371)

Not applicable to Avianca Avianca fleet has incorporated Mod 24371 C

2

0

(M) May be inoperative in the open position.

C

2

0

(O) May be inoperative in the closed position provided the associated pack(s) is (are) not used.

OPERATIONS (O) 21-52-02 Refer to Operational Procedure on MEL item 21-52-01. MAINTENANCE (M) 21-52-02 To Deactivation of the Air Inlet Flap in the Open Position refer to Aircraft Maintenance Manual (AMM) 2161-00-040-002.


N Registration

Page21.53


SUBJECT

21-52-03 Air Cond Pack Ram Air Outlet Flaps (Without Mod 26249)


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable to Avianca. Avianca fleet has incorporated Mod 26249

N Registration

Page21.54


SUBJECT

21-55-01 Emergency Ram Air Inlet

CAT

No INS

MIN REQ

C

1

0


(O) Except for ER operations and extended overwater flight, may be inoperative in the open position for unpressurized flight.

PLACARD Install 21-55-01 INOP placard on RAM AIR p.b. switch (Air Conditioning Panel). OPERATIONS (O) 21-55-01 The flight is not pressurized refer to FCOM/PRO-SPO-20 Flight Without Cabin Pressurization


N Registration

Page21.55


SUBJECT

21-55-02 ECAM Emergency RAM Air Inlet Indication (ECAM BLEED Page)

CAT

No INS

MIN REQ

C

1

0


(M) May be inoperative provided Ram Air Inlet system is verified to operate normally.

PLACARD Install 21-55-02 INOP placard adjacent to lower ECAM display. MAINTENANCE (M) 21-55-02 To Operational test of the Emergency Ram-Air Inlet System refer to Aircraft Maintenance Manual (AMM) Task Number 21-55-00-040-001.


N Registration

Page21.56


SUBJECT

21-61-01 Pack Temperature Control Primary Channels (Without Mod 30626)


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable to Avianca. Avianca fleet has incorporated Mod.30626

N Registration

Page21.57


CAT

No INS

21-61-02 Turbine bypass valves

C

2

ITEM

MIN REQ

1


PLACARD Install 21-61-02 INOP placard adjacent to lower ECAM display.


N Registration

Page21.58


SUBJECT

21-63-01 Zone Controller System (A319/A320/A321) (Without Mod30626)


CAT

No INS

MIN REQ


N Registration

Page21.59


SUBJECT

CAT

No INS

MIN REQ


21-63-02 Cockpit/Cabin Trim Air Valves (Without Mod 30626) (With Mod 30626)


3

0

(O) May be inoperative provided associated valve(s) is confirmed closed on ECAM COND page before each flight.

C

3

0

(O) May be inoperative provided hot air pressure regulating valve is confirmed operative on ECAM COND page before each flight.

C

3

0

May be inoperative provided the hot air pressure regulating valve is considered inoperative. NOTE: For aircraft equipped with forward cargo compartment heating (Mod 20082), refer to Livestock Transportation Manual. (Avianca fleet does not have Mod. 20082 incorporated)

PLACARD Install placard 21-63-02 INOP adjacent to lower ECAM display. Second Proviso Select HOT AIR pb-sw OFF. Check on ECAM COND page that hot air pressure regulating valve is closed amber. OPERATIONS (O) 21-63-02 (With Mod 30626) First proviso If affected zone temperature becomes uncomfortable select HOT AIR pb sw OFF. Second Proviso Select HOT AIR pb sw OFF then ON. Check on ECAM COND page that hot air pressure regulating valve follows HOT AIR pb sw command. If affected zone temperature becomes uncomfortable select HOT AIR pb sw OFF.


N Registration

Page21.60


SUBJECT

CAT

No INS

MIN REQ


21-63-03 Hot Air Pressure Regulating Valve (Without Mod 30626) (With Mod 30626)


1

0

May be inoperative in the closed position provided: a) HOT AIR p.b. switch is selected OFF , and b) Hot air pressure regulating valve is verified closed on ECAM COND page.

C

1

0

May be inoperative in the open position provided: a) HOT AIR p.b. switch is selected OFF , and b) All trim air valves are verified closed on ECAM COND page.

C

1

0

(M) May be inoperative provided valve is secured closed. NOTE: For aircraft equipped with forward cargo compartment heating (Mod 20082), refer to Livestock Transportation Manual. (Avianca fleet does not have Mod. 20082 incorporated).

MAINTENANCE (M) 21-63-03 To Deactivation of the Hot-Air Pressure-Regulating Valve refer to AMM 21-63-00-040-002.


N Registration

Page21.61


CAT

No INS

MIN REQ

1) Fault Light

C

1

0

2) OFF Light

C

1

0

SUBJECT


21-63-04 HOT AIR p.b. Switch May be inoperative provided zone duct temperatures are available on ECAM.

PLACARD Install 21-63-04 INOP placard adjacent to HOT AIR p.b. switch.


N Registration

Page21.62


CAT

No INS

MIN REQ

1) On COND Page

C

13

1

All indications may be inoperative, except L+R CAB FAN FAULT

2) On CRUISE Page

C

7

4

Cabin and cockpit zone indications may be inoperative.

a) Pack outlet temperature

C

2

0

b) Pack Turbine bypass valve position

C

2

0

c) Pack compressor outlet temperature

C

2

0

d) Pack Flow

C

2

0

e) Pack flow control valve position

C

2

0

C

13

11

SUBJECT


21-63-05 ECAM Indication

3) On Bleed Page

4) On CAB PRESS Page

Pack 1 and 2 indications may be inoperative.



N Registration

Page21.63


SUBJECT

CAT

No INS

MIN REQ


C

4

2

Except for ER operations, one on each side may be inoperative.

C

4

2

One on each side may be inoperative provided AIR COND CTL 1-B FAULT is not displayed on ECAM E/WD

21-63-06 Air Conditioning System Controller (ACSC) (With Mod 30626) 1) Channels COND CTL 1(2)- A(B)



N Registration

Page21.64

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 22 AUTO FLIGHT ITEM

SUBJECT

22-10-01 Autopilot Systems

CAT

No INS

MIN REQ

C

2

1

One may be inoperative provided approach minimums do not require its use

B

2

0

May be inoperative provided: a) Approach minimums do not require their use, b) Enroute operations do not require their use, and c) Number of flight segments and segment duration is acceptable to flight crew.


NOTE 1: Any mode which operates normally may be used. NOTE 2: If both Autopilot systems are inoperative, do not conduct RVSM operations) NOTE 3: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL. NOTE 4: For PBN operations refer to Appendix PBN (RNAV- RNP) operations of this MEL. PLACARD 22-10-01 Install INOP placard as applicable adjacent to autopilot engage switches on Flight Control Unit (FCU)


N Registration

Page: 22.1


SUBJECT

22-10-02 Flight Director Systems

CAT

No INS

MIN REQ

C

2

0

REMARKS OR EXCEPTIONS (O) May be inoperative provided: a) Approach minimums do not require their use, and b) Alternate takeoff procedures are established and used. NOTE : For PBN operations refer to Appendix PBN (RNAV- RNP) operations of this MEL.

PLACARD 22-10-02 Install INOP placard adjacent to applicable Flight Director engage switch OPERATIONS (O) 22-10-02 FLIGHT PREPARATION/LIMITATIONS For aircraft with the RNP AR capability, RNP AR operations are not permitted.  If both FDs are inoperative: RNAV 1 / RNAV 2 operations are not permitted. RNP 1 operations are not permitted. RNP APCH operations are not permitted. FOR TAKEOFF For a takeoff without FDs: Refer to FCOM/PRO-NOR-SRP-01-30 No Flight Director Takeoff.


N Registration

Page: 22.2


SUBJECT

CAT

No INS

MIN REQ


C

2

1

(O) One may be inoperative provided: a) Autopilots are not utilized at less than initial approach altitude, b) Priority function is verified to operate normally before each departure, and c) Approach minimums do not require the use of autopilot(s). NOTE : For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.

B

2

0

(O) May be inoperative provided: a) Autopilots are not engaged, b) Enroute operations do not require their use, c) Priority function is verified to operate normally before each departure, d) Approach minimums do not require the use of autopilots, and e) Number of flight segments and segment duration is acceptable to flight crew. NOTE : If both Autopilot Disconnect Function are inoperative, do not conduct RVSM operations.

22-10-03 Take Over p.b. Switch 1) AP Disconnect Function

PLACARD INSTRUCTIONS 22-10-03 Install INOP placard adjacent to associated side stick priority light on the glareshield OPERATIONS (O) 22-10-03 Before engines start: AP1........…………………………………………………………………………………...................................ON Operative take-over pb.......………………………………………………………………........................PRESS Check that the red AP OFF message appears on ECAM AP2.......…………………………………………………………………………………....................................ON Operative take-over pb...........………………………………………………………………....................PRESS Check that the red AP OFF message appears on ECAM Note: 1) If one is inoperative and if autopilot is used for approach, pilot flying will be the one provided with the operative button. 2) Maximum landing capability is CAT 1.


N Registration

Page: 22.3


SUBJECT

22-10-04 Autoland Lights

CAT

No INS

MIN REQ


C

2

0

May be inoperative provided approach minimums do not require use of autoland. NOTE: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.

PLACARD 22-10-04 Install INOP placard as applicable adjacent to Autoland light on glareshield


N Registration

Page: 22.4


SUBJECT

22-10-05 AP Disengagement Warning System

CAT

No INS

MIN REQ

B

1

0

REMARKS OR EXCEPTIONS May be inoperative provided both autopilots are not used. NOTE 1: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL. NOTE 2: If Autopilot Disengagement Warning is inoperative, do not conduct RVSM operations

PLACARD 22-10-05 Install INOP placard adjacent to Autopilot engage switches located on FCU


N Registration

Page: 22.5


SUBJECT

22-10-06 Side Sticks and Rudder Locking Solenoids in AP Mode

CAT

No INS

MIN REQ

C

3

1

REMARKS OR EXCEPTIONS May be inoperative unlocked provided: a) Autopilot Disconnect Warning operates normally, and b) Autoland is not used. NOTE: If one of the locking solenoids is inoperative in the unlocked position, the affected side stick or pedals will move freely and the "hard point" will not be felt any longer by pilots. This may result in an unintentional AP disconnection.

PLACARD 22-10-06 Install INOP placard adjacent to Autopilot mode selector switches


N Registration

Page: 22.6


SUBJECT

22-10-07 Autopilot FMA Indications on PFD


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Combined with Item 22-83-02.

N Registration

Page: 22.7


SUBJECT

AP/FD TCAS mode 22-10-08 (With MOD 152037/ MP P11363)

CAT

No INS

MIN REQ


D

1

0

Applicable only to A320NEO and A321NEO only (O) May be inoperative.

OPERATIONS (O) 22-10-08 IN FLIGHT In the case of a TCAS Resolution Advisory, the flight crew must apply the basic TCAS procedure. Refer to FCOM/PRO-ABN-34 TCAS WARNINGS


N Registration

Page: 22.8


SUBJECT

22-30-01 Autothrust Function

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS (M) May be inoperative provided: a) All thrust lever sensors are verified to operate normally, and b) Approach minimums do not require its use. NOTE: Alpha floor is not available with autothrust function inoperative. NOTE 1: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.

PLACARD 22-30-01 Install INOP placard adjacent to Autothrust push button switch on the FCU MAINTENANCE (M) 22-30-01 Refer to Aircraft Maintenance Manual (AMM) Task Number 22-30-00-040-004 to Check the Throttle Control Units.


N Registration

Page: 22.9


SUBJECT

22-30-02 Autothrust Instinctive Disconnect Switches

CAT

No INS

MIN REQ


C

2

1

(O) One may be inoperative provided ability to disconnect A/THR by means of the remaining Instinctive Disconnect p.b. and by the FCU A/THR p.b., is verified prior to each departure.

PLACARD 22-30-02 Install INOP placard adjacent to Autothrust engage push button on FCU. OPERATIONS (O)22-30-02 The purpose of the procedure is to check the A/THR disconnection via the remaining Instinctive Disconnect pb and via the A/THR pb on the FCU. AFTER IRS ALIGNMENT NOTE: Disregard alerts during the test. Use the EMER CANCEL pb on ECAM control panel as necessary. Aircraft configuration for the check via the FMS 1: ENG/FADEC GND PWR 1 and 2. …......................................................................….…...ON BOTH THRUST LEVERS ………………………………………………………..…..MCT FD ………………………………….........................…..…..OFF AUTO FLT/FMGC/2 (121 VU M17) C/B .............................................................................….PULL A/THR …………………………………..........................…..…....ON Check that green SPEED and white A/THR indications appear on PFD Check that A/THR pb light bars are ON. Check of the A/THR disconnection via the remaining Instinctive Disconnect pb:

A/THR instinctive disconnect pb (non affected throttle)……..........................................…...................PUSH Check that the A/THR pb light bars are OFF Check that green SPEED and white A/THR indications are no more displayed on PFD. A/THR ....................................................................................ON Check that the A/THR pb light bars are ON. Check that green SPEED and white A/THR indications are displayed on PFD. Check of the A/THR disconnection via the A/THR pb on the FCU:

A/THR pb (on FCU) ..................................................................................OFF Check that the A/THR pb light bars are OFF. Check that green SPEED and white A/THR indications are no more displayed on PFD. A/THR .....................................................................................ON Aircraft configuration for the check via the FMS 2: AUTO FLT/FMGC/2 (121VU M17) C/B ................................................................................PUSH AUTO FLT/FMGC/1 (49VU B02) C/B .................................................................................PULL Wait 2 minutes

(Continued) Revision: 36 June 30, 2017

N Registration

Page: 22.10

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 22 AUTO FLIGHT ITEM 22-30-02

SUBJECT

CAT

No INS

MIN REQ


Autothrust Instinctive Disconnect Switches (Continued)

Check of the A/THR disconnection via the remaining Instinctive Disconnect pb:

A/THR instinctive disconnect pb (non affected throttle)……..........................................…...................PUSH Check that the A/THR pb light bars are OF Check that green SPEED and white A/THR indications are no more displayed on PFD. A/THR ....................................................................................ON Check that the A/THR pb light bars are ON. Check that green SPEED and white A/THR indications are displayed on PFD. Check of the A/THR disconnection via the A/THR pb on the FCU:

A/THR pb (on FCU) ..................................................................................OFF Check that the A/THR pb light bars are OFF. Check that green SPEED and white A/THR indications are no more displayed on PFD. A/THR .....................................................................................ON Restore normal aircraft configuration: A/THR ………...………….....................................................Push AUTO FLT/FMGC/1 (49VU B02) C/B …...............................................................................PUSH ENG/FADEC GND PWR 1 and 2 …........................................................................…......OFF BOTH THRUST LEVER …............................................................................….IDLE RCL pb (on ECAM control panel). ……...........................................................................PUSH Wait at least 2 minutes before using MCDU and FD.


N Registration

Page: 22.11


SUBJECT

22-30-03 Autothrust Disengagement Warning System

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS (O) May be inoperative provided : a) autothrust is disconnected and is considered inoperative, and b) Approach minimums do not require its use. NOTE: Alpha floor is not available. NOTE 1: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.

PLACARD 22-30-03 Install INOP placard adjacent to Autothrust engage push button on FCU. OPERATIONS (O) 22-30-03 After engines start, push either autothrottle instinctive disconnect pb for at least 15 seconds. Note: 1) The A/THR system is permanently disconnected for the remainder of the flight. All A/THR functions including ALPHA FLOOR are lost. 2) Maximum landing capability is CAT 2.


N Registration

Page: 22.12


SUBJECT

22-63-01 Yaw Dampers 1) System 1

2) System 2

CAT

No INS

MIN REQ

C

1

0

C

1

0


(M) May be inoperative provided: a) System 1 is deactivated, b) System 2 is operative, and c) Approach minimums do not require its use. (M) May be inoperative provided: a) System 2 is deactivated in the case of actuator leakage b) System 1 is operative, and c) Approach minimums do not require its use. NOTE: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.

PLACARD Install INOP placard adjacent to lower ECAM display. MAINTENANCE (M) 22-63-01 1) & 2) To deactivation of the Yaw Damper Servo-Actuator refer to Aircraft Maintenance Manual (AMM) 27-26-00040-001.


N Registration

Page: 22.13


SUBJECT

CAT

No INS

MIN REQ

C

1

0


22-66-01 Flight Augmentation Computers (FAC) 1) FAC 2

(O) May be inoperative provided: a) Both FCU channels operate normally, b) ELAC, SEC, ADIRS, SFCC, RA, and LGCIU systems operate normally, and c) Approach minimums do not require its use. NOTE: Loss of FAC 1 will result in Direct Law Mode at landing gear down. NOTE 1: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.

PLACARD 22-66-01 Install INOP placard adjacent to FAC 2 switch on Flight Deck Overhead panel. OPERATIONS (O) 22-66-01 for A318 only FLIGHT PREPARATION/LIMITATIONS For aircraft with the RNP AR capability, RNP AR operations are not permitted. Maximum landing capability is CAT 3 SINGLE. ON GROUND If the AUTO FLT FAC 2 FAULT alert is displayed on the EWD or If erroneous speeds are displayed: ‐ AUTO FLT/FAC 2/28VDC (121VU M19) C/B....................................................................Pull ‐ FAC 2 pb-sw.....................................................................................................................OFF IN FLIGHT In the case of failure of the remaining FAC, or In the case of failure of the opposite yaw damper system: If severe turbulences occur: Limit the turbulence speed in accordance with the QRH and do not exceed 255 kt. Refer to QRH/OPS Severe Turbulence. OPERATIONS (O) 22-66-01 for A319, A320, A321, A320NEO and A321NEO only FLIGHT PREPARATION/LIMITATIONS For aircraft with the RNP AR capability, RNP AR operations are not permitted. Maximum landing capability is CAT 3 SINGLE. ON GROUND If the AUTO FLT FAC 2 FAULT alert is displayed on the EWD or If erroneous speeds are displayed: ‐ AUTO FLT/FAC 2/28VDC (121VU M19) C/B....................................................................Pull ‐ FAC 2 pb-sw.....................................................................................................................OFF


N Registration

Page: 22.14


CAT

No INS

MIN REQ

1) FAULT Lights

C

2

1

2) OFF Lights

C

2

0

SUBJECT


22-66-02 FAC p.b. Switch

PLACARD 22-66-02 Install INOP placard adjacent to associated FAC switch on Flight Deck Overhead panel.


N Registration

Page: 22.15


SUBJECT

CAT

No INS

MIN REQ


22-66-03 Windshear Detection/Guidance And Avoidance Systems 1) Windshear Detection and Avoidance System (Predictive)

2) Windshear Warning and Flight Guidance System(Reactive)

Moved to item 34-41-01

B

2

0

(O) May be inoperative provided alternate procedures are established and used. NOTE: Operator’s alternate procedures should include reviewing windshear avoidance and windshear recovery procedures.

C

2

0

(O) May be inoperative provided: a) Alternate procedures are established and used, and b) Windshear Detection and Avoidance System (Predictive) operates normally.

PLACARD Reactive Windshear Install 22-66-03 INOP placard adjacent to upper ECAM Display. OPERATIONS (O) 22-66-03 2) 1.

Flight may be conducted if there are no windshear conditions for takeoff and none are forecast for landing

2.

If current weather reports for route(s) to be flown indicate thunderstorms or other potentially hazardous condition may be present, verify normal operation of Weather Radar System when clear of ramp area.

3.

Refer to FCOM PRO-ABN-80 Miscellaneous Abnormal & Emergency Procedures Windshear and FCOM PRO-SUP-91-20 Operations in Windshear or Downburst Conditions.


N Registration

Page: 22.16


SUBJECT

22-72-01 Lateral Navigation

CAT

No INS

MIN REQ

C

2

1

REMARKS OR EXCEPTIONS One may be inoperative provided operations/procedures do not require its use. NOTE: For PBN operations refer to Appendix PBN (RNAV- RNP) operations of this MEL.

PLACARD 22-72-01 Install INOP placard adjacent to the applicable MCDU panel.


N Registration

Page: 22.17


SUBJECT

22-73-01 Performance Information and/or Vertical Navigation

CAT

No INS

MIN REQ

C

2

0

REMARKS OR EXCEPTIONS May be inoperative provided operations/procedures do not require their use.



N Registration

Page: 22.18

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 22 AUTO FLIGHT SUBJECT

CAT

No INS

22-73-02 Fuel/Time Predictions

C

2

ITEM

MIN REQ

0

REMARKS OR EXCEPTIONS May be inoperative provided operations/procedures do not require their use.



N Registration

Page: 22.19


SUBJECT

22-73-05 Navigation


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Moved to item 34-61-01.

N Registration

Page: 22.20


SUBJECT

22-75-01 RNP p.b switch ON Light


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not Applicable to Avianca

N Registration

Page: 22.21


SUBJECT

22-75-02 RNP p.b switch


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not Applicable to Avianca

N Registration

Page: 22.22


SUBJECT

22-81-01 FCU 1) Channels

CAT

No INS

MIN REQ


B

2

1

Except for ER operations, one may be inoperative provided 2 RMPs, all DUs, both RAs, both LGCIUs, both FACs, both cabin pressure controllers, the three ADIRS and standby altimeter (or ISIS Baroaltimeter function)operate normally.

A

2

1

One may be inoperative for one flight leg provided 2 RMPs, all DUs, both RAs, both LGCIUs, both FACs, both cabin pressure controllers, the three ADIRS and standby altimeter (or ISIS Baroaltimeter function)operate normally. NOTE: For PBN operations refer to Appendix PBN (RNAV- RNP) operations of this MEL.

PLACARD 22-81-01 Install INOP placard adjacent to the associated FCU push button switch.


N Registration

Page: 22.23


CAT

No INS

MIN REQ


a) LOC

C

1

0

May be inoperative provided approach minimums do not require its use.

b) EXPED (Without Mod 24414)

C

1

0

May be inoperative provided crew procedures do not require its use.

c) APPR

C

1

0


SUBJECT

22-81-03 Auto Flight Control Panel 1) Mode Engagement Pb

NOTE 1: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL. NOTE 2: For PBN operations refer to Appendix PBN (RNAV- RNP) operations of this MEL. 2) Selection Windows (Without Mod 24035, 24160, 23963, or 24211)

Not applicable to Avianca. Avianca fleet has included Mod. 24035

3) Selection Windows (With Mod 24035, 24160, 23963, or 24211)

C

4

1

SPD MACH, HDG TRK, and V/S FPA windows may be inoperative provided: a) Associated indications are operative on both PFD's and both ND's, and b) Procedures are not dependent on their use.

4) HDG-V/S TRK-FPA Change Over p.b.

C

1

0

May be inoperative provided: a) a) HDG-V/S selection is operative, and b) Crew procedures do not require use of Pb

5) SPD/MACH Change Over p.b

C

1

0

May be inoperative provided SPD selection is operative.

6) Metric ALT p.b

C

1

0

(O) May be inoperative provided alternate procedures are established and used.

D

1

0

May be inoperative provided operations do not require its use

7) Engagement p.b. Light Bars

D

3

0

May be inoperative provided associated indication is available on both PFD's.

8) V/S-FPA Selection Knob

C

1

0

May be inoperative provided procedures do not require its use.

9) V/S-FPA Push-to level OFF function

C

1

0


(O) May be inoperative provided: a) V/S-FPA selection knob operates normally, and b) Alternate procedures are established and used. (Continued)

N Registration

Page: 22.24

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 22 AUTO FLIGHT ITEM 22-81-03

SUBJECT

CAT

No INS

MIN REQ


Auto Flight Control Panel (Continued)

PLACARD 22-81-03 Install INOP placard adjacent to appropriate push button switch on AFC panel OPERATIONS (O) 22-81-03 6) Refer to FCOM PER-OPD-GEN OPERATIONS (O) 22-81-03 9) Establish an upper rate of descent/ascent to get Target Altitude or disconnect Autopilot to do manual leveling.


N Registration

Page: 22.25

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 22 AUTO FLIGHT SUBJECT

CAT

No INS

22-81-04 EFIS Control Panel 1) Baro Reference Display Windows

C

2

1

a) Hg

C

2

0

May be inoperative provided: a) Route of flight does not require its use, and b) Both hPa indications are available on EFIS control panel.

b) hPa

C

2

0

May be inoperative provided: a) Route of flight does not require its use, and b) Both Hg indications are available on EFIS control panel.

3) ILS/LS Pushbutton

C

2

1

Note: FAR and RAC requirements are already included herein.

4) Optional Data Display p.b.

C

10

0

May be inoperative provided operations/procedures do not require their use.

5) ND Range

C

2

1

One may be inoperative provided the ND unit associated with the operative ND range selector is operative.

6) ND Mode Select

C

2

1

One may be inoperative provided: a) ND unit associated with the operative ND selector is operative, and b) Operations/procedures do not require its use.

7) ADF/VOR Sel

C

4

2


8) Display p.b. Light Bars

D

14

0

May be inoperative provided associated indication is available on associated PFD or ND.

ITEM

MIN REQ


2) Baro Reference Sel Outer Ring (Hg/hPa)

PLACARD Install 22-81-04 INOP placard adjacent to appropriate function on EFIS control panel.


N Registration

Page: 22.26


SUBJECT

22-81-06 Automatic Landing System (AUTOLAND)


CAT

No INS

MIN REQ


C

1

0


N Registration

Page: 22.27


SUBJECT

CAT

No INS

MIN REQ

C

2

1


22-82-01 Multi Purpose Control Display Units (MCDU) 1) Flight Crew Positions 2) Maintenance MCDU

3) MCDU Annunciator Lights

One may be inoperative provided navigation procedures do not require its use. Not applicable to Avianca Avianca fleet does not have this optional item installed.

C

4

0 NOTE: For PBN operations refer to Appendix PBN (RNAV- RNP) operations of this MEL.

PLACARD 22-82-01 Install INOP on placard affected MCDU


N Registration

Page: 22.28


SUBJECT

CAT

No INS

MIN REQ


A

2

1

(M)(O) Except for ER operations, one may be inoperative provided: a) Alternate procedures are established and used, b) Affected FMGC is deactivated, and c) Repairs are made within three flight legs.

22-83-01 Flight Management Guidance Computer (FMGC)

NOTE 1: Without Mod. 34825 (Applicable to A318 aircraft only) If FMGC 1 is inoperative, the terrain function of the TAWS is inoperative refer to MEL 3448-01. NOTE 2: For PBN operations refer to Appendix PBN (RNAV- RNP) operations of this MEL. NOTE 3: If FMGC is inoperative the related Navigation Database is not accessible. Refer to MEL 34-61-01. NOTE 4 : For CAT II/III dispatch refer to Appendix CAT II/III of this MEL. PLACARD 22-83-01 Install INOP placard adjacent to both MCDUs OPERATIONS (O) 22-83-01 FLIGHT PREPARATION/LIMITATIONS For aircraft with the RNP AR capability, RNP AR operations are not permitted. Maximum landing capability is CAT 3 SINGLE.  If the BACK/UP NAV function is inoperative: RNAV 10 operations are not permitted. RNP 4 operations are not permitted. DURING COCKPIT PREPARATION

If FMGC 1 affected: C/B AUTO FLT/FMGC/1 (49VU B02 or 121VU M16) If FMGC 2 affected: C/B AUTO FLT/FMGC/2 (121VU M17)

……………………………………...PULL ….………………………….PULL

Note: During IR alignment, when FMGC 2 is deactivated, IRS IN ALIGN memo cannot be displayed until FD 1 is engaged. 1) FMGC operates on single mode; Entries can still be made from either MCDU. 2) Verify departure and destination airport weather is at and forecast to remain within VFR minimums for proposed departure and arrival times. MAINTENANCE (M) 22-83-01 Pull and collar associated FMGC circuit breaker AUTO FLT/FMGC/1 (49VU B02) or AUTO FLT/FMGC/2 (121VU M17) Revision: 36 June 30, 2017

N Registration

Page: 22.29


SUBJECT

CAT

No INS

MIN REQ

C

2

1

Indications may be inoperative on PNF FMA.

B

2

0

Except for ER operations, indications may be inoperative on both FMAs provided: a) Autopilots/Flight Directors are not engaged, b) Enroute operations do not require their use, and c) Approach minimums do not require use of autopilot. NOTE: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.

A

2

1

Indications may be inoperative on PNF FMA provided repairs are made within three flight days.

C

2

0

(O) Indications may be inoperative on both FMAs provided: a) Autothrust is disconnected and considered inoperative, and b) Approach minimums do not require their use. NOTE: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.

C

2

1

(O) One or more may be inoperative on one FMA provided approach minimums do not require their use.

C

2

0

(O) One or more may be inoperative on both FMA's provided approach minimums do not require their use. NOTE : For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.

C

1

0

May be Inoperative


22-83-02 FMA Indications on PFD 1) Autopilot/ Flight Director Related Indications

2) Autothrust Related Indications

3) Approach and Landing capabilities

4) Soft Go Around Function A320neo MOD 161254/MP P13922

PLACARD INSTRUCTIONS 22-83-02 Install INOP placard adjacent to applicable PFD (Continued) Revision: 36 June 30, 2017

N Registration

Page: 22.30


SUBJECT

CAT

No INS

MIN REQ


OPERATIONS (O) 22-83-02 -2) After engines start, push either autothrottle instinctive disconnect pb for at least 15 seconds. Check that A/THR is displayed in INOP SYS on ECAM STATUS page. OPERATIONS (O) 22-83-02 -3) FLIGHT PREPARATION/LIMITATIONS When one FMA is affected: Maximum landing capability is CAT 2. When both FMAs are affected: Maximum landing capability is CAT 1.


N Registration

Page: 22.31


SUBJECT

CAT

No INS

MIN REQ




N Registration

Page: 22.32

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 23 COMMUNICATIONS ITEM 23-00

SUBJECT

CAT

No INS

MIN REQ


CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) Fault(s) Indicated by CIDS 1 (2)

C NOTE 1: Dispatch with this maintenance status message displayed on ECAM is permitted without CFDS interrogation. NOTE 2: The systems are designed to be fault tolerant for a period of time given on the category column in accordance with MEL preamble information. Quantities are not required for this item while the idea is to allow these fault indication.


N Registration

Page: 23.1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 23 COMMUNICATIONS ITEM

SUBJECT

23-10-01 HF/VHF Communications


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Moved to 23-11-01 and 23-12-01 respectively.

N Registration

Page: 23.2


SUBJECT

23-11-01 High Frequency (HF) Communication System

CAT

No INS

MIN REQ

D

2

0

Applicable to A319, A320, A321 aircraft only.

D

1

0

Applicable to N195AV, N454AV, N519AV, N536AV, N538AV, N557AV, N603AV, N632AV, N690AV, N694AV, N696AV, N723AV, N724AV, N725AV, N728AV, N729AV, N730AV, N740AV, N742AV, N743AV, N744AV, N745AV, N748AV, N750AV, N751AV, N753AV, N759AV, N761AV, N764AV, N765AV, N821AV, N862AV and N939AV.

0

0

HF Communication System not instaled in A318 aircraft.


N477AV, N562AV, N695AV, N726AV, N741AV, N746AV, N755AV, N789AV,

May be inoperative provided, In accordance with a)

For over flight operations Beyond 30 minutes or 180 Km (100 nautical miles) from the coast line, adherence to the following instructions is required:

i. VHF1 and VHF2 Communication System operate normally. ii. Flight is not conducted for a period of two hours or more; unless two way communications can be established with a Commercial ground station or other Avianca approved facility that can relay the information to the company or to the airplane. iii. Notify dispatch. b) If flight is not conducted over water operations as mentioned on numeral a), HF communications System may be inoperative provided: i. VHF 1 and VHF 2 Communication system must be operative, ii. Notify Dispatch. c)

If paragraph a) and b) are not accomplished at least one HF must be operative.

NOTE: FAR and RAC requirements are already included herein. PLACARD 23-11-01 Install INOP placard adjacent to HF pushbutton on both Radio Management Panels


N Registration

Page: 23.3


SUBJECT

23-11-02 CALSEL System


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Deleted, REV 20.

N Registration

Page: 23.4

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 23 COMMUNICATIONS SUBJECT

CAT

No INS

23-12-01 VHF Communications Systems

D

3

ITEM

MIN REQ


2

May be inoperative provided it is not powered by an Essential Bus and not required for emergency procedures. NOTE 1: FAR and RAC requirements are already included herein. NOTE 2: In case of VHF 3 failure, the ATSU (refer to 46-21-01) is considered inoperative

PLACARD 23-12-01 Install INOP placard adjacent to VHF pushbutton on both Radio Management Panels


N Registration

Page: 23.5


CAT

No INS

MIN REQ

C

3

2

VHF No. 2 or No. 3 may be inoperative.

C

2

0

NOTE: If HF is required for flight, HF 1 select key must be operative.

C

1

0

May be inoperative provided RMP 3 operates normally.

a) VHF Comm Select Keys

C

3

2

b) HF Comm Select Keys

C

2

0


C

1

0

May be inoperative provided RMP 2 operates normally.

a) VHF Comm Select Keys

C

3

2

b) HF Comm Select Keys

C

2

0

SUBJECT


23-13-01 Radio Management Panels (RMP) 1) RMP 1 a) VHF Comm Select Keys b) HF Comm Select Keys 2) RMP 2

3) RMP 3


PLACARD 23-13-01 Install INOP placard adjacent to Radio Management Panel


N Registration

Page: 23.6


SUBJECT

23-24-01 ACARS System

CAT

No INS

MIN REQ

C

1

0


D

1

0



Note: Any ACARS function or mode that operates normally may be used. PLACARD 23-24-01 Install INOP placard adjacent to VHF 3 pushbutton on both Radio Management Panels OPERATIONS (O) 23-24-01 HF Communications system must be operative and used to communicate with the main base.


N Registration

Page: 23.7


SUBJECT

CAT

No INS

MIN REQ

23-28-01 Satellite Communication (SATCOM) System

1) Voice Channels

2) Data Channel

REMARKS OR EXCEPTIONS Applicable to Fleet A320 NEO and A321NEO Only

C

1

0


D

1

0

May be inoperative provided operations or procedures are established and used.

C

1

0


D

1

0

May be inoperative provided operation or procedures do not require its use.

C

1

0


D

1

0

May be inoperative provided operations or procedures do not require its use.

OPERATIONS (O) 23-28-01, 1) and 2) 1. Prior to each flight, the crew must perform a HF radio and SELCAL check, to ensure proper communication. 2. Notify AVA Dispatch Control Center about this condition. Required reporting points along the route of flight must be established. 3. The crew must perform adequate Flight Following procedures.


N Registration

Page: 23.8


SUBJECT

CAT

No INS

MIN REQ


B

1

0

(O) May be inoperative provided: a) Alternate normal and emergency procedures, and/or operating restrictions are established and used (See operational procedure), and b) Flight attendant alerting system (audio and visual) operates normally..

23-31-01 Passenger Address System 1) Passenger Configuration

NOTE: Any station function(s) that operates normally may be used. a) Lavatory Speakers

C

3

0


b) Cabin Speakers

C C C C

23 29 35 41

20 26 31 38

For A318 For A319 For A320 For A321 May be inoperative provided inoperative speakers are not adjacent to each other.

OPERATIONS (O) 23-31-01 -1) and -1a) Captain will brief the first attendant as follow: Before takeoff, the first attendant shall ensure direct voice communication with all the passengers in each cabin. The megaphones may be used to make these announcements. The flight crew shall be notified when preflight announcements have been completed. In an emergency, the flight crew shall notify the cabin crew and cabin crew will establish direct voice contact with each passenger. The megaphones may be used for making announcements. Flight deck/cabin interphone system must operate normally. Attendant call chimes and lights must operate normally. a) Return to seat light/sign must be operative.


N Registration

Page: 23.9


SUBJECT

23-31-02 PA IN USE LIGHT

CAT

No INS

MIN REQ

D

1

0


PLACARD 23-31-02 Install INOP placard adjacent to PA IN USE LIGHT pb-sw on 27 VU panel.


N Registration

Page: 23.10


CAT

No INS

23-42-01 Ground External Horn

C

1

ITEM

MIN REQ


0

(O) May be inoperative provided personnel are available to monitor APU.

PLACARD 23-24-01 Install INOP placard adjacent to ground call switch on overhead panel OPERATIONS (O) 23-42-01 The avionics equipment ventilation must be monitored in the cockpit when aircraft electrical network is supplied. Before leaving aircraft, the three ADIRS mode selectors must be selected OFF.


N Registration

Page: 23.11


SUBJECT

CAT

No INS

MIN REQ


23-42-02 Alerting System (Chime/Light) 1) ATT Call Lights (Flight Deck Call Lights/CAPT and F/O ACP) 2) Flight Attendant Call Lights (EMER/FWD/MID EXIT/AFT)

Moved to item 23-51-02

B B

4 8

0 0

For A318, A319 and A320 fleet For A321 fleet (O) May be inoperative provided: a) PA System is operative, b) Affected light is not used for Lavatory Smoke Detector Alerting, and c) Alternate procedures for contacting flight attendants are established and used. NOTE 1: Passenger to Attendant Call System is considered an NEF item. NOTE 2: Any visual alerting system function(s) that operate(s) normally may be used.

3) Flight Attendant Chimes

B

2

0

(O) May be inoperative provided: a) PA System operates normally, b) Affected Chime is not used for Lavatory Smoke Detector Alerting, and c) Alternate procedures for contacting flight attendants are established and used. NOTE 1: Passenger to Attendant Call System is considered an NEF item. NOTE 2: Any audio alerting system function(s) that operate(s) normally may be used

4) ALL ATTND CALL

D

1

0

OPERATION (O) 23-42-02-2) and 3) Prior to flight, the pilot in command should brief cabin crew members on the alternate emergency procedures to be used. ALTERNATE EMERGENCY PROCEDURES Alternate signals should be arranged between the Cabin Crew and the Flight Crew to provide entrance to the cockpit, while ensuring positive identification of the individual requesting flight deck access. Also, a signal should be arranged, using the PA or chimes, which will allow the captain to authorize the Flight Attendants to the cockpit.


N Registration

Page: 23.12


CAT

No INS

23-43-01 Flight Deck To Ground Interphone System

B

1

0


1) External power Panel call light

C

1

0


2) External power Panel call switch

C

1

0


ITEM

MIN REQ


PLACARD 23-43-01 Install INOP placard adjacent to Captain’s ACP and external communications panel forward of NLG bay. OPERATIONS (O) 23-43-01 -

If normal jack is inoperative, use any other service interphone jack operative Hand signals through sliding window will be used for communications between cabin and ground crew. Verify to ground crew personnel before main cabin doors is closed that ECAM message NW STRG DISC is displayed.


N Registration

Page: 23.13


SUBJECT

CAT

No INS

MIN REQ

B

2

1


23-43-02 Crewmember Interphone System 1) Passenger Configuration a) Flight Deck to Cabin, Cabin to Flight Deck.

(O) May be inoperative provided: a) Flight deck to cabin and cabin to flight deck interphone functions operate normally on at least fifty percent of the cabin handsets, and b) Alternate communications procedures between the affected Flight Attendants station(s) are established and used. NOTE: Any station function(s) that operate normally may be used.

b) Cabin to Cabin Function

B

2

0

(O) May be inoperative provided alternate communications procedures between the affected flight attendants stations are established and used. NOTE: Any station function(s) that operate normally may be used.

B

2

1

(O) May be inoperative provided: a) Cabin to cabin interphone functions operate normally on at least fifty percent of the cabin handsets, and b) Alternate communications procedures between the affected Flight Attendants station(s) are established and used. NOTE: Any station function(s) that operate normally may be used.

OPERATIONS (O) 23-43-02 a) and b) A. B.

Use PA system to communicate with cabin and use operative station to communicate with cabin crew. Use operative station to communicate with Flight Deck


N Registration

Page: 23.14


SUBJECT

CAT

No INS

MIN REQ

C

1

0


23-43-04 Handsets 1) Passenger Configuration a) Flight Deck Handset

(O) May be inoperative provided: a) Flight Deck to cabin communication operates normally, and b) Alternate procedures are established and used.

b) Cabin Attendant Handsets

D

1

0


B B

3 5

2 4

For A318, A319 and A320 fleet For A321 fleet (O) May be inoperative provided: a) Fifty percent of cabin handsets operate normally, b) Operative handset(s) is located at an operative flight attendant seat, and c) Alternate communications procedures between the affected Flight Attendants station(s) are established and used. NOTE 1: Any operative handset at an inoperative flight attendant seat shall not be counted to satisfy the fifty percent requirement NOTE 2: Any handset(s) function(s) that operate normally may be used. NOTE 3: Communication between Flight Deck and 1L station must be operative.

PLACARD 23-43-04 Install INOP placard adjacent to appropriate Flight Attendant call panel OPERATIONS (O) 23-43-04 –1)a) Use ACP to make announcements. OPERATIONS (O) 23-43-04 -1)b) A. Use PA system to communicate with cabin and use operative station to communicate with cabin crew.


N Registration

Page: 23.15


SUBJECT

23-44-01 Service Interphone Jack System

CAT

No INS

MIN REQ

C

8

0

REMARKS OR EXCEPTIONS (O)

OPERATIONS (O) 23-44-01 Hand signals through sliding window will be used for communications between cabin and ground personnel. Refer to MGO (Manual de Operaciones de Vuelo), chapter 3, (Normas generales de operación) – “Señales de mano para movimientos de Aviones”


N Registration

Page: 23.16


SUBJECT

23-51-01 Selcal (AMU)

CAT

No INS

MIN REQ

C

1

0

(O) May be inoperative provided alternate procedures are established and used

D

1

0



OPERATIONS (O) 23-51-01 1. Flight crew must monitoring appropriate ATC/ARINC or Ramp frequencies to assure operational control 2. If company frequencies are affected dispatch operations must be inform so that can established alternated procedures to contact the aircraft.


N Registration

Page: 23.17


SUBJECT

CAT

No INS

MIN REQ

C

2

1


23-51-02 Audio Control Panel (ACP) 1) CAPT and F/O

(O) One may be inoperative provided: a) ACP 3 operates normally, and b) AUDIO SWITCHING selector operates normally.

2) ACP 3

See Primary Observer Seat for relief.

3) Fourth Occupant

Not applicable to Avianca Fleet.

4) Avionics Compartment


5) ATT Call Lights (Flight Deck Call Lights/CAPT and F/O ACP)

B

2

0

May be inoperative provided the flight deck buzzer is operative. NOTE: The flight deck buzzer must always be operative.

6) Transmission key(s)

C

14

13

One may be inoperative on each ACP provided: a) VHF 1 transmission key operates normally on either CAPT ACP or F/O ACP, and b) HF 1 transmission key (If HF 1 is required) operates normally on either CAPT ACP or F/O ACP.

7) Reception Knob(s)

C

30

28

One may be inoperative on each ACP provided: a) VHF 1 reception knob operates normally on either CAPT ACP or F/O ACP, and b) HF 1 reception knob (If HF 1 is required) operates normally on either CAPT ACP or F/O ACP.

8) Reception Knob Light(s)

C

30

0

OPERATIONAL (O) 23-51-02 1) In order to recover audio channel on the affected side: AUDIO SWITCHING…………………………………………………………………CAPT 3 (F/O 3)


N Registration

Page: 23.18


SUBJECT

CAT

No INS

MIN REQ

C

1

0


23-51-03 Switching Panel 1) Audio Selector

Must operate in NORM Position.

PLACARD 23-51-03 Install INOP placard adjacent to Audio Switching Selector panel on overhead


N Registration

Page: 23.19


SUBJECT

CAT

No INS

MIN REQ

A

2

0


23-51-04 Flight Deck Headsets/ Headphones 1) Headset Boom Microphones

May be inoperative provided: a) Associated hand microphone is installed and operates normally, b) Flight Data Recorder (FDR) operates normally, and c) Repairs are made within three flight days. Note 1: The Headset-boom microphones may be inoperative provided associated hand microphone operates normally, and Note 2: The Headset-boom microphones that is assigned to each member of the crew (captain, F/O and/or Observer) is considered the quantity Installed.

2) Headset Earphones/ Headphones

C

2

1

Either Captain's or First Officer's earphone/headphones may be inoperative provided associated flight deck speaker operates normally. Note 1: See item 25-11-06. Note 2: The Headset-boom microphones may be inoperative provided associated hand microphone operates normally, and Note 3: The Headset-boom microphones that is assigned to each member of the crew (captain, F/O and/or Observer) is considered the quantity Installed.

PLACARD 23-51-04 Install INOP placard adjacent to appropriate station panel


N Registration

Page: 23.20


CAT

No INS

MIN REQ

1) CAPT/ F/O

C

2

0

May be inoperative provided associated boom microphone operates normally.

2) Observers Seat(s)/ Avionics Compartment

D

1

0

May be inoperative or missing provided procedures do not require their use.

SUBJECT


23-51-05 Hand Mic System


N Registration

Page: 23.21


SUBJECT

23-51-06 Cockpit Speakers

CAT

No INS

MIN REQ

C

2

1

REMARKS OR EXCEPTIONS The F/O speaker (speaker number 2) may be inoperative provided at least one crew member on flight deck duty wears a headset.

PLACARD 23-51-06 Install INOP placard adjacent to associated speaker volume knob


N Registration

Page: 23.22


SUBJECT

23-51-08 Side Stick Radio Selector (PTT)

CAT

No INS

MIN REQ


C

2

0

May be inoperative in open/neutral position (non transmitting position) provided INT/RAD switches on CAPT ACP, F/O ACP and ACP3 operate normally.

C

2

0

(M) May be inoperative provided: a) INT/RAD switches on CAPT ACP, F/O ACP and ACP3 operate normally, and b) Affected switch is deactivated in open/neutral position (non transmitting position).

PLACARD Install 23-51-08 INOP placard adjacent to associated side stick controller MAINTENANCE (M) 23-51-08 To Deactivation of the Radio PTT Switch refer to Aircraft Maintenance Manual (AMM) 23-51-00-040-001.


N Registration

Page: 23.23


SUBJECT

23-51-09 Passenger Audio System (Observer Position)


CAT

No INS

MIN REQ

D

1

0

N Registration


Page: 23.24


SUBJECT

23-71-01 Cockpit Voice Recorder System (CVR)

CAT

No INS

MIN REQ

A

1

0

REMARKS OR EXCEPTIONS May be inoperative provided: a) Flight Data Recorder (FDR) operates normally, and b) Repairs are made within three flight days.

1) Independent Power Source

C

1

0

Applicable to N195AV, N281AV, N284AV, N345AV, N454AV, N477AV, N481AV, N519AV, N536AV, N538AV, N557AV, N567AV, N599AV, N562AV, N603AV, N632AV, N690AV, N694AV, N695AV, N696AV, N723AV, N724AV, N725AV, N726AV, N728AV, N729AV, N730AV, N740AV, N741AV, N742AV, N743AV, N744AV, N745AV, N746AV, N748AV, N750AV, N751AV, N753AV, N755AV, N759AV, N761AV, N763AV, N764AV, N765AV, N789AV, N821AV, N862AV and N939AV.

PLACARD 23-71-01 Install INOP placard on the Cockpit Voice Recorder Panel


N Registration

Page: 23.25


SUBJECT

CAT

No INS

MIN REQ

A

1

0

C

1

0

1

0


23-71-02 RCDR Control Panel 1) RCDR/GND CTL p.b. Sw.

A

2) RCDR/GND CTL p.b. Sw. ON Light

C

1

0

3) CVR Erase p.b.

C

1

0

4) CVR TEST p.b.

A

1

0

(O) May be inoperative in AUTO position provided repairs are made within three flight days. (O) May be inoperative in ON position. May be inoperative provided: a) CVR is considered inoperative, and b) Repairs are made within three flight days.

May be inoperative provided: a) CVR is considered inoperative, and b) Repairs are made within three flight days.

OPERATIONS (O) 23-71-02 RCDR/GND CTL Pb-sw On ground : CVR can only be tested through the CVR test pb during the first 5 minutes after supply of the aircraft electrical network. After landing : If needed, CVR recording can only be stopped by pulling C/B COM/CVR/SPLY (49VU E14).


N Registration

Page: 23.26


SUBJECT

CAT

No INS

MIN REQ


A

1

0

Applicable N281AV, N284AV, N345AV, N398AV, N401AV, N411AV, N416AV, N422AV, N426AV, N446AV, N451AV, N481AV, N567AV, N599AV, N647AV, N664AV, N691AV, N729AV, N740AV, N741AV, N742AV, N743AV, N744AV, N745AV, N746AV, N748AV, N750AV, N751AV, N753AV, N755AV, N759AV, N761AV, N763AV, N764AV, N765AV, N961AV, N980AV, N992AV aircraft only

23-72-01 Flight Deck Door Visual

Surveillance Systems 1) Electric System(CDSS) (with Mod. 36414/MP K11047 or Mod. 38111/MP K11684 or Mod. 32087/MP K7778)

(O) May be inoperative provided:

a) Alternate procedures are established and used, and b) Repairs are made within three flight days. C

1

0

(O) May be inoperative provided: a) A flight deck door viewing port is installed and operates normally, and b) Alternate procedures are established and used.

D

1

0


0

0

No applicable to Avianca.

A

1

0

(O) May be inoperative provided: a) Alternate procedures are established and used, and b) Repairs are made within three flight days.

C

1

0

(O) May be inoperative provided: a) An electronic flight deck door visual surveillance system is installed and operates normally, and b) Alternate procedures are established and used.

a) Cargo Configuration 2) Viewing Ports

(Continued)


N Registration

Page: 23.27


SUBJECT

CAT

No INS

MIN REQ

D

1

0


0

0

No applicable to Avianca.


23-72-01 Flight Deck Door Visual

Surveillance Systems (Continued)

a) Cargo Configuration

OPERATIONS (O) 23-72-01 1) CAUTION: Before the beginning of the flight or changing crews, the Captain will coordinate with the JCP the procedure to open the door during flight. The briefing must include how the JCP will inform the Captain both normal and abnormal conditions that occurs in the cabin. Before each flight, the Captain will brief the JCP the procedure to follow when the Flight Deck Door Visual Surveillance System is inoperative. 1. Review “Procedimiento Para La Apertura De La Puerta De Cabina De Mando” in MOV Chapter 3. 2. Additionally the flight crew must use the flight deck door viewing port to ensure the area aft of the flight deck door is secure and cabin crews requesting entry are not doing so under duress. OPERATIONS (O) 23-72-01 2) CAUTION: Before the beginning of the flight or changing crews, the Captain will coordinate with the JCP the procedure to open the door during flight. The briefing must include how the JCP will inform the Captain both normal and abnormal conditions that occurs in the cabin. Before each flight, the Captain will brief the JCP the procedure to follow when the Flight Deck Door Viewing port is inoperative. 1. Review “Procedimiento Para La Apertura De La Puerta De Cabina De Mando” in MOV Chapter 3. 2. Additionally the flight crew must use the electronic flight deck door visual surveillance system to ensure the area aft of the flight deck door is secure and cabin crews requesting entry are not doing so under duress.


N Registration

Page: 23.28


SUBJECT

23-73-01 Cabin Intercommunication Data System (CIDS) CIDS Director

CAT

No INS

MIN REQ

C

2

1

REMARKS OR EXCEPTIONS (M) One may be inoperative NOTE 1: Failure of a single CIDS director is indicated by a MAINTENANCE message on the STATUS SD page. Refer to Item 23-00 1) Fault(s) Indicated by CIDS 1(2). NOTE 2: In the case of disturbance of the CIDS function, the deactivation/removal of the affected CIDS director may recover normal operation of the CIDS function. Refer to AMM TASK 23-7300-040-001.

1) Smoke Detection Function Channels (CIDS-SDF) (With Mod 30354 or with Mod 33100)

C

2

0

(O) May be inoperative provided: a) Restrictions concerning inoperative lavatory smoke detection system are applied and, b) Procedures are established and used to ensure all cargo compartment remain empty, or are verified to contain only empty cargo handling equipment, ballast (ballast may be loaded in ULDs), and/or Fly Away Kits. NOTE 1: Failure of a single SDF channel is indicated by a MAINTENANCE message on ECAM STATUS page. NOTE 2: The materials used as ballast or Fly Away Kits (K.O.B) Must not be those considered as Dangerous Materials. Refer to Avianca´s Dangerous Goods Manual NOTE 3: Class E cargo compartments require only the installation of smoke or fire detection systems (not suppression).

2) Emergency Cockpit Alerting System (ECAS)

0

0

Not applicable to Avianca Fleet

OPERATIONS (O) 23-73-01 1) Notify Dispatch (Continued)


N Registration

Page: 23.29


SUBJECT

CAT

No INS

MIN REQ


23-73-01 Cabin Intercommunication Data System (CIDS) CIDS Director (Continued) Prior to each flight pilot must confirm with the ground personnel that only ballast or the Fly Away Kit (K.O.B) is allowed to be carried on the aircraft and those items must not be considered as dangerous materials. Refer to Avianca’s Dangerous Goods Manual If K.O.B (Kit On Board) or ballast is not carried in this compartment, it must be empty. MAINTENANCE (M) 23-73-01 In the case of disturbance of the CIDS function, the deactivation/removal of the affected CIDS director may recover normal operation of the CIDS function. Refer to AMM TASK 23-73-00-040-001.


N Registration

Page: 23.30


SUBJECT

23-73-02 Cabin Intercommunication Data System (CIDS) CIDS DEU A

CAT

No INS

MIN REQ

C C C

10 12 16

5 6 8

REMARKS OR EXCEPTIONS Applicable to A318 aircraft only. Applicable to A319 and A320 aircraft only Applicable to A321 aircraft only. (M) May be inoperative provided: a) No two consecutive or adjacent DEUs are verified to be inoperative, and b) Lavatory speaker is verified to operate normally, or return to seat sign is verified to operate normally for an associated inoperative DEU.

C C C

10 12 16

5 6 8

Applicable to A318 aircraft only. Applicable to A319 and A320 aircraft. Applicable to A321 aircraft only. (M) May be inoperative provided: a) No two consecutive or adjacent DEU's are verified to be inoperative, and b) Lavatory door is locked closed and placarded “INOPERATIVE-DO NOT ENTER” for an associated inoperative DEU. NOTE 1: These provisos are not intended to prohibit lavatory use or inspections by crewmembers. NOTE 2: The following items may be affected: Loudspeakers; No Smoking/Fasten Seat Belt Signs; general illumination and Passenger Call.

MAINTENANCE (M) 23-73-02 1. 2. 3. 4.

Perform test to DEU A using PTP Make sure that there are not two consecutive or adjacent DEU’s inoperative. Confirm that lavatory speakers and return to seat signs operates normally. If lavatory speaker door not operate, lock lavatory door and placard “INOP DO NOT ENTER” refer Lavatory inoperative procedure of AVA A318/A319/A320 MEL on item 38-30-01


N Registration

Page: 23.31


SUBJECT

CAT

No INS

MIN REQ

C C

5 4

3 2


23-73-03 Cabin Inter communication Data System (CIDS) 1) CIDS DEU B

For A321 Fleet For A318/A319/A320 Fleet (M)(O) May be inoperative provided: a) DEU B and the associated handset are operative at each pair of floor level exit doors, and b) Alternate procedures are established and used. NOTE: The following items may be affected: Cabin attendant station intercommunications; slide bottle pressure indications on PTP/FAP; lavatory smoke detection system; and door bottle pressure indication on PTP/FAP.

2) Attendant Indication Panels (AIP)

3) Area Call Panel

C

2

0

May be inoperative at a non required cabin attendant station.

C

2

0

(O) May be inoperative at a required cabin attendant station provided: a) Corresponding area call panel operates normally, b) Passenger address and cabin interphone at affected station operate normally, and c) Alternate procedures are established and used.

C

1

0

May be inoperative at a non required cabin attendant station.

C

1

0

(O) May be inoperative provided: a) Corresponding Attendant Indication Panel operates normally, b) Passenger address and cabin interphone at affected station operate normally, and c) Alternate procedures are established and used.

(Continued)


N Registration

Page: 23.32


SUBJECT

CAT

No INS

MIN REQ


23-73-03 Cabin Inter communication Data System (CIDS) (Continued) 4) Lavatory Smoke Detection System (Indication on PTP/FAP)

Moved to item 23-73-07 5) and 23-73-08 9).

5) Drain Masts (Indication on PTP/FAP)

Moved to item 23-73-07 4) for aircraft without mod. 30354, or without Mod. 33100, or item 2373-08 8) for aircraft with mod. 30354. or with Mod. 33100. Note 1: All A319, A320, A321 aircrafts has incorporated mod 33100. Note 2: A318 aircrafts has incorporated mod 30354.

6) Additional Attendant Panel (AAP)

D

1

0

OPERATIONS (O) 23-73-03 -1) Item 1. Flight deck crew brief the cabin crew of the following upon (their) first flight of the day and upon subsequent changes of cabin crew personnel: - If cabin attendant station communications are affected, communication will be via the P.A. system - If slide bottle pressure and door bottle pressure are not available on PTP, visually verify slide bottle pressure and door bottle pressure on each door. - During on emergency, the cabin attendants will say the respective announcements using the PA system or the megaphones. OPERATIONS (O) 23-73-03 -2) and –3) Upon the first flight of each day and upon subsequent cabin crew changes, the captain will brief the flight attendants on the need to use area control panel in lieu of inoperative Attendant Indication Panel (AIP). -

FLT attendant’s station intercommunications may be affected. PA system must operate normally. PA may be required for cabin communications. Visually detect passengers call lights Use handset to identify crew member calling.

MAINTENANCE (M) 23-73-03 -1) Verify that FWD Galley left handset operates normally and at least one of handset at each operative station operates normally.


N Registration

Page: 23.33


SUBJECT

23-73-04 Forward Attendant Panel (FAP) (Without Mod 30354 or without Mod. 33100)


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not Applicable to Avianca Fleet. Avianca fleet has incorporated Mod 33100 (A319/A320/A321) and Mod 30354 (A318).

N Registration

Page: 23.34


SUBJECT

23-73-05 Prerecorded Announcement and Music Reproducer


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Moved to item 23-73-04 2) for aircraft without mod. 30354, or without Mod. 33100, or item 2373-08 2) for aircraft with mod. 30354 or with Mod. 33100. Note: Avianca fleet has incorporated Mod 33100 (A319/A320/A321) and Mod 30354 (A318).

N Registration

Page: 23.35


SUBJECT

23-73-06 Programmed Cabin Assignment Module (CAM)


CAT

No INS

MIN REQ

C

1

0

N Registration


Page: 23.36


SUBJECT

23-73-07 Programming and Test Panel (PTP) (Without Mod 30354, or without Mod. 33100,)


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not Applicable to Avianca Fleet. Avianca fleet has incorporated Mod 33100 (A319/A320/A321) and Mod 30354 (A318).

N Registration

Page: 23.37


SUBJECT

23-73-08 Flight Attendant Panel (FAP) (With Mod 30354 or with Mod. 33100)

CAT

No INS

MIN REQ


C

1

0

(M)(O) May be inoperative provided: a) Associated FAP functions are considered inoperative, and b) Alternate procedures are established and used.

1)

Cabin Lighting Control functions on FAP

C

4

0

(O) May be inoperative provided lighting is sufficient for cabin attendants to perform their duties.

2)

Prerecorded Announcement and Music Reproducer Control on FAP

D

1

0


3)

CABIN READY on FAP

D

1

0


4)

EVAC Light/ CMD Pb (On FAP)

D

1

0


5)

SYSTEM INOP Light on WATER WASTE Panel on FAP

D

1

0

(M) May be inoperative provided alternate procedures are established and used.

6)

Slide Bottle Pressure Indication (On FAP)

a)

Passenger Doors

C

4

0

(O) May be inoperative provided the associated slide bottle pressure is verified prior to each departure.

b)

Overwing Emergency Exits (A318/A319/A320)

C

2

0

(M) May be inoperative provided associated slide bottle pressure is verified before the first flight of each day.

Cabin Emergency Exit (A321)

C

4

0

(O) May be inoperative provided the associated slide bottle pressure is verified prior to each departure.

Door Bottle Pressure Indication (On FAP) (A318/A319/A320) (A321)

C C

4 8

0 0

(M) May be inoperative provided associated slide bottle pressure is verified before the first flight of each day.

c)

7)

(Continued)


N Registration

Page: 23.38


SUBJECT

CAT

No INS

MIN REQ


23-73-08 Flight Attendant Panel (FAP) (With Mod 30354 or with Mod. 33100) (Continued) 8)

Drain Masts Indication (On FAP)

C

1

0

9)

Lavatory Smoke Detection System (Indication on FAP)

C

1

0

10)

Other Functions (On FAP)

D

2

0

(O) May be inoperative provided alternate procedures are established and used. NOTE: EMER Pb must always be operative.

OPERATIONS (O) 23-73-08 ARMING AND DISARMING SLIDES: Each Flight Attendant will confirm via interphone and crosscheck visually. The Flight Attendant Manager (JCP) will call the Captain to inform the procedure. OPERATIONS (O) 23-73-08 1) Lights on Y/C will be operated by AAP (After Attendant panel) Lights on B/C will be set on Full Bright automatically OPERATIONS (O) 23-73-08 2) Flight Attendants will explain the procedure visually and by PA OPERATIONS (O) 23-73-08 3) This procedure will be done via interphone and PA between Flight Attendants and the CAPT. OPERATIONS (O) 23-73-08 4) The CAPT will verify operation of the P/B from the Cockpit. OPERATIONS (O) 23-73-08 6 a) The Flight Attendant Manager (JCP) keeps contact with the Captain to maintain an adequate temperature in cabin OPERATIONS (O) 23-73-08 6 c) This procedure will be done via interphone and PA between Flight Attendants and the CAPT. OPERATIONS (O) 23-73-08 10) The Flight Attendant Manager (JCP) keeps contact with the Captain to maintain an adequate temperature in cabin MAINTENANCE (M) 23-73-08 For Flight Attendant Panel (FAP), refer to Aircraft Maintenance Manual (AMM) task Number 25-62-00040-005-A


N Registration

Page: 23.39


SUBJECT

CAT

No INS

MIN REQ


23-73-08 Flight Attendant Panel (FAP) (With Mod 30354 or with Mod. 33100) (Continued) MAINTENANCE (M) 23-73-08 5) For Flight Attendant Panel (FAP), SYSTEM INOP Light on WATER WASTE Panel on FAP, refer to Aircraft Maintenance Manual (AMM) task Number 38-31-00-740-001 MAINTENANCE (M) 23-73-08 6) For Flight Attendant Panel (FAP), Emergency Exits, refer to Aircraft Maintenance Manual (AMM) task Number 25-62-00-040-005 MAINTENANCE (M) 23-73-08 7) For Flight Attendant Panel (FAP), Door Bottle Pressure Indication (On FAP), refer to Aircraft Maintenance Manual (AMM) task Number 25-62-00-040-005


N Registration

Page: 23.40


SUBJECT

23-90-01 Cabin Surveillance System (CSS) STC No. ST02483AT


CAT

No INS

MIN REQ

0

0

REMARKS OR EXCEPTIONS Not applicable to Avianca. Avianca does not have this system.

N Registration

Page: 23.41


SUBJECT

23-90-02 Cockpit Door Surveillance System (CDSS) (with Mod. 36414/MP K11047 or Mod. 38111/MP K11684 or Mod. 32087/MP K7778).

CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Moved to 23-72-01.

PLACARD Install 23-90-02 INOP placard adjacent to Cockpit Door Panel.


N Registration

Page: 23.42


SUBJECT

23-90-03 Wireless Aircraft Data Link System (WADL) STC No. ST01447NY


CAT

No INS

MIN REQ

0

0

REMARKS OR EXCEPTIONS Not applicable to Avianca. Avianca does not have this system.

N Registration

Page: 23.43


SUBJECT

CAT

No INS

MIN REQ




N Registration

Page: 23.44

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 24 ELECTRICAL POWER ITEM 24-00

SUBJECT

CAT

No INS

MIN REQ


CLASS II MAINTENANCE MESSAGES DIS PLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) Fault(s) Indicated by DC BUS TIE

C

2) Fault(s) Indicated by GPCU or AC GEN

C NOTE 1: Dispatch with either of the above maintenance status messages displayed on ECAM is permitted without CFDS interrogation. NOTE 2: The systems are designed to be fault tolerant for a period of time given on the category column in accordance with MEL preamble information. Quantities are not required for this item while the idea is to allow these fault indication.


N Registration

Page: 24.1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 24 ELECTRICAL POWER ITEM

SUBJECT

CAT

No INS

MIN REQ


B

2

1

Applicable to A318 aircraft only. A318 aircraft has Mod 31296 and 32875 incorporated.

24-20-01 Engine Driven Generator Channel (IDG, GCU, Line Contactor) 1) CFM 56-5 Engines Aircraft with Mods: • 31296/MP P6319 (Digital AMU) and 32875/MP P7945 (GCU 5.1), or Aircraft with Mods: • 31107/MP P7009 (Digital SATCOM AMU) and 32875/MP P7945 (GCU 5.1)

(M)(O)Except for ER operations, one may be inoperative provided: a) APU generator operates normally and is used throughout the flight, b) Operator ensures that the APU oil quantity is adequate for the intended flight, c) All busses can be powered, d) All indications and warnings associated with the remaining engine and APU driven generator channels operate normally. e) Galley automatic shedding is verified to operate normally, f) Aircraft remains at or below FL330, g) Approach minimums do not require its use, and h) When the Engine Driven Generator Channel 1 is inoperative, the AC ESS FEED manual transfer must be checked to operate normally. NOTE: Relief is not applicable to aircraft with Mods:39670/MP P10300 (GCU 5.2), or 37782/MP P10402 (Digital AMU Power Supply Upgrade), or 37317/MP P10098 (AC ESS FEED automatic switching)

2) CFM 56-5 Engines (Aircraft with an analog AMU or with any of the following Mods:) • 37782/MP P10402 (Digital AMU Power Supply Upgrade), or • 37317/MP P10098 (AC ESS FEED automatic switching), or Aircraft with Mods: • 31107/MP P7009 (Digital SATCOM AMU), and • 39670/MP P10300 (GCU 5.2) and CFMLEAP-1A Engines

B

2

1

Applicable to A319, A320 and A321 aircraft with CFM 56 Engines or CFM-LEAP-1A Engines only. (M)(O) Except for ER operations, one may be inoperative provided: a) APU generator operates normally and is used throughout the flight, b) Operator ensures that the APU oil quantity is adequate for the intended flight, c) All busses can be powered, d) All indications and warnings associated with the remaining engine and APU driven generator channels operate normally, e) Galley automatic shedding is verified to operate normally, f) Aircraft remains at or below FL330, and g) Approach minimums do not require its use.


N Registration

Page: 24.2


SUBJECT

CAT

No INS

MIN REQ


24-20-01 Engine Driven Generator Channel (IDG, GCU, Line Contactor) (Continued) 3) IAE Engines (With IDGs which incorporate Mod. 26929/MP P5059/P/N 772292 or Mod.30375/MP P6557/P/N 772292), and Aircraft with either Mod: 31296/MP P6319 (Digital AMU) and 32875/MP P7945 (GCU 5.1), or 31107/MP P7009 (Digital SATCOM AMU) and 32875/MP P7945 (GCU 5.1) 4) IAE Engines (Aircraft with an Analog AMU or with any of the following Mod’s: 37782/MP P10402 (Digital AMU Power Supply Upgrade), or 37317/MP P10098 (AC ESS FEED automatic switching), or Aircraft with Mod’s:31107/MP P7009 (Digital SATCOM AMU) and 39670/MP P10300 (GCU 5.2).

Not applicable to Avianca Fleet

B

2

1

Applicable to A319, A320 and A321 aircraft with IAE Engines only. (M)(O) Except for ER operations, one may be inoperative provided: a) APU generator operates normally and is used throughout the flight b) Operator ensures that the APU oil quantity is adequate for the intended flight, c) All busses can be powered, d) All indications and warnings associated with the remaining engine and APU driven generator channels operate normally, e) Galley automatic shedding is verified to operate normally, f) Aircraft remains at or below FL330, g) Fuel recirculation system associated with the operative IDG is operative, and h) Approach minimums do not require its use.

5) PW 6000 Engines Only

Not applicable to Avianca. Avianca fleet does not have PW 6000 engines.

6) PW 1100G Engines

Not applicable to Avianca. Avianca fleet does not have PW 1100G engines.

PLACARD Install 24-20-01 INOP placard on flight Deck overhead ELEC panel. (Continued) Revision: 34 May 26, 2016

N Registration

Page: 24.3

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 24 ELECTRICAL POWER ITEM 24-20-01

SUBJECT

CAT

No INS

MIN REQ


Engine Driven Generator Channel (IDG, GCU, Line Contactor) (Continued)

OPERATIONS (O) 24-20-01 NOTE: Maximum landing capability is CAT 3 SINGLE. APU fuel consumption with APU GEN pb-sw On:

NOTE: When the External Power is disconnected, the IFE is lost until the APU supplies the electrical network. DURING COCKPIT PREPARATION Check of the galley automatic load shed system: - Supply the electrical network from the APU or the external power. - GALY & CAB pb-sw…………………………………………………………………………………….AUTO - ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24) C/B………………………………………….Pull - Check that a part of the operative galley equipment does not operate. - ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24) C/B………………………………………….Push Note: Disregard this procedure if main galleys are not connected. When the AC main generation 1 is inoperative (applicable to A318 fleet) ‐ AC ESS FEED pb-sw…………………………………………………………………………………..ALTN ‐ On the ELEC SD page, check that the AC BUS 2 supplies the AC ESS BUS. ‐ AC ESS FEED pb-sw…………………………………………………………………………………..NORM AFTER ENGINE START Check that the electrical busses have power: ‐ APU MASTER SW pb-sw..............................................................................................................ON ‐ APU GEN pb-sw…………………………………………………………………………………………On ‐ GEN 1 pb-sw……………………………………………………………………………………………..OFF ‐ GEN 2 pb-sw……………………………………………………………………………………………..OFF ‐ On the ELEC SD page, check that all AC busses have power. ‐ GEN pb-sw (operative)………………………………………………………………………………….On ‐ APU GEN pb-sw…………………………………………………………………………………………OFF ‐ On the ELEC SD page, check that all AC busses have power. ‐ APU GEN pb-sw…………………………………………………………………………………………On Note: If necessary, the IDG may be disconnected. Caution: For economical reason, the IDG should not operate for more than 50 flight hours in the disconnected mode. (Continued) Revision: 27 Page: 24.4 N Registration May 20, 2014


SUBJECT

24-20-01

CAT

No INS

MIN REQ


Engine Driven Generator Channel (IDG, GCU, Line Contactor) (Continued)

IN FLIGHT (applicable to A318 aircraft only): When the AC main generation 1 is inoperative: In the case of failure of the AC BUS 1: AC ESS FEED pb-sw……………………………………………………………………………..ALTN MAINTENANCE (M) 24-20-01 Check of the AC Main Generation Maintenance Condition refer to Aircraft Maintenance Manual (AMM) Task number 24-20-00-040-001. MAINTENANCE (M) 24-20-01 (Additional maintenance procedure required by FAA 2011-19-01 R1) NOTE:

THIS PROCEDURE MUST BE ACCOMPLISHED ONLY IF A GEN IS SHUT DOWN AUTOMATICALLY OR IF A GEN IS SHUT DOWN BY THE FLIGHT CREW AS CONSEQUENCE OF FOLLOW FAILURES: -

Affected Display Unit (DU) blank or display distorted. Diagonal line or “Invalid Data” on affected DU. Inversion of EWD and SD displays. Affected DU(s) or MCDU flashes intermittently.

The corrective actions indicated in the following Troubleshooting Manual references must be carried out before further flight, as required: - TSM 24-20-00-810-803: Loss of the GEN 1 (Failure of the Electrical Wiring between the IDG 1, GLC 1 and GCU 1) - TSM 24-20-00-810-805: Loss of the GEN 1 (Failure of the IDG 1 Feeder) - TSM 24-20-00-810-811: Loss of the GEN 2 (Failure of the Electrical Wiring between the IDG 2, GLC 2 and GCU 2) - TSM 24-20-00-810-813: Loss of the GEN 2 (Failure of the IDG 2 Feeder) - TSM 24-21-00-810-846: Failure of the IDG Cables


N Registration

Page: 24.5


SUBJECT

CAT

No INS

MIN REQ


24-20-02 APU Generator Channel 1) Aircraft without Mod. 24642/MP P3524 or AES APU without Mod. 24498/MP K3680 or without Mod. 25568/MP K4157) 2) Aircraft with Mod. 24642/MP P3524 or AES APU with Mod. 24498/MP K3680 or with Mod. 25568/MP K4157 or APIC APU or APU GTCP 1319(A))

Not applicable to Avianca Avianca fleet has incorporated those Modifications

A

1

0

Except for ER operations beyond 120 min, may be inoperative provided: a) APU GEN p.b switch is set to OFF, and b) Repairs are made within four flight legs. NOTE: When GPCU/Ground Power Control Function of the GAPCU and APU generator are both inoperative, engines cannot be started.

C

1

0

Except for ER operations, may be inoperative provided APU GEN p.b. sw is set to OFF. NOTE: When GPCU/Ground Power Control Function of the GAPCU and APU generator are both inoperative, engines cannot be started.

C

1

0

Except for ER operations, may be inoperative provided APU is not used. NOTE: When GPCU/Ground Power Control Function of the GAPCU and APU generator are both inoperative, engines cannot be started.

C

1

0

(M) Except for ER operations, may be inoperative provided APU generator is deactivated or removed. NOTE: When GPCU/GAPCU Ground Power Control Function and APU generator are both inoperative, engines cannot be started.

PLACARD 24-20-02 Install INOP placard adjacent to APU GEN push button switch MAINTENANCE (M) 24-20-02 To Deactivation of the APU Generator refer to Aircraft Maintenance Manual (AMM) 24-23-00-040-002-A. Revision: 29 October 23, 2014

N Registration

Page: 24.6


CAT

No INS

MIN REQ

1) Manual Transfer to the AC BUS 2 (ALTN Function)

C

1

0

(O) May be inoperative provided: a) AC ESS FEED p.b switch is set at NORM position, b) It is checked on the ELEC SD page that the AC BUS 1 supplies the AC ESS BUS, and c) TR 2 operates normally.

2) Automatic Transfer to the AC BUS 2 (For aircraft with Mod 37317/MP P10098)

C

1

0

Applicable to A319, A320, A321 aircraft

SUBJECT


24-20-07 AC ESS Feed Control

(O) May be inoperative provided: a) AC ESS FEED p.b switch is set at NORM position, b) It is checked on the ELEC SD page that the AC BUS 1 supplies the AC ESS BUS, and c) TR 2 operates normally.

PLACARD 24-20-07 Install INOP placard on AC ESS FEED switch on Flight Deck Overhead ELEC panel OPERATIONAL (O) 24-20-07 DURING PRELIMINARY COCKPIT PREPARATION On the ELEC SD page, check that the AC BUS 1 supplies the AC ESS BUS.


N Registration

Page: 24.7


SUBJECT

24-27-01 IDG FAULT Lights

CAT

No INS

MIN REQ


C

2

1

One may be inoperative provided frequency and temperature indications are available on ECAM ELEC page, and are monitored.

PLACARD 24-27-01 Install INOP placard adjacent to applicable IDG switch on Flight Deck Overhead ELEC panel 35VU


N Registration

Page: 24.8


CAT

No INS

MIN REQ

1) FAULT Lights

C

3

1

2) OFF Lights

C

3

0

SUBJECT


24-27-02 GEN p.b. Switch One GEN and/or the APU FAULT Light may be inoperative provided the associated indications are avail able on ECAM ELEC page.

PLACARD 24-27-02 Install INOP placard adjacent to associated GEN switch (es) on Flight Deck Overhead ELEC panel 35VU


N Registration

Page: 24.9


SUBJECT

24-27-03 AC ESS FEED FAULT/ALTN Light

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS May be inoperative provided AC ESS bus indication is available ECAM ELEC page .

PLACARD 24-27-03 Install INOP placard adjacent to applicable light on Flight Deck Overhead ELEC panel 36VU


N Registration

Page: 24.10


CAT

No INS

MIN REQ


1) FAULT Light

C

1

0

(O) May be inoperative provided: a) AC load indication for each generator channel is available on ECAM ELEC page, and b) Automatic shedding operates normally.

2) OFF Light

C

1

0

SUBJECT

24-27-04 GALLEY/GALY&CAB p.b. Switch

PLACARD 24-27-04 Install INOP placard adjacent to galley switch on Flight Deck Overhead ELEC panel 35VU OPERATIONS (O) 24-27-04 On ground with electrical network supplied from APU or external power : GALY & CAB ...…………………………………...................CHECK AUTO C/B ELEC/GALLEY/GND/FLT/LOGIC (122VU S24)...………………………………………………..........PULL Check that a part of the operative galley equipment does not operate. C/B ELEC/GALLEY/GND/FLT/LOGIC (122VU S24).……………………………………………..............PUSH Note: Disregard this procedure if main galleys are not connected.


N Registration

Page: 24.11

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 24 ELECTRICAL POWER SUBJECT

CAT

No INS

24-27-05 RAT and EMER GEN FAULT Light

C

1

ITEM

MIN REQ

0

REMARKS OR EXCEPTIONS (O) May be inoperative provided indications are available on associated ECAM ELEC page.

PLACARD 24-27-05 Install INOP placard adjacent to lower ECAM Display OPERATIONS (O) 24-27-05 Verify RAT and EMER GENERATOR indications are available on ECAM. If RAT and EMER generator is required, monitor indications on ECAM display.


N Registration

Page: 24.12


CAT

No INS

24-27-06 Indications On ECAM ELEC Page

C

25

22

(O) Indications related to AC generation may be inoperative provided: a) Load, voltage and frequency indications of at least one engine driven generator operate normally, b) Associated GEN FAULT caution on ECAM operates normally, and c) Automatic shedding operates normally.

C

3

0

Except for ER operations, may be inoperative provided both Engine Driven Generators are operative.

ITEM

a) APU GEN Parameters

MIN REQ


PLACARD 24-27-06 Install INOP placard adjacent to lower ECAM Display OPERATIONS (O) 24-27-06 During cockpit preparation : Check that FAULT light of GEN 1(2) pb sw is ON (pb at ON position) On ground with electrical network supplied from APU or external power : GALLEY ……………………………………..................CHECK AUTO C/B ELEC/GALLEY/GND/FLT/LOGIC (122VU S24).……………………………………………...............PULL Check that a part of operative galley equipment does not operate. C/B ELEC/GALLEY/GND/FLT/LOGIC (122VU S24)..…………………………………………….............PUSH Note: Disregard this procedure if main galleys are not connected.


N Registration

Page: 24.13


SUBJECT

CAT

No INS

MIN REQ

C

1

0


24-27-09 COMMERCIAL p.b. Switch 1) OFF Light


N Registration

Page: 24.14


CAT

No INS

24-30-01 Transformer/ Rectifier Units (TR)

A

3

ITEM

MIN REQ

2

REMARKS OR EXCEPTIONS (O) Except for ER operations, TR1 may be inoperative provided: a) Extract fan operates normally, b) Battery voltage indicator operates normally, c) Both packs operate normally, and d) Repairs are made within two flight days. e) Approach minimums do not require its use.

1) Without Mod. 27620 2) With Mod. 27620

Not applicable to Avianca Fleet A

3

2

(M)(O) Except for ER operations, TR2 may be inoperative provided: a) Extract fan operates normally, b) Battery voltage indicator operates normally, c) Both packs operate normally, d) Repairs are made within two flight days, e) AC ESS FEED control is checked operative once each day, f) ISIS Horizon operates normally, g) Standby Compass operates normally, and h) Approach minimums do not require its use.

PLACARD 24-30-01 Install INOP placard adjacent to Electrical Power panel located on Flight Deck overhead panel OPERATIONS (O) 24-30-01 FLIGHT PREPARATION/LIMITATIONS Maximum landing capability is CAT 3 SINGLE. DURING PRELIMINARY COCKPIT PREPARATION TR 1/CNTOR/SPLY (125VU CF01) C/B.......................................................................................Pull On the ELEC SD page, disregard the indications related to the deactivated TR 1. On the ELEC SD page, check that the TR 2 and the ESS TR voltages are both equal to or above 27 V. The batteries must be set to OFF for the following check: On the battery voltage indicator, check that the BAT 1 and the BAT 2 voltages are both equal to or above 25.5 V.

(Continued)


N Registration

Page: 24.15


SUBJECT

CAT

No INS

MIN REQ


24-30-01 Transformer/ Rectifier Units (TR) (Continued) OPERATIONS (O) 24-30-01 2) FLIGHT PREPARATION/LIMITATIONS Maximum landing capability is CAT 3 SINGLE. DURING PRELIMINARY COCKPIT PREPARATION TR 2/CNTOR/SPLY (124VU BC01) C/B...................................................................................... Pull On the ELEC SD page, disregard the indications related to the deactivated TR 2. On the ELEC SD page, check that the TR 1and the ESS TR voltages are both equal to or above 27 V. The batteries must be set to OFF for the following check: On the battery voltage indicator, check that the BAT 1 and the BAT 2 voltages are both equal to or above 25.5 V. AC ESS FEED pb-sw................................................................................................................ALTN IN FLIGHT In the case of failure of the AC BUS 2, all DUs are lost. In this case: AC ESS FEED pb-sw..........................................................................................................Norm In the case of failure of the AC BUS 1: RAT MAN ON pb-sw (on HYD overhead panel)....................................................................Set MAINTENANCE (M) 24-30-09 Refer to Aircraft Maintenance Manual (AMM) Task Number 24-30-00-040-002.


N Registration

Page: 24.16


SUBJECT

24-30-04 Battery Volt-Meters

CAT

No INS

MIN REQ

C

2

0

REMARKS OR EXCEPTIONS (O) May be inoperative provided: a) Battery indications are available on ECAM, and b) Battery voltage is confirmed adequate before APU start.

PLACARD 24-30-04 Install INOP placard adjacent to appropriate Voltmeter on Flight Deck overhead ELEC panel 35 VU OPERATIONS (O) 24-30-04 -

Verify Voltage indication (s) available on ECAM. Confirm battery voltage is adequate before starting APU. Batteries select to off during this check.


N Registration

Page: 24.17


CAT

No INS

MIN REQ

1) FAULT Lights

C

2

0

2) OFF Lights

C

2

0

SUBJECT


24-30-05 BAT p.b. Switches

PLACARD 24-30-05 Install INOP placard adjacent to BAT FAULT light


N Registration

Page: 24.18


CAT

No INS

MIN REQ

1) DC TIE contactor 1 (DC BUS 1-DC BAT BUS)

C

1

0

May be inoperative open provided DC TIE contactor ESS operates normally.

2) DC TIE contactor ESS (DC BAT BUS- DC ESS BUS)

C

1

0

May be inoperative open provided DC TIE contactor 1 operates normally

SUBJECT


24-30-06 DC BUS TIE SYSTEM

PLACARD 24-30-06 Install INOP placard adjacent to lower ECAM Display


N Registration

Page: 24.19


SUBJECT

CAT

No INS

MIN REQ

C

1

0


24-30-07 BUS TIE p.b. Switch 1) OFF Light PLACARD 24-30-07 Install INOP placard adjacent to BUS TIE switch


N Registration

Page: 24.20


SUBJECT

24-30-08 ECAM ELEC Page (DC)

CAT

No INS

MIN REQ

C

10

0

REMARKS OR EXCEPTIONS Indications related to DC generation may be inoperative.

PLACARD 24-30-08 Install INOP placard adjacent to lower ECAM display


N Registration

Page: 24.21


CAT

No INS

24-30-09 External Power Panel ADIRU/AVNCS Vent Caution Light

C

1

ITEM

MIN REQ


0

(M) May be inoperative provided avionics ventilation system warning horn is verified to operate normally.

PLACARD 24-30-09 Install INOP placard adjacent to lower ECAM Display MAINTENANCE (M) 24-30-09 Refer to Aircraft Maintenance Manual (AMM) Task Number 21-26-00-040-012.


N Registration

Page: 24.22


CAT

No INS

MIN REQ

1) Ground Power Control Unit (GPCU) /Ground Power Control function of the Ground and Auxiliary Power Control unit (GAPCU)

C

1

0

2) Receptacle

C

SUBJECT


24-41-01 AC External Power Control May be inoperative provided external power is not used. NOTE: When GPCU/Ground Power Control Function of the GAPCU and APU generator are both inoperative, engines cannot be started. 1

0

(M) May be inoperative provided external power is not used. NOTE: When GPCU/Ground Power Control Function of the GAPCU and APU generator are both inoperative, engines cannot be started.

PLACARD 24-41-01 Install INOP placard adjacent to lower ECAM Display MAINTENACE (M) 24-41-01 Refer to Aircraft Maintenance Manual (AMM) Task Number 24-41-00-040-001


N Registration

Page: 24.23


SUBJECT

24-41-02 External Power NOT IN USE and AVAIL Panel Lights

CAT

No INS

MIN REQ

C

2

0

REMARKS OR EXCEPTIONS (O) May be inoperative provided alternate procedures are established and used.

PLACARD 24-41-02 Install INOP placard adjacent to lower ECAM Display OPERATIONS (O) 24-41-02 AVAIL Light Before pushback : Confirm the external power disconnection either on ECAM ELEC AC Page or with the ground mechanic. On parking : If APU is not available, set EXT PWR at ON and confirm the external power connection either on ECAM ELEC Page or with the ground mechanic before setting ENG MASTERS OFF.


N Registration

Page: 24.24


CAT

No INS

MIN REQ

1) AVAIL Light

C

1

0

2) ON Light

C

1

0

SUBJECT


24-41-03 EXT PWR Pb Switch (O) May be inoperative provided alternate procedures are established and used.

PLACARD 24-41-03 Install INOP placard adjacent to lower ECAM Display and Ext panel OPERATIONS (O) 24-41-03 AVAIL Light Before pushback : Confirm the external power disconnection either on ECAM ELEC AC Page or with the ground mechanic. On parking : If APU is not available, set EXT PWR at ON and confirm the external power connection either on ECAM ELEC Page or with the ground mechanic before setting ENG MASTERS OFF.


N Registration

Page: 24.25


SUBJECT

CAT

No INS

MIN REQ

C

1

0


24-50-01 Warning and Caution On ECAM E/WD 1) C/B TRIPPED

(M) May be inoperative provided alternate procedures are used to verify that no circuit breaker is tripped on associated C/B panel.

2) ELEC IDG 1(2) OIL LO LVL Alert (A319neo/A320 neo/A321neo with PW 1100G Engines)

Not Applicable to Avianca.

3) ELEC IDG 1(2) FILTER CLOG Alert (A319neo/ A320neo/A321neo with PW1100G Engines)


MAINTENANCE (M) 24-50-01 Refer to Aircraft Maintenance Manual (AMM) Task Number 24-50-00-040-001.


N Registration

Page: 24.26


CAT

No INS

MIN REQ


1) Automatic Load Shedding System

C

1

0

May be inoperative provided GALLEY/ GALY&CAB p.b. switch and GALLEY/GALY&CAB FAULT Light in the cockpit operate normally.

2) Automatic and Manual Load Shedding Systems

C

2

0

(M) May be inoperative provided all GALLEY/GALY&CAB loads are disconnected.

(With Mod 20343/MP P0473 or with Mod 31276/MP P7175)

C

2

0

(M)(O) May be inoperative provided that the COMMERCIAL supply system is checked operative.

3) COMMERCIAL Supply System (With Mod 20343/MP P0473 or with Mod 31276/MP P7175)

C

1

0

(O) May be inoperative.

SUBJECT

24-56-01 GALLEY/GALY&CAB and COMMERCIAL Supply Systems

PLACARD Install 24-56-01 INOP placard adjacent to ELEC Panel. OPERATIONAL (O) 24-56-01 2) ON GROUND OR IN FLIGHT If the AVNCS SMOKE emergency procedure is applied or if the AVIONICS SMOKE alert is displayed on the EWD replace the action to set the GALY & CAB pb-sw to OFF by the following actions: ‐ EMER EXIT LT selector....................................................................................................As required ‐ COMMERCIAL pb-sw.......................................................................................................OFF Note: When the COMMERCIAL pb-sw is set to OFF, the normal cabin lighting goes off. Minimum cabin lighting is recovered when the EMER EXIT LT selector is set to ON. OPERATIONAL (O) 24-56-01 3) ON GROUND OR IN FLIGHT If the AVNCS SMOKE emergency procedure is applied or if the AVIONICS SMOKE alert is displayed on the EWD replace the action to set the COMMERCIAL pb-sw to OFF by the following actions: (Continued) Revision: 29 October 23, 2014

N Registration

Page: 24.27


SUBJECT

CAT

No INS

MIN REQ


24-56-01 GALLEY/GALY&CAB and COMMERCIAL Supply Systems (Continued) OPERATIONAL (O) 24-56-01 3) (Continued) ‐ BUS TIE pb.......................................................................................................................OFF ‐ GEN 2 pb-sw....................................................................................................................OFF The F/O PFDU, the F/O NDU, and the ECAM lower display are lost. If the smoke persists: ‐ GEN 2 pb-sw......................................................................................................................On When the GEN 2 pb-sw is set to on, all the electrical busses are recovered but the TR 2 remains inoperative ‐ BUS TIE pb........................................................................................................................AUTO Before the landing gear extension: ‐ GEN 2 pb-sw......................................................................................................................On When the GEN 2 pb-sw is set to on, all the electrical busses are recovered but the TR 2 remains inoperative ‐ BUS TIE pb.........................................................................................................................AUTO MAINTENANCE (M) 24-56-01 2) First Proviso To Deactivation of the Galley Supply System refer to Aircraft Maintenance Manual (AMM) 24-56-00-040002. MAINTENANCE (M) 24-56-01 2) Second Proviso To Deactivation of the Galley Supply System Refer to Aircraft Maintenance Manual (AMM) 24-51-00-040001.


N Registration

Page: 24.28

Avianca AIRBUS A318/A319/A320/321 MINIMUM EQUIPMENT LIST ATA 25 EQUIPMENT/FURNISHING ITEM

CAT

No INS

MIN REQ

D

2

0

(M) May be inoperative provided: a) Horizontal and vertical mechanical adjustments operates normally, and b) Associated electrical control is deactivated

2) Primary Horizontal Mechanical Adjustment

2

2

Must be operative

3) Backup Horizontal Mechanical Adjustment

0

0

Not applicable. Applicable to aircraft with Backup Horizontal Mechanical Adjustment installed.

SUBJECT


25-11-01 Pilot Seat Adjustments 1) Electrical Adjustment

4) Vertical Mechanical Adjustment

C

2

0

May be inoperative provided vertical electrical adjustment operates normally.

5) Lumbar

C

2

0

May be inoperative provided seat contour is satisfactory to individual/crewmember requirements.

6) Recline Systems

A

2

0

(M) May be inoperative provided: a) Seat is secured in an upright position acceptable to the affected crewmember, and b) Repairs are made within two flight days.

MAINTENANCE (M) 25-11-01 1) Refer to AMM TASK 25-11-00-040-001 and TASK 25-11-00-040-002 MAINTENANCE (M) 25-11-01 6) Refer to AMM TASK 25-11-00-040-001 and TASK 25-11-00-040-001


N Registration

Page: 25.1


SUBJECT

25-11-02 Crewmember Shoulder Harness (Flight Deck)

1) Manual Shoulder Harness Locking Device

CAT

No INS

MIN REQ

D

4

2

Captain and First officer’s Shoulder Harness must be operative all time

D

4

3

One additional must be operative for use of the Civil Aviation Authority / Check Airman for performance of official duties.

A

4

3

(M) One may be inoperative provided: a) Inertial reel auto locking mechanism is verified to operate normally, and b) Repairs are made within three flight days.


Note: Captain and First officer’s Manual Shoulder Harness Locking Device must be operative all time

PLACARD Install 25-11-02 FAIL placard on associated crewmember’s glareshield. MAINTENANCE (M) 25-11-02 Check inertial reel auto locking mechanism for associated shoulder harness for proper operation.


N Registration

Page: 25.2


CAT

No INS

MIN REQ


C

2

0

May be inoperative provided setting is acceptable to crewmember(s).

2) Pitch Control (Tilt)

C

2

0

May be inoperative provided setting is acceptable to crewmember(s).

3) Armrest Memory Position Display

C

2

0

SUBJECT

25-11-03 CAPT and F/O Outboard Armrest Controls 1) Height Control


N Registration

Page: 25.3

Avianca AIRBUS A318/A319/A320/321 MINIMUM EQUIPMENT LIST ATA 25 EQUIPMENT/FURNISHING SUBJECT

CAT

No INS

25-11-04 CAPT and F/O Inboard Armrest Vertical Adjustment Controls

C

2

ITEM


MIN REQ

0

N Registration


Page: 25.4


CAT

No INS

25-11-05 Pilot SEAT Headrests

D

2

ITEM


MIN REQ

0

N Registration


Page: 25.5


SUBJECT

25-11-06 Primary Observer's Sliding Seat (Including associated equipment)

CAT

No INS

MIN REQ

A

1

0

May be inoperative provided: a) A passenger seat in the passenger cabin is made available to Civil Aviation Inspector for the performance of official duties, and b) Repairs are made within two flight days.

A

1

0

May be inoperative provided: a) Secondary observer's seat is available to Civil Aviation Inspector for performance of official duties, and b) Repairs are made within two flight days.

A

1

0

May be inoperative provided: a) Required minimum safety equipment (safety belt and oxygen) is available, b) Seat is acceptable to Civil Aviation Inspector for performance of official duties, and c) Repairs are made within two flight days.


NOTE 1: These provisos are intended to provide for occupancy of the above seats by Civil Aviation Inspector when the minimum safety equipment (oxygen and safety belt) is functional and the inspector determines the conditions to be acceptable. NOTE 2: The pilot-in-command will determine if the minimum safety equipment is functional for other persons authorized to occupy any observer seat(s).


N Registration

Page: 25.6


CAT

No INS

25-11-07 Additional Observer’s Fixed Seat (Including associated equipment)

D

1

ITEM

MIN REQ

0

REMARKS OR EXCEPTIONS (M) May be inoperative provided or removed:

NOTE: The pilot-in-command will determine if the minimum safety equipment is functional for other persons authorized to occupy any observer seat(s). MAINTENANCE (M) 25-11-07 Refer to Aircraft Maintenance Manual (AMM) Task Number 25-11-00-040-004


N Registration

Page: 25.7


CAT

No INS

MIN REQ

1) Sliding Tables

D

2

0

(M) May be inoperative in the stowed position, or removed.

2) Table Tilt Function

D

2

0

May be inoperative provided associated table can be stowed.

SUBJECT


25-13-01 CAPT and F/O Sliding Tables

3) Chart Clips

Deleted, REV 20. Refer to NEF

MAINTENANCE (M) 25-13-01 Refer to Aircraft Maintenance Manual (AMM) Task Number 25-13-00-040-001


N Registration

Page: 25.8


CAT

No INS

25-13-02 CAPT and F/O Retractable Footrests

D

4

ITEM

MIN REQ

0

REMARKS OR EXCEPTIONS (M) May be inoperative secured in the retracted position or removed.



N Registration

Page: 25.9


SUBJECT

25-15-01 Crew Foot Warmer


CAT

No INS

MIN REQ

D

2

0

N Registration


Page: 25.10


SUBJECT

25-21-01 Passenger Seat(s)

CAT

No INS

MIN REQ

D D D D D D

100 120 150 153 194 195

0 0 0 0 0 0

REMARKS OR EXCEPTIONS For A318 Fleet (12BC/88YC) For A319 Fleet (12BC/108YC) For A320 Fleet (12BC/138YC) For A320Neo Fleet (12BC/141YC) For A321 Fleet (12BC/182YC) For A321 Neo Fleet (12BC/183YC) May be inoperative provided: a) Seat does not block an Emergency Exit, b) Seat does not restrict any passenger from access to the main aircraft aisle, and c) Affected seat(s) are blocked and placarded "DO NOT OCCUPY". NOTE 1: A seat with an inoperative seat belt is considered inoperative. NOTE 2: Inoperative seats do not affect the required number of Flight Attendants. NOTE 3: Affected seat(s) may include the seat(s) behind and/or adjacent outboard seats.

1) Recline Mechanism

D D D D D D

90 114 138 141 186 180

0 0 0 0 0 0

For A318 Fleet (12BC/78YC) For A319 Fleet (12BC/102YC) For A320 Fleet (12BC/126YC) For A320Neo Fleet (12BC/129YC) For A321 Fleet (12BC/174YC) For A321 Neo Fleet (12BC/168YC) (M) May be inoperative and seat occupied provided seat is secured in the full up-right position.

D D D D D D

90 114 138 141 186 180

0 0 0 0 0 0

For A318 Fleet (12BC/78YC) For A319 Fleet (12BC/102YC) For A320 Fleet (12BC/126YC) For A320Neo Fleet (12BC/129YC) For A321 Fleet (12BC/174YC) For A321 Neo Fleet (12BC/168YC) May be inoperative and seat occupied provided seat back is immovable in full upright position.

(Continued)


N Registration

Page: 25.11


SUBJECT

CAT

No INS

MIN REQ

C C C C C C

36 42 52 53 68 68

0 0 0 0 0 0


25-21-01 Passenger Seat(s) (Continued) 2) Underseat Baggage Restraining Bars

For A318 Fleet For A319 Fleet For A320 Fleet For A320Neo Fleet For A321 Fleet For A321 Neo Fleet (O) May be inoperative provided: a) Baggage is not stowed under seat with inoperative restraining bar, b) Associated seat is placarded "DO NOT STOW BAGGAGE UNDER THIS SEAT", and c) Procedures are established to alert Cabin Crew of inoperative restraining bar.

3) Armrests a)Armrest with recline mechanism

D D D D D D

90 114 138 141 186 180

0 0 0 0 0 0

For A318 Fleet (12BC/78YC) For A319 Fleet (12BC/102YC) For A320 Fleet (12BC/126YC) For A320Neo Fleet (12BC/129YC) For A321 Fleet (12BC/174YC) For A321 Neo Fleet (12BC/168YC) (M) May be inoperative or missing and seat occupied provided: a) Armrest does not block an Emergency Exit, b) Armrest does not restrict any passenger from access to the main aircraft aisle, and c) If armrest is missing, seat is secured in the full upright position.

b)Armrest without recline mechanism

D D D D D D

10 6 12 12 8 15

0 0 0 0 0 0

For A318 Fleet For A319 Fleet For A320 Fleet For A320Neo Fleet For A321 Fleet For A321 Neo Fleet May be inoperative or missing and seat occupied provided: a) Armrest does not block an Emergency Exit, and b) Armrest does not restrict any passenger from access to the main aircraft aisle.


N Registration

Page: 25.12


SUBJECT

CAT

No INS

MIN REQ

D D D D D D

100 120 150 153 194 195

0 0 0 0 0 0


25-21-01 Passenger Seat(s) (Continued) 4) Mechanical Functions (Tracking/Swivel, Headrest/Footrest)

For A318 Fleet (12BC/88YC) For A319 Fleet (12BC/108YC) For A320 Fleet (12BC/138YC) For A320Neo Fleet (12BC/141YC) For A321 Fleet (12BC/182YC) For A321 Neo Fleet (12BC/183YC) May be inoperative and seat occupied provided: a) Seat does not block an Emergency Exit, b) Seat does not restrict any passenger from access to the main aircraft aisle, and c) Seat is secured in the takeoff/landing position

OPERATIONS (O) 25-21-01 -2) Advise and Brief the cabin crew to ensure baggage is not stowed under seats with inoperative or missing restraining Bars. Before each departure receive a positive confirmation by the cabin crew that baggage is not stowed under seats with inoperative or missing restraining Bars. Advise cabin crew to inform passengers occupying seat with affected bar and passenger behind the seat with the affected bar not to stow baggage under the seat MAINTENANCE (M) 25-21-01 –1) Deactivate the recline mechanism cable, put an inoperative label and notify to the flight attendants MAINTENANCE (M) 25-21-01 –3)a) For an inoperative armrest with recline mechanism, seat must be secured in the full upright position.


N Registration

Page: 25.13


SUBJECT

CAT

No INS

MIN REQ

C C

4 5

0 0

C

6

0

C

8

0


25-22-01 Flight Attendant Seat Assembly (single or dual position) Applicable to all A318 and A320Neo Applicable to N422AV, N519AV, N557AV, N647AV and N691AV. Applicable to all A320Ceo fleet, N690AV, N694AV, N695AV, N723AV, N726AV, N730AV, N741AV, N751AV and N753AV. Applicable to all A321 Fleet. (O) May be inoperative or missing provided: a) No passengers are carried, b) A maximum of 19 persons authorized in accordance with Equipment relief without passengers definition (refer to definitions section of this MEL) for non-passenger carrying operations are carried, and c) Alternate procedures are established and used. 1) Required Flight Attendant Seats

B B

3 4

2 3

For A318 and A319 Fleet For A320 and A321 Fleet (M)(O)One seat position or assembly (dual position) may be inoperative provided: a) Affected seat position or seat assembly is not occupied, b) Flight Attendant(s) displaced by inoperative seat(s) occupies either an adjacent flight attendant seat or the passenger seat which is most accessible to the inoperative seat(s), so as to most effectively perform assigned duties, c) Alternate procedures are established and used as published in crewmember manuals, d) Folding type seat stows automatically or is secured in the retracted position, and e) Passenger seat assigned to flight attendant is placarded "FOR FLIGHT ATTENDANT USE ONLY". NOTE 1: An automatic folding seat that will not stow automatically is considered inoperative. NOTE 2: A seat position with an inoperative or missing restraint system is considered inoperative.

(Continued)


N Registration

Page: 25.14


SUBJECT

CAT

No INS

MIN REQ


25-22-01 Flight Attendant Seat Assembly (single or dual position) (Continued) NOTE 3: Individual operators, when operating with inoperative seats, will consider the locations and combinations of seats to ensure that the proximity to exits and distribution requirements of the applicable FAR (FAR 25.785) and RAC are met. NOTE 4: If one side of a dual seat assembly is inoperative and a flight attendant is displaced to the adjacent seat, the adjacent seat must operate normally. 2) Excess Flight Attendant Seats

C

1

0

Applicable to all A318 fleet.

C

2

0

Applicable to all A320 Ceo fleet N422AV, N519AV, N557AV, N647AV and N691AV.

C

3

0

Applicable to N690AV, N694AV, N695AV, N723AV, N726AV, N730AV, N741AV, N751AV and N753AV.

C

4

0

Applicable to all A321 Fleet. (M) May be inoperative provided: a) Affected seat position or seat assembly is not occupied, and b) Folding type seat stows automatically or is secured in the retracted position. NOTE 1:An automatic folding seat that will not stow automatically is considered inoperative. NOTE 2: A seat position with an inoperative or missing restraint system is considered inoperative.

3) All Cargo Configuration

Not applicable to Avianca Fleet. Avianca fleet does not have cargo configuration aircraft.

4) Without Passengers

Not applicable to Avianca fleet. Avianca is an operator under FAR 129.

OPERATIONS (O) 25-22-01 1. No passengers may be carried. 2. A maximum of 19 persons authorized in accordance with Equipment relief without passengers definition (refer to definitions section of this MEL) may be carried. (Continued) Revision: 36 June 30, 2017

N Registration

Page: 25.15


SUBJECT

CAT

No INS

MIN REQ


25-22-01 Flight Attendant Seat Assembly (single or dual position) (Continued) 3. Captain will brief the first attendant as follow: Before takeoff, the first attendant shall ensure direct voice communication with the persons on board to provide a safety briefing about: a) No smoking during entire flight. b) The use of seat belts c) The location and operation of emergency exits, and d) For extended overwater operations, the location and operation of life preservers including a demonstration of the method of donning and inflating a life preserver. OPERATIONS (O) 25-22-01 1) Ensure affected seat(s) are stowed and secured in retracted position. The flight attendant(s) displaced by the inoperative seat(s) must occupy an adjacent F/A seat or the pax seat which is most accessible to their assigned exit(s). In this case, the pax seat must be placarded “FOR FLIGHT ATTENDANT USE ONLY”. Notify to MCC and/or Operations Dispatch Department. MAINTENANCE (M) 25-22-01 1. 2. 3. 4.

The inoperative seat must be secured in the retracted (stowed position or removed). Placard the seat (if not removed) “INOPERATIVE” If removed notify dispatch for Weight and Balance adjustments. The passenger seat assigned to the cabin attendant(s) must be the seat most accessible to the nearest exists and placarded “FOR FLIGHT ATTENDANT USE ONLY”


N Registration

Page: 25.16


SUBJECT

25-22-03 Non-essential Equipment & Furnishings (NEF)

CAT

No INS

MIN REQ


0

May be inoperative, damaged or missing provided that the item(s) is deferred in accordance with the Avianca A318/A319/A320/A321 NEF deferral program. The NEF program, procedures and processes are outlined in the Avianca A318/A319/A320/A321 NEF Manual. (M) and (O) procedures where is required, are available to the flight crew and maintenance staff in Avianca NEF Program Manual. NOTE: Exterior lavatory door ash trays are not considered NEF items.


N Registration

Page: 25.17


SUBJECT

CAT

No INS

MIN REQ


25-22-04 Exterior Lavatory Door Ashtrays 1) Airplanes with more than one exterior lavatory door ashtray installed 2) Airplanes with only one exterior lavatory door ashtray installed


Not applicable to Avianca. Avianca fleet has one Exterior Lavatory Door Ashtrays installed. A

1

0

May be missing or inoperative for 10 days.

N Registration

Page: 25.18


SUBJECT

25-27-01 Heating Function of Heated Floor Panels (Passenger/Crew Doors, Emergency Exits, and Galley Areas)

CAT

No INS

MIN REQ

D

4

0

REMARKS OR EXCEPTIONS (M) May be inoperative provided the heating elements of the affected heated floor panel are deactivated.

MAINTENANCE (M) 25-27-01 Deactivate the Heated Floor Panel by pulling the circuit breakers “1DS” ( Door 2 ) or “11DS” ( Door 3) as applicable.


N Registration

Page: 25.19


CAT

No INS

25-28-01 Storage Bin(s)/ Cabin, Galley, and Lavatory Storage Compartment/Closets

C

26

9

C

34

9

C

24

9

ITEM

MIN REQ

REMARKS OR EXCEPTIONS For A320 fleet (Minimum qty required is where is located Emergency Equipment (EE)). For A321 fleet (Minimum qty required is where is located Emergency Equipment (EE)). For A318 and A319 fleet (Minimum qty required is where is located Emergency Equipment (EE)). (M) May be inoperative provided: a) Procedures are established to secure compartment CLOSED b) Associated bin or compartment is prominently placarded DO NOT USE, c) Any emergency equipment located in affected compartment is considered inoperative, and d) Affected compartment is not used for storage of any item(s) except for those permanently affixed. NOTE: For overhead storage compartments, if no partitions are installed, the entire overhead storage compartment is considered one compartment.

C

26

9

C

34

9

C

24

9

For A320 fleet (Minimum qty required is where is located Emergency Equipment (EE)). For A321 fleet (Minimum qty required is where is located Emergency Equipment (EE)). For A318 and A319 fleet (Minimum qty required is where is located Emergency Equipment (EE)). (M) (O) May be inoperative provided: a) Affected door(s) is (are) removed or, for retractable doors, secured in the retracted (fully open) position, b) Associated bin or compartment is not used for storage of any items, except those permanently affixed, c) Associated bin or compartment is prominently placarded DO NOT USE, d) Procedures are established and used to alert crew members and passengers of inoperative bins, and e) Passengers are briefed that associated bin or compartment is not used. NOTE 1: For overhead storage compartments, if no partitions are installed, the entire overhead storage compartment is considered one compartment. (Continued)


N Registration

Page: 25.20


SUBJECT

CAT

No INS

MIN REQ


25-28-01 Overhead Storage Bin(s)/ Cabin and Galley Storage Compartment/Closets (Continued) NOTE 2: Any emergency equipment located in the associated compartment (permanently affixed) is available for use. 1) Storage Compartment Key Locks

D D D

63 68 57

0 0 0

For A320 fleet. For A321 fleet. For A318 and A319 fleet. (M) May be inoperative in the unlocked position provided doors can be secured by other means.

2) Multi Latch/ Quarter Turn Lug Installations Compartment Locks

C

44

40

One latch per compartment may be inoperative provided: a) Remaining latch(es)/lug(s) on affected compartment(s) operate normally, and b) If affected compartment is used for a galley cart, the cart remains empty.

0

0

Not installed on Avianca fleet.

3) Mid-Latch Locking Assembly OPERATIONS (O) 25-28-01

Crew must check that associated bin or compartment is not used for storage of any items, except those permanently affixed. Advise passengers do not use associated bins. MAINTENANCE (M) 25-28-01 and 1) Maintenance must advise passenger service and operations departments for carry on baggage restrictions, before boarding. Install INOP placard and secure the affected compartment in closed position by using tape around the door. Refer to AMM TASK TASK 25-20-00-040-001


N Registration

Page: 25.21

Avianca AIRBUS A318/A319/A320/321 MINIMUM EQUIPMENT LIST ATA 25 EQUIPMENT/FURNISHING ITEM 25-40-01

SUBJECT Lavatory Waste Receptacle Access Doors/Covers/Flapper/ Doors

CAT

No INS

C

3

MIN REQ

2

REMARKS OR EXCEPTIONS (M) May be inoperative provided: a) Associated waste container is empty, b) Affected receptacle access doors/covers/flapper door is secured to prevent waste introduction into the receptacle, c) Lavatory is used only by crewmembers, and d) Associated lavatory entrance door is locked closed and placarded, INOPERATIVE - DO NOT ENTER. NOTE: These provisios are not intended to prohibit lavatory use or inspections by crewmembers.

MAINTENANCE (M) 25-40-01 Refer to AMM TASK 25-40-00-040-001


N Registration

Page: 25.22


SUBJECT

25-45-01 Galley/ Cabin Waste Receptacles Access Doors/Covers

CAT

No INS

MIN REQ


C

3

1

(M)(O) May be inoperative provided: a) The container is empty and the access is secured to prevent waste introduction into the compartment, and b) Procedures are established to ensure that sufficient galley/ cabin waste receptacles are available to accommodate all waste that may be generated on a flight.

OPERATIONS (O) 25-45-01 -

The container is empty and the access is secured with tape only to prevent waste introduction into the compartment. Remaining containers must be capable to handle the waste.

MAINTENANCE (M) 25-45-01 -

Empty galley waste container, secure access door in close position and placard “DO NOT USE”. Advise the flight crew and attendants.


N Registration

Page: 25.23


SUBJECT

25-50-01 Cargo Loading System

CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable to Avianca. Avianca Fleet does not have this system installed

-


N Registration

Page: 25.24


SUBJECT

25-50-02 Blow In/Out Panels in Cargo Compartment FWD Cargo Compartment AFT and Bulk Cargo compartment

CAT

No INS

MIN REQ

C C C

7 10 6

0 0 0

Applicable to A320 Fleet Applicable to A321 Fleet Applicable to A318 and A319 Fleet

C C C

12 15 10

0 0 0

Applicable to A320 Fleet Applicable to A321 Fleet Applicable to A318 and A319 Fleet


(O) May be damaged or missing provided procedures are established and used to ensure the associated compartment remains empty, or is verified to contain only empty cargo handling equipment, ballast, (ballast may be loaded in ULDs), and/or Fly Away Kits ((K.O.B) Kit on Board). NOTE: The materials used as ballast or Fly Away Kits (K.O.B) Must not be those considered as Dangerous Materials. Refer to Avianca´s Dangerous Goods Manual. OPERATIONS (O) 25-50-02 May be damaged or missing and ensure the associated compartment remains empty. Prior to each flight pilot must confirm with Ramp that the only items allowed to be carried is the Fly Away Kit (K.O.B), empty cargo handling equipment or ballast. If ballast is needed those materials must not to be considered as dangerous materials. Refer to Avianca´s Dangerous Goods Manual.


N Registration

Page: 25.25


SUBJECT

25-50-03 Cargo Compartment Sidewall Lining and Ceiling Panels

CAT

No INS

MIN REQ

C C C

52 88 124

0 0 0

REMARKS OR EXCEPTIONS For A318 and A319 Fleet For A320 Fleet Applicable to A321 Fleet (O) May be damaged or missing provided procedures are established and used to ensure the associated compartment remains empty or is verified to contain only empty cargo handling equipment, ballast,(ballast may be loaded in ULDs), and/or Fly Away Kits. NOTE: The materials used as ballast or Fly Away Kits (K.O.B) Must not be those considered as Dangerous Materials. Refer to Avianca´s Dangerous Goods Manual.

OPERATIONS (O) 25-50-03 Notify dispatch. Prior to each flight pilot must confirm with the ground personnel that only ballast or the Fly Away Kit (K.O.B) is allowed to be carried on the aircraft and those items must not be considered as dangerous materials. Refer to Avianca’s Dangerous Goods Manual If K.O.B (Kit On Board) or ballast is not carried in this compartment, it must be empty


N Registration

Page: 25.26


SUBJECT

25-50-04 Cargo Restraint System (Nets, Attach Points, Stanchions, etc) FWD Cargo Compartment

AFT Cargo Compartment


CAT

No INS

MIN REQ


A

1

0

(M) Divider Net, may be inoperative, damage or missing provided: a. FWD cargo compartment is fully loaded, and b. Approved cargo loading limits (Weight and Balance documents) are observed. c. Repairs are made prior to the completion of the next heavy maintenance visit.

A

3

0

(M) Door Net, May be inoperative, damage or missing provided: a. Divider Net is installed, and b. Luggage is not accommodated after divider Net (behind door nets), and c. Approved cargo loading limits (Weight and Balance documents) are observed. d. Repairs are made prior to the completion of the next heavy maintenance visit.

C

4

0

(O) All Nets (Divider and Doors nets) May be inoperative or missing provided associated cargo compartment remains empty or is check to contain only empty cargo handling equipment, ballast (ballast may be loaded in ULDs), and/or Fly Away Kits.

A

2

0

(M) Divider Net, may be inoperative, damage or missing provided: a. AFT cargo compartment is fully loaded, and b. Approved cargo loading limits (Weight and Balance documents) are observed. c. Repairs are made prior to the completion of the next heavy maintenance visit.

A

4

0

(M) Door Net, may be inoperative, damage or missing provided: a. Divider Net is installed, and b. Luggage is not accommodated after divider Net (behind door nets), and c. Approved cargo loading limits (Weight and Balance documents) are observed. d. Repairs are made prior to the completion of the next heavy maintenance visit.

C

6

0

(O) All Nets (Divider and Doors nets) May be inoperative or missing provided associated cargo compartment remains empty or is check to contain only empty cargo handling equipment, ballast (ballast may be loaded in ULDs), and/or Fly Away Kits. (Continued)

N Registration

Page: 25.27


SUBJECT

CAT

No INS

MIN REQ

C C

3 7

0 0


25-50-04 Cargo Restraint System (Nets, Attach Points, Stanchions, etc) (Continued) Bulk Cargo Compartment

For A319 and A320 For A321 (O) May be inoperative or missing provided associated cargo compartment remains empty or is check to contain only empty cargo handling equipment, ballast (ballast may be loaded in ULDs), and/or Fly Away Kits.

OPERATIONS (O) 25-50-04 Notify Dispatch Ramp personnel must be advice with instructions given by dispatch center in order to keep in mind that the associated cargo compartment has some weight and balance distribution penalties. See Weight and Balance Manual. MAINTENANCE (M) 25-50-04 Refer to AMM Task 25-50-00-210-050 or refer to AMM T Subtask 25-50-00-300-001 for reparation or Refer to AMM Task 25-52-00 PB 001 for restrictions


N Registration

Page: 25.28


SUBJECT

25-50-05 Protection Panel of Decompression Panels at the FWD partition wall of FWD Cargo Compartment

CAT

No INS

MIN REQ


C

2

0

(M) One or more may be damaged provided: a) The affected protection panel is removed if the damage prevents correct operation of the decompression panel, and b) Bulk loading is not permitted in the section between the affected protection panel and the closest divider net. NOTE: Tied down cargo is not considered as bulk loading

MAINTENANCE (M) 25-50-05 Refer to Aircraft Maintenance Manual (AMM) Task Card 25-54-00-040-801


N Registration

Page: 25.29


SUBJECT

25-60-01 Evacuation Alarm Signaling System (EVAC COMMAND)

CAT

No INS

MIN REQ

C

1

0

(O) May be inoperative provided alternate procedures are established and used (See operational procedure).

D

1

0

May be inoperative provided operations do not require its use.


OPERATIONS (O) 25-60-01 Advise all crew member each flight in order to keep in mind this situation in every brief meeting The information will be given through Public Address or Cabin interphone


N Registration

Page: 25.30


SUBJECT

25-60-03 SLIDE ARMED Light Systems

CAT

No INS

MIN REQ

C C

8 6

0 0

REMARKS OR EXCEPTIONS For A321 Only For A318/A319/A320 Only (O) May be inoperative provided alternate procedures are established and used.

OPERATIONS (O) 25-60-03 Verify slides are armed on ECAM door/oxy page, before each departure. Crew must advise the Flight attendant to verify the affected door(s) is/are closed and slide armed


N Registration

Page: 25.31


SUBJECT

CAT

No INS

MIN REQ

B B

4 8

0 0


25-60-04 SLIDE Indications on ECAM DOOR/OXY Page 1) Passenger Doors a) Armed Indication

For A318, A319 and A320 fleet. For A321 (O) May be inoperative provided alternate procedures are established and used

b) Not armed Indication

C C

4 8

0 0

For A318, A319 and A320 fleet. For A321 (M)(O )May be inoperative provided: a) Alternate procedures are established and used, and b) Aircraft is not operated at night.

2) Overwing Emergency Exit(s) (A318/A319/A320) a) Armed Indication

B

2

0

(M) May be inoperative provided a visual check is made to verify that slide(s) is armed.

b) Not armed Indication

C

2

0

(M) May be inoperative provided: a) Visual check is made that slide(s) is armed, and b) Aircraft is not operated at night.


After door closure, the Flight attendant have to verify the affected passenger door slide (s) is/are armed Upon arrival the flight attendance have to verify the affected door slide(s) is/are disarmed.

MAINTENANCE (M) 25-60-04 –1)b) Refer to Aircraft Maintenance Manual (AMM) Task Number 52-70-00-040-007 MAINTENANCE (M) 25-60-04 –2)a) Refer to Aircraft Maintenance Manual (AMM) Task Number 52-70-00-040-008 MAINTENANCE (M) 25-60-04 –2) b) Refer to Aircraft Maintenance Manual (AMM) Task Number 52-70-00-040-009


N Registration

Page: 25.32


SUBJECT

25-60-05 Slide Bottle Pressure Indication (On PTP/FAP)

CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Moved to item 23-73-07 2) for aircraft without mod. 30354 or without Mod. 33100 or item 2373-08 6) for aircraft with mod. 30354 or with Mod. 33100. Note 1: A319, A320 and A321 aircrafts has incorporated mod 33100. Note 2: A318 aircrafts has incorporated mod 30354.


N Registration

Page: 25.33


SUBJECT

25-60-06 CABIN PRESSURE Light Systems


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Moved to Item 52-70-02.

N Registration

Page: 25.34


SUBJECT

25-60-07 "Fasten Seat Belts While Seated" Signs or Placards

CAT

No INS

MIN REQ

C C C C C

36 42 52 53 68

18 21 26 27 34

For A318 Fleet – Signs-light. For A319 Fleet – Signs-light. For A320 Ceo Fleet – Signs-light. For A320 Neo Fleet - Signs-light. For A321 Fleet – Signs-light.

C

100

50

For A318 Fleet – (Placards) Text engraved on each seat rear meal table or backrest.

C

120

60

For A319 Fleet – (Placards) Text engraved on each seat rear meal table or backrest.

C

150

75

For A320Ceo Fleet – (Placards) Text engraved on each seat rear meal table or backrest.

C

153

78

For A320Neo Fleet (Placards) Text engraved on each seat rear meal table or backrest.

C

194

97

For A321Ceo Fleet – (Placards) Text engraved on each seat rear meal table or backrest.

C

195

98

For A321Neo Fleet – (Placards) Text engraved on each seat rear meal table or backrest


One or more may be illegible or missing provided a legible sign or placard is visible from each occupied passenger seat.


N Registration

Page: 25.35


CAT

No INS

25-60-08 Flashlight And Holders (Flight Deck or Cabin)

C C C C

8 10 7 6

ITEM

MIN REQ

0 0 0 0

REMARKS OR EXCEPTIONS For A320 Ceo Fleet For A321 Fleet. For A319 Fleet For A318 and A320 Neo Fleet. (O) May be inoperative or missing provided: a) No passengers are carried, b) A maximum of 19 persons authorized in accordance with Equipment relief without passengers definition (refer to definitions section of this MEL) for non-passenger carrying operations are carried, and c) Alternate procedures are established and used.

C C C C

8 10 7 6

6 8 5 5

For A320 Ceo Fleet. For A321 Fleet. For A319 Fleet For A318 and A320Neo Fleet. May be inoperative or missing provided crewmember assigned to associated seat has a flashlight with equivalent characteristics readily available.

OPERATIONS (O) 25-60-08 1. No passengers may be carried. 2. A maximum of 19 persons authorized in accordance with Equipment relief without passengers definition (refer to definitions section of this MEL) may be carried. 3. Captain will brief the first attendant as follow: Before takeoff, the first attendant shall ensure direct voice communication with the persons on board to provide a safety briefing about: a) No smoking during entire flight. b) The use of seat belts c) The location and operation of emergency exits, and d) For extended overwater operations, the location and operation of life preservers including a demonstration of the method of donning and inflating a life preserver.


N Registration

Page: 25.36


CAT

No INS

MIN REQ

C

2

0

(O) May be inoperative or missing provided: a) No passengers are carried, b) A maximum of 19 persons authorized in accordance with Equipment relief without passengers definition (refer to definitions section of this MEL) for non-passenger carrying operations are carried, and c) Alternate procedures are established and used.

1) Passenger Configuration

2

2

All must be operative, no extra equipment installed on the airplanes.

2) Cargo Configuration

0

0

Not applicable to Avianca. Avianca fleet does not have cargo configuration aircraft

SUBJECT

25-60-09 Megaphones


OPERATIONS (O) 25-60-09 1. No passengers may be carried. 2. A maximum of 19 persons authorized in accordance with Equipment relief without passengers definition (refer to definitions section of this MEL) may be carried. 3. Captain will brief the first attendant as follow: Before takeoff, the first attendant shall ensure direct voice communication with the persons on board to provide a safety briefing about: a) No smoking during entire flight. b) The use of seat belts c) The location and operation of emergency exits, and d) For extended overwater operations, the location and operation of life preservers including a demonstration of the method of donning and inflating a life preserver.


N Registration

Page: 25.37


SUBJECT

25-60-10 Emergency Locator Beacon


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Moved to 25-61-01, Ref ATA Spec 2200, MMEL REV 21.

N Registration

Page: 25.38


CAT

No INS

25-60-11 Slide Raft Lanyards (White and/or Yellow)

D

8

ITEM

MIN REQ


6

Applicable to A319, A320 and A321 aircraft only. (O) May be missing or damaged beyond serviceable. NOTE: Two lanyards are installed by slide raft, therefore it is permissible to have one or two lanyards missing or damaged in a slide raft while the opposite slide raft has both lanyards in good condition.

OPERATIONS (O) 25-60-11 Notify dispatch Aircraft can not be operated on extended overwater flights


N Registration

Page: 25.39


SUBJECT

25-60-12 Overwater Survival Kits


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Incorporated into 25-60-17.

N Registration

Page: 25.40


CAT

No INS

MIN REQ


1) Automated External Defibrillator (AED) and/or Associated Equipment

A

1

0

(O) May be incomplete, missing or inoperative provided: a) AED is resealed in a manner that will identify it as a unit that can not be mistaken for a fully serviceable unit, and b) Repairs or replacements are made within 1 flight cycles. Note: The AED contains two bags of pads, at least one must be serviceable in order to consider the AED operative.

2) Emergency Medical Kit and/or Associated Equipment

A A

2 1

1 1

Applicable to A319, A320 and A321 aircraft only. Applicable to A318 aircraft only.

SUBJECT

25-60-13 Emergency Medical Equipment

(O) May be incomplete, missing or inoperative provided: a) EMK is resealed in a manner that will identify it as a unit that cannot be mistaken for a fully serviceable unit, and b) Repairs or replacements are made within 1 flight cycles. 3) First Aid Kits and/or Associated Equipment

A A

2 3

1 2

Applicable to A318, A319 and A320 Applicable to A321 (O) Only one of the required first aid kits may be incomplete, missing or inoperative provided: a) FAK is resealed in a manner that will identify it as a unit that can not be mistaken for a fully serviceable unit, and b) Repairs or replacements are made within 1 flight cycles.

a) FAK in Excess

D

1

0

Applicable to A318, A319,A320 and A321 (O) FAK in excess may be incomplete, missing or inoperative. NOTE: The FAK in excess is an additional unit of those required by regulations (FAR/RAC) those units are included into equipment diagram. Used the item 25-60-13 3) when the first unit (FAK) is inoperative, for more than one refer to item 25-60-13 3) a)

OPERATIONAL 25-60-13 1) Report the Automated External Defibrillator (AED) condition in to the Deferred Maintenance Log. Brief all assigned crew members, prior to each flight that the EMK is not complete, is missing or is inoperative. OPERATIONAL 25-60-13 2) and 3) and 3)a) See the attached list on the EMK/FAK for more details about medicines and quantities may be incomplete. Revision: 34 May 26, 2016

N Registration

Page: 25.41


SUBJECT

CAT

No INS

MIN REQ

D D

4 2

2 1


25-60-14 Escape Life Lines 1) Overwing (A318/A319/A320)

For A320 Fleet For A319 and A318 Fleet May be damaged or missing provided aircraft is not operated on extended overwater flights.

2) Flight Deck Escape Life Line Cover Plates


C

2

0

May be damaged or missing.

N Registration

Page: 25.42


SUBJECT

25-60-15 Emergency Vision Assurance Systems (EVAS) (A319/A320/A321) (Vision Safe STC #SA00892LA)


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable to Avianca. Avianca fleet does not have installed this system.

N Registration

Page: 25.43


SUBJECT

CAT

No INS

MIN REQ


25-60-16 Flotation Equipment (Crew and Passenger) a) Life Vest

D D D D D D

D

118 108 (M) For A318 Fleet. 10 spare life vests are installed in OHSC aft box. Refer to Emergency Equipment Diagram. 139 129 (M) For A319 Fleet. 10 spare life vests are installed in OHSC aft box. Refer to Emergency Equipment Diagram. 170 160 (M) For A320 Ceo Fleet. 10 spare life vests are installed in OHSC aft box. Refer to Emergency Equipment Diagram. 171 170 (M) For A320 Neo Fleet. 10 spare life vests are installed in OHSC aft box. Refer to Emergency Equipment Diagram. 216 206 (M) For A321Ceo Fleet. 10 spare life vests are installed in OHSC aft box. Refer to Emergency Equipment Diagram. 217 207 (M) For A321 Neo Fleet. 10 spare life vests are installed in OHSC aft box. Refer to Emergency Equipment Diagram. 10

5

(M) 10 life vest for infants are installed in OHSC FWD box. Refer to Emergency Equipment Diagram. NOTE 1: In case that a crew life vest (red color) is found missing or damage during preflight in a base different to Bogotá, it is possible to use a spare life vest for passenger (yellow color) while it is replaced immediately arrives to Bogotá base. NOTE 2: all live vests can be missing if overwater operations are not conducted.

b) Life Raft

D

3

0

Applicable to A318 aircraft only. (O) May be incomplete, missing, or inoperative provided aircraft is not operated on extended overwater flights.

MAINTENANCE (M) 25-60-16 If any spare life vest or life vest for infant is found missing or used, report it in the Aircraft log book. OPERATIONAL (O) 25-60-16 Notify dispatch. Aircraft cannot be operated on extended overwater flights.


N Registration

Page: 25.44


SUBJECT

CAT

25-60-17 Survival Kit D

No INS

MIN REQ

4

4

Applicable to A321, A320 and A319 fleet.

3

0

Applicable to A318 fleet only. May be incomplete, missing, or inoperative provided aircraft is not operated on extended overwater flights


Note 1: In accordance with FAR 91.509 and RAC 4.2.5.3 a survival kit, appropriately equipped for the route to be flown, must be attached to each required life raft. Note 2: FAR and RAC requirements are already included herein.


N Registration

Page: 25.45


SUBJECT

25-60-18 Crash Axe/Crow Bar


CAT

No INS

MIN REQ

1

1

REMARKS OR EXCEPTIONS Must be operative.

N Registration

Page: 25.46


SUBJECT

CAT

No INS

MIN REQ

D

1

0


25-61-01 Emergency Locator Transmitter a) Survival Type ELTs

Except for over water operations beyond 30 minutes or 100 nautical miles. Notify Dispatch

b) Fixed ELTs

A

1

0

Except for over water operations beyond 30 minutes or 100 nautical miles. (M) May be inoperative provided: a) System is deactivated, b) The aircraft may be dispatched on a flight or series of flights until next arrival to BOG where repair must be accomplished prior to dispatch, and c) Survival ELT is operative. Notify Dispatch

A

1

0

Except for over water operations beyond 30 minutes or 100 nautical miles. a) The aircraft may be dispatched on a flight or series of flights until next arrival to BOG where repair must be accomplished prior to dispatch b) Survival ELT is operative. Notify Dispatch Note: In Accordance with RAC 4.2.2.4 and 4.19.7.3 for over water operations beyond 30 minutes or 100 nautical miles both ELT must be operative.

MAINTNANCE (M) 25-61-01 Get access to the ELT. Remove the ceiling panel 261BC (Refer to AMM TASK 25-23-42-000-002) Set the ARM/OFF/TX switch (11) to the OFF position. (Ref. Fig. 401/TASK 25-65-35-991-001 SHEET 401.1)


N Registration

Page: 25.47


SUBJECT

25-61-02 Passenger or Over Wing Door Slide/Slide Rafts (Without Passengers)

CAT

No INS

MIN REQ

C C

6 8

1 1

REMARKS OR EXCEPTIONS Applicable to A318, A319 and A320 Fleet Applicable to A321 Fleet (M)(O) May be inoperative or missing provided: a) No passengers are carried, b) A maximum of 19 persons authorized in accordance with Equipment relief without passengers definition (refer to definitions section of this MEL) for non-passenger carrying operations are carried, and c) Each person has unobstructed access from their seat to an operative exit, either regular or emergency, d) Inoperative exits are conspicuously identified as inoperative, e) An Emergency Exit sign and floor proximity lights associated only with the inoperative exits are covered to obscure the sign and lights, f) Safety briefing includes the location of the inoperative exit(s) and instructions not t use the inoperative exit(s), and g) Alternate procedures are established and used.

MAINTNANCE (M) 25-61-02 One or more may be removed provided that the associated door is considered inoperative. -For Cabin Passenger Door Slide or Slide Raft, Refer to AMM 52-10-00-040-001. -For Overwing Emergency Exit Slide or Slide Raft, Refer to AMM 25-62-00-040-006. OPERATIONS (O) 25-60-09 1. No passengers may be carried. 2. A maximum of 19 persons authorized in accordance with Equipment relief without passengers definition (refer to definitions section of this MEL) may be carried. 3. Captain will brief the first attendant as follow: Before takeoff, the first attendant shall ensure direct voice communication with the persons on board to provide a safety briefing about: a) No smoking during entire flight. b) The use of seat belts c) The location and operation of emergency exits, and d) For extended overwater operations, the location and operation of life preservers including a demonstration of the method of donning and inflating a life preserver.


N Registration

Page: 25.48


SUBJECT

25-65-01 Security Kit and Associated Equipment


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable to Avianca. Kit not installed on Avianca fleet.

N Registration

Page: 25.49


SUBJECT

25-65-02 Fireproof Gloves


CAT

No INS

MIN REQ

D

1

0

N Registration


Page: 25.50


SUBJECT

CAT

No INS

MIN REQ

C C C C C C

100 120 150 153 194 195

0 0 0 0 0 0


25-90-01 Printed Supplemental Safety Information For A318 Fleet For A319 Fleet For A320Ceo Fleet For A320Neo Fleet For A321Ceo Fleet For A321Neo Fleet (O) May be inoperative or missing provided: a) No passengers are carried, b) A maximum of 19 persons authorized in accordance with Equipment relief without passengers definition (refer to definitions section of this MEL) for non-passenger carrying operations are carried, and c) Alternate procedures are established and used. C C C C C C

100 120 150 153 194 195

42 46 60 62 80 81

For A318 Fleet For A319 Fleet For A320Ceo Fleet For A320Neo fleet For A321Ceo Fleet For A321Neo Fleet (M)(O) May be missing or damaged provided: a) Safety Information Card is located in convenient locations for use of each passenger; b) Cards cannot be missing from each exit seat; and c) Any seat(s) or row(s) of seats must be blocked where a Safety Information Card is not located in convenient locations for use of each passenger. NOTE1: The convenient location for Executive Class seats can be any of the two seats of any Row. NOTE2: The convenient location for Tourist Class seats is the middle seat of the three seats of any row.

OPERATIONS (O) 25-90-01 1. No passengers may be carried. 2. A maximum of 19 persons authorized in accordance with Equipment relief without passengers definition (refer to definitions section of this MEL) may be carried. 3. Captain will brief the first attendant as follow: Before takeoff, the first attendant shall ensure direct voice communication with the persons on board to provide a safety briefing about: a) No smoking during entire flight. (Continued) Revision: 36 June 30, 2017

N Registration

Page: 25.51


SUBJECT

CAT

No INS

MIN REQ


25-90-01 Printed Supplemental Safety Information (Continued) b) The use of seat belts c) The location and operation of emergency exits, and d) For extended overwater operations, the location and operation of life preservers including a demonstration of the method of donning and inflating a life preserver OPERATIONS (O) 25-90-01 second condition 3. Captain will brief the first attendant as follow: Before takeoff, the first attendant shall ensure direct voice communication with the persons on board to provide a safety briefing about: a) No smoking during entire flight. b) The use of seat belts c) The location and operation of emergency exits, and d) For extended overwater operations, the location and operation of life preservers including a demonstration of the method of donning and inflating a life preserver MAINTNANCE (M) 25-90-01 second condition In case there are not enough Supplementary Safety cards to be placed in the convenient location, the entire row must be blocked. Place a " Do not occupy" placard on each seat of the row.


N Registration

Page: 25.52

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 26 FIRE PROTECTION ITEM

26-00

SUBJECT

CAT

No INS

MIN REQ


CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) Fault(s) indicated by SDCU (Without Mod 30354 or without Mod. 33100)

C

2) Fault(s) indicated by SMOKE (With Mod 30354 or with Mod. 33100)

C

Not applicable to Avianca. Avianca fleet has incorporated Mod.30626 (A318) and Mod.33100 (A319-A320-A321)

NOTE: Dispatch with the above maintenance status message displayed on ECAM is permitted without CFDS interrogation.


N Registration

Page: 26.1


CAT

No INS

MIN REQ


1) Loop A

C

2

0

Except for ER operations beyond 120 minutes, one may be inoperative on each engine provided: a) Associated Loop B is operative, and b) The engine fire test is performed before each departure

2) Loop B

C

2

0

Except for ER operations beyond 120 minutes, one may be inoperative on each engine provided: a) Associated Loop A is operative, and b) The engine fire test is performed before each departure

SUBJECT

26-12-01 Engine Fire detection Systems


N Registration

Page: 26.2


SUBJECT

26-12-02 FIRE Lights on ENG Control Panel


CAT

No INS

MIN REQ

C

2

0

N Registration


Page: 26.3


SUBJECT

CAT

No INS

MIN REQ

C

16

8


26-12-03 ENG FIRE p.b. Lights 1) Bulbs/ LEDs


Four bulbs/ LEDs in each push button switch may be inoperative.

N Registration

Page: 26.4


SUBJECT

CAT

No INS

MIN REQ


C

2

1

Except for ER operations beyond 120 minutes, detection loop (B) may be inoperative provided APU fire test is performed before each APU start.

C

2

1

Except for ER operations beyond 120 minutes, detection loop (A) may be inoperative provided: a) APU fire test is performed before each APU start, and b) During ground operations, APU condition is monitored in the cockpit.

A

2

0

Except for ER operations beyond 120 minutes, may be inoperative provided: a) APU is not used, and b) Repairs are made within four flights.

C

2

0

Except for ER operations, may be inoperative provided APU is not used.

26-13-01 APU FIRE Detection System 1) Loops


N Registration

Page: 26.5


SUBJECT

CAT

No INS

MIN REQ

C

8

4

Four bulbs/ LEDs in push button may be inoperative

C

8

0

Except for ER operations, may be inoperative provided APU is not used.


26-13-02 APU FIRE p.b. Light 1) Bulbs/ LEDs


N Registration

Page: 26.6


SUBJECT

26-14-01 APU Fire Warning Light (on External Fire Panel)


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Moved to 26-22-11 REV 20 MMEL.

N Registration

Page: 26.7


SUBJECT

26-15-01 Avionic Smoke Detection System

CAT

No INS

MIN REQ


A

1

0

(O) Except for ER operations, may be inoperative for three flights legs.

Operational (O) 26-15-01 In case of electrical smoke in flight, apply AVIONICS SMOKE procedure. Refer to Quick Reference Handbook ABN-26-Fire Protection.


N Registration

Page: 26.8


SUBJECT

26-16-01 Blow In/Out Panels in Cargo Compartment


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Moved to Item 25-50-02.

N Registration

Page: 26.9


SUBJECT

26-16-03 Smoke Detectors in FWD Cargo Compartment

CAT

No INS

MIN REQ

C

2

0

For A318, A319 and A320 Fleet

C

4

0

For A321 Fleet


(O) May be inoperative provided procedures are established and used to ensure the associated compartment remains empty, or is verified to contain only empty cargo handling equipment, ballast (ballast may be loaded in ULDs), and/or Fly Away Kits NOTE: Operator MELs should define which items are approved for inclusion in the Fly Away Kits, and which materials can be used as ballast.

Aircraft with AAE, Ltd. STC No. ST01077WI (4 detector system)

Not applicable. Applicable to Aircraft with STC No. ST01077WI installed.

OPERATIONS (O) 26-16-03 Notify Dispatch Prior to each flight pilot must confirm with the ground personnel that only ballast or the Fly Away Kit (K.O.B) is allowed to be carried on the aircraft and those items must not be considered as dangerous materials. Refer to Avianca’s Dangerous Goods Manual If K.O.B (Kit On Board) or ballast is not carried in this compartment, it must be empty.


N Registration

Page: 26.10


SUBJECT

26-16-04 Smoke Detectors in AFT and Bulk Cargo Compartments

CAT

No INS

MIN REQ

C

4

0

For A318, A319 and A320 Fleet

C

6

0

For A321 Fleet


(O) May be inoperative provided procedures are established and used to ensure the associated compartment remains empty, or is verified to contain only empty cargo handling equipment, ballast (ballast may be loaded in ULD´s), and/or Fly Away kits. NOTE: Operator MELs should define which items are approved for inclusion in the Fly Away Kits, and which materials can be used as ballast. Aircraft with AAE, Ltd. STC No. ST01077WI (6 detector system)

Not applicable. Applicable to Aircraft with STC No. ST01077WI installed.

OPERATIONS (O) 26-16-04 Notify Dispatch Prior to each flight pilot must confirm with the ground personnel that only ballast or the Fly Away Kit (K.O.B) is allowed to be carried on the aircraft and those items must not be considered as dangerous materials. Refer to Avianca’s Dangerous Goods Manual If K.O.B (Kit On Board) or ballast is not carried in this compartment, it must be empty.


N Registration

Page: 26.11


SUBJECT

26-16-05 FWD/AFT Detection Loops/Channels AAE, Ltd. STC No. ST01077WI


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable. Applicable to Aircraft with STC No. ST01077WI installed.

N Registration

Page: 26.12


SUBJECT

26-17-01 Lavatory Smoke Detection System

CAT

No INS

MIN REQ

C

3

2

REMARKS OR EXCEPTIONS (M)(O) For each lavatory, the lavatory smoke detection system may be inoperative provided: a) Lavatory waste receptacle is empty, b) Lavatory door is locked closed and placarded "INOPERATIVE-DO NOT ENTER," and c) Lavatory is used only by crewmembers. NOTE: These provisos are not intended to prohibit lavatory use or inspections by crewmembers.

OPERATIONS (O) 26-17-01 If lavatory smoke detector system does not operate normally, ensure that the associated lavatory door remains locked and is not entered except for inspection by crewmembers MAINTENANCE (M) 26-17-01 1. If lavatory with defective smoke detector can be identified: 2. Access applicable lavatory waste bin, verify the fire extinguisher indicator gauge on the extinguisher bottle is in the green (serviceable) band and inspect extinguisher bottle and arm for damage. a) Is indicator is not in green (serviceable) band or bottle / discharge tube is damage, replace extinguisher. b) OR c) Empty lavatory waste receptacle. d) Deactivate lavatory and lock close. 3. Dispatch Concurrence required due lavatory (ies) usage may be affected.


N Registration

Page: 26.13


SUBJECT

26-17-02 Smoke Detection Control Unit (SDCU) (A319/A320/A321) (Without Mod 30354 or without Mod 33100)


CAT

No INS

MIN REQ


N Registration

Page: 26.14

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 26 FIRE PROTECTION SUBJECT

CAT

No INS

26-21-01 Engine AGENT 1&2 DISCH Light Systems

C

4

ITEM

MIN REQ


2

(M) One may be inoperative for each engine provided associated bottle(s) is verified properly charged before the first flight of each day.

PLACARD Install 26-21-01 INOP placard adjacent to AGENT 1 or AGENT 2 p.b switch affected. MAINTENANCE (M) 26-21-01 To Bottle Pressure Check refer to Aircraft Maintenance Manual (AMM) 26-21-00-040-001.


N Registration

Page: 26.15


CAT

No INS

26-21-02 Engine AGENT 1&2 SQUIB Light Systems

C

4

ITEM

MIN REQ


0

(M) May be inoperative provided it is verified that the failure is in the test circuit only.

PLACARD Install 26-21-02 INOP placard adjacent to AGENT 1 or AGENT 2 p.b switch affected. MAINTENANCE (M) 26-21-02 To Test of the SQUIB Legend of the AGENT Pushbutton switch refer to Aircraft Maintenance Manual (AMM) 26-21-00-040-003.


N Registration

Page: 26.16


SUBJECT

26-21-03 ENG FIRE Test Systems

CAT

No INS

MIN REQ

C

2

1

REMARKS OR EXCEPTIONS (M) One test function may be inoperative provided: a) The fault is in the test system only, b) System is tested once each flight day, and c) All other functions of fire detect systems operate normally.

PLACARD Install 26-21-03 INOP placard adjacent to TEST p.b switch affected. MAINTENANCE (M) 26-21-03 To ENG FIRE TEST - Circuit Verification refer to Aircraft Maintenance Manual (AMM) 26-21-00-040-002.


N Registration

Page: 26.17


CAT

No INS

26-22-00 APU Fire Extinguisher System

C

1

ITEM


MIN REQ

0

REMARKS OR EXCEPTIONS May be inoperative provided the APU is not used.

N Registration

Page: 26.18


SUBJECT

26-22-01 APU Agent DISCH Light

CAT

No INS

MIN REQ


C

1

0

(M) May be inoperative provided bottle is verified properly charged before the first flight of each day.

C

1

0

May be inoperative provided APU is not used.

PLACARD Install 26-22-01 INOP placard adjacent to AGENT p.b switch. MAINTENANCE (M) 26-22-01 To Bottle Pressure check refer to Aircraft Maintenance Manual (AMM) 26-22-00-040-004.


N Registration

Page: 26.19


SUBJECT

26-22-02 APU SQUIB Light

CAT

No INS

MIN REQ

C

1

0

(M) May be inoperative provided APU extinguishing system firing circuit is verified operative before the first flight of the day.

C

1

0



PLACARD Install 26-22-01 INOP placard adjacent to AGENT p.b switch. MAINTENANCE (M) 26-22-02 To Circuit Verification refer to Aircraft Maintenance Manual (AMM) 26-22-00-040-005.


N Registration

Page: 26.20

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 26 FIRE PROTECTION ITEM 26-22-03

SUBJECT APU Ground Automatic Fire Extinguisher System


CAT

No INS

MIN REQ


C

1

0

May be inoperative provided APU is continuously monitored in the cockpit during all APU ground operations.

C

1

0


N Registration

Page: 26.21


CAT

No INS

26-22-04 APU Fire Test System

C

1

0

(M) May be inoperative provided firing circuit and bottle low pressure detection systems are verified operative before the first flight of the day

C

1

0


ITEM

MIN REQ


PLACARD Install 26-22-04 INOP placard adjacent to TEST p.b switch. MAINTENANCE (M) 26-22-04 To Test Circuit Verification refer to Aircraft Maintenance Manual (AMM) 26-22-00-040-012.


N Registration

Page: 26.22


SUBJECT

26-22-05 APU fire Extinguisher Overpressure Indication (Red Disc)

CAT

No INS

MIN REQ


C

1

0

(M) May be missing provided: a) Squib test is used to verify squib integrity, and b) Bottle pressure switch is verified operative before the first flight of each day.

C

1

0

May be missing provided APU is not used.

MAINTENANCE (M) 26-22-05 To Bottle Pressure Switch Check refer to Aircraft Maintenance Manual (AMM) 26-22-00-040-007.


N Registration

Page: 26.23


CAT

No INS

26-22-06 APU FIRE PUSH p.b.

C

1

ITEM


MIN REQ

0


N Registration

Page: 26.24


SUBJECT

26-22-07 APU AGENT p.b.


CAT

No INS

MIN REQ

C

1

0


N Registration

Page: 26.25


CAT

No INS

26-22-08 APU Fire Extinguisher Bottle

C

1

ITEM


MIN REQ

0


N Registration

Page: 26.26


CAT

No INS

26-22-09 APU Fire Bottle Squibs

C

2

1

(M) One may be inoperative provided the remaining squib is verified operative before the first flight of each day.

C

2

0

May be inoperative provided the APU is not used.

ITEM

MIN REQ


PLACARD Install 26-22-09 INOP placard adjacent to APU FIRE Panel. MAINTENACE (M) 26-22-09 To Check of the remaining Squib Integrity refer to Aircraft Maintenance Manual (AMM) 26-22-00-040-008.


N Registration

Page: 26.27


SUBJECT

26-22-10 APU AUTO EXTING TEST


CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS May be inoperative provided the APU Automatic Fire Extinguishing System is considered inoperative.

N Registration

Page: 26.28


CAT

No INS

26-22-11 APU FIRE Light on External Power Panel

C

1

0

(M) May be inoperative provided the APU Automatic Fire Extinguishing System is verified operative.

C

1

0

May be inoperative provided APU is continuously monitored in the cockpit during all APU ground operations.

ITEM

MIN REQ


PLACARD Install 26-22-11 INOP adjacent to APU FIRE Light (External Power Panel). MAINTENANCE (M) 26-22-11 To make sure that the APU Automatic Fire Extinguishing System is operative when the APU FIRE Light on External Power Panel is inoperative refer to Aircraft Maintenance Manual (AMM) 26-22-00-040-010.


N Registration

Page: 26.29


SUBJECT

26-22-12 APU SHUT OFF p.b. on External Power Panel.

CAT

No INS

MIN REQ

C

1

0

(M) May be inoperative provided the APU Automatic Fire Extinguishing System is verified operative.

C

1

0

May be inoperative provided the APU Automatic Fire Extinguishing System is considered inoperative.


PLACARD Install 26-22-12 INOP adjacent to APU SHUT OFF p.b. switch (External Power Panel). MAINTENANCE (M) 26-22-12 To make sure that the APU Automatic Fire Extinguishing System is operative when the APU SHUT OFF PB on External Power Panel is inoperative refer to Aircraft Maintenance Manual (AMM) 26-22-00-040011.


N Registration

Page: 26.30


SUBJECT

CAT

No INS

MIN REQ

C

1

0


26-23-01 FWD/AFT and Bulk Cargo Compartment Fire Extinguishing System 1) Bottle 1

(O) May be inoperative provided procedures are established and used to ensure the associated compartment remains empty, or is verified to contain only empty cargo handling equipment, ballast (ballast may be loaded in ULD´s), and/or Fly Away kits NOTE 1: Operator MELs should define which items are approved for inclusion in the Fly Away Kits, and which materials can be used as ballast. NOTE 2: Class E cargo compartments require only the installation of smoke or fire detection systems (not suppression).

2) Bottle 2 3) Squib of Cargo Bottle 1

Not applicable to Avianca Fleet. C

2

0

(O) May be inoperative provided procedures are established and used to ensure all compartment remains empty, or is verified to contain only empty cargo handling equipment, ballast (ballast may be loaded in ULD´s), and / or Fly Away Kits. NOTE 1: Operator MELs should define which items are approved for inclusion in the Fly Away Kits, and which materials can be used as ballast. NOTE 2: Class E cargo compartments require only the installation of smoke or fire detection systems (not suppression).

4) Squib of Cargo Bottle 2


OPERATIONS (O) 26-23-01 1) & 3) Notify Dispatch. Prior to each flight pilot must confirm with the ground personnel that only ballast or the Fly Away Kit (K.O.B) is allowed to be carried on the aircraft and those items must not be considered as dangerous materials. Refer to Avianca’s Dangerous Goods Manual If K.O.B (Kit On Board) or ballast is not carried in this compartment, it must be empty.


N Registration

Page: 26.31


CAT

No INS

26-23-02 FWD/AFT Cargo Compartment DISCH Lights

C

1

0

(M) May be inoperative provided an acceptable test procedure is used once each flight day to verify that bottle is properly charged.

C

1

0

(O) May be inoperative provided procedures are established and used to ensure the associated compartment remains empty, or is verified to contain only empty cargo handling equipment, ballast (ballast may be loaded in ULD´s), and/or Fly Away kits

ITEM

MIN REQ


NOTE 1: Operator MELs should define which items are approved for inclusion in the Fly Away Kits, and which materials can be used as ballast. NOTE 2: If the AFT Cargo Compartment DISCH light is inoperative, the bulk cargo compartment must also remain empty.

PLACARD Install 26-23-02 INOP placard adjacent to DISCH light affected. OPERATIONS (O) 26-23-02 Notify Dispatch. Prior to each flight pilot must confirm with the ground personnel that only ballast or the Fly Away Kit (K.O.B) is allowed to be carried on the aircraft and those items must not be considered as dangerous materials. Refer to Avianca’s Dangerous Goods Manual. If K.O.B (Kit On Board) or ballast is not carried in this compartment, it must be empty. MAINTENANCE (M) 26-23-02 To Cargo Compartment DISCH LT - Verification of Fire-Extinguisher Bottle Weight refer to Aircraft Maintenance Manual (AMM) 26-23-00-040-001.


N Registration

Page: 26.32


SUBJECT

26-23-03 CARGO SMOKE DISCH AGENT 2 light


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable. Applicable to aircraft with CARGO SMOKE DISCH AGENT 2 light installed.

N Registration

Page: 26.33


SUBJECT

26-23-04 “PUSH” DSCH Switch Lights AAE, Ltd. STC No. ST01077WI


CAT

No INS

MIN REQ


N Registration

Page: 26.34


SUBJECT

26-23-05 “AUTO/MAN” DSCH Switchlights AAE, Ltd. STC No. ST01077WI


CAT

No INS

MIN REQ


N Registration

Page: 26.35


SUBJECT

26-23-06 DET LEDs AAE, Ltd. STC No. ST01077WI


CAT

No INS

MIN REQ


N Registration

Page: 26.36


SUBJECT

26-23-07 FAIL LEDs AAE, Ltd. STC No. ST01077WI


CAT

No INS

MIN REQ


N Registration

Page: 26.37


SUBJECT

26-23-08 Fault Panel (E & E compartment) AAE, Ltd. STC No. ST01077WI


CAT

No INS

MIN REQ


N Registration

Page: 26.38


SUBJECT

26-25-01 Lavatory Waste Bin fire Extinguisher System

CAT

No INS

MIN REQ

C

3

0

For each lavatory, the fire extinguisher system may be inoperative provided lavatory smoke detection system operates normally.

C

3

0

(M)(O) For each lavatory, the fire extinguisher system may be inoperative provided: a) Lavatory waste receptacle is empty, b) Lavatory door is locked closed and placarded "INOPERATIVE-DO NOT ENTER" and c) Lavatory is used only by crewmembers.


NOTE: These provisos are not intended to prohibit lavatory use or inspections by crewmembers OPERATIONS (O) 26-25-01 If lavatory Waste Bin fire Extinguisher System does not operate normally, ensure that the associated lavatory door remains locked and is not entered except for inspection by crewmembers MAINTENANCE (M) 26-25-01 Check the associated lavatory smoke detection system; refer to Aircraft Maintenance Manual (AMM) 2617-00-710-001.


N Registration

Page: 26.39


SUBJECT

26-26-24 Portable Fire Extinguishers

CAT

No INS

MIN REQ

D

5

4

For A318 Fleet

D

6

4

For A319 Fleet

D

7

4

For A320 and A321 Fleet


May be inoperative or missing provided: a) Inoperative fire extinguisher is tagged inoperative, removed from installed location, and placed out of sight so it cannot be mistaken for a functional unit, and b) Required distribution is maintained. NOTE 1: FAR 25.851 and RAC 4.5.6.6 requirements are already included herein. NOTE 2: For required distribution the portable Fire Extinguishing on cockpit must be operative and remaining Fire extinguishing must be located in order to cover all interior cabin.


N Registration

Page: 26.40

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 27 FLIGHT CONTROLS ITEM 27-00

SUBJECT

CAT

No INS

MIN REQ


CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) Fault(s) Indicated by F/CTL

C

2) Fault(s) Indicated by SFCS

C NOTE 1: Dispatch with either of the above maintenance status messages displayed on ECAM is permitted without CFDS interrogation. NOTE 2: The systems are designed to be fault tolerant for a period of time given on the category column in accordance with MEL preamble information. Quantities are not required for this item while the idea is to allow these fault indication.

3) Fault(s) Indicated by F/CTL (Aircraft without Mods: 21964 or 22087 or 22548)


Deleted MMEL revision 18.

N Registration

Page: 27.1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 27 FLIGHT CONTROLS ITEM

SUBJECT

CAT

No INS

MIN REQ

27-14-01 Aileron Servo Controls (A320-200 without Mod 26334 or 26335) (A318/A319/A321 and A320 with Mod 26334 or 26335)

REMARKS OR EXCEPTIONS Not applicable to Avianca. Avianca fleet has included Mod. 26335

A

4

2

(M)Two associated with ELAC 2 (left green and right blue) may be inoperative provided: a) Servos remain mechanically connected and hydraulically supplied (damping function is not affected), b) All roll spoilers operate normally, c) Aileron Servo Controls associated with ELAC 1 operate normally, and d) Repairs are made within three flight days.

A

4

2

(M)(O)Two associated with ELAC 1 (left blue and right green) may be inoperative provided: a) Servos remain mechanically connected and hydraulically supplied (damping function is not affected), b) All roll spoilers operate normally, c) Aileron Servo Controls associated with ELAC 2 operate normally, d) TR 1 and TR 2 operate normally, e) DC TIE contactor 1 is verified closed before takeoff, and f) Repairs are made within three flight days.

OPERATIONS (O) 27-14-01 Left Blue Servo-Control (Controlled by ELAC 1) During cockpit preparation: Aircraft supplied either by APU generator or by external power: Check on ECAM ELEC page link between DC BUS 1 and DC BAT BUS. Right Green Servo-Control (Controlled by ELAC 1) During cockpit preparation: Aircraft supplied either by APU generator or by external power: Check on ECAM ELEC page link between DC BUS 1 and DC BAT BUS. MAINTENANCE (M) 27-14-01 Refer to Aircraft Maintenance Manual (AMM) 27-14-00-040-001


N Registration

Page: 27.2


CAT

No INS

MIN REQ

1) ECAM Aileron Position Indications

C

2

0

2) ECAM Aileron Actuator Indications

C

4

0

SUBJECT


27-14-02 Aileron Indications on ECAM Flight Control Page (O) May be inoperative provided capability to move affected aileron through each servo control is verified visually before each departure.

OPERATIONS (O) 27-14-02 During cockpit preparation: YELLOW ELEC PUMP ………………………………………………………………………………..ON PTU ……………………………………………………………………………………..CHECK AUTO BLUE ELEC PUMP …………………………………………………………………..CHECK AUTO BLUE PUMP OVRD ………………………………………………………………………………..ON ELAC 1 and 2 ………………………………………………………………………………………….ON Move the stick from left stop to right stop and check visually the full travel of ailerons. If the expected aileron movement does not occur, maintenance action is due. ELAC 1 ………………………………………………………………………………………………….OFF Move the stick from left stop to right stop and check visually the full travel of ailerons. If the expected aileron movement does not occur, maintenance action is due. ELAC 1 …………………………………………………………………………………………………...ON YELLOW ELEC PUMP ……………………………………………………………………………….OFF BLUE ELEC PUMP …………………………………………………………………OFF then AUTO


N Registration

Page: 27.3


SUBJECT

27-14-03 ECAM Aileron Actuator Indications


CAT

No INS

MIN REQ


N Registration

Page: 27.4


SUBJECT

27-20-01 ECAM Rudder Position Indication

CAT

No INS

MIN REQ

B

1

0

REMARKS OR EXCEPTIONS (O) May be inoperative provided: a) A visual verification of rudder movement is made before each departure, and b) RUD TRIM indication is verified at zero before each departure.

OPERATIONS (O) 27-20-01 During cockpit preparation: YELLOW ELEC PUMP Establish Communications with ground personnel. On the CAPT or F/O side: Apply left rudder. Visually check rudder moves to left. On the CAPT or F/O side: Apply right rudder. Visually check rudder moves to right. On the CAPT or F/O side: Release pedals. Visually check rudder at neutral. YELLOW ELEC PUMP


…………………………………………..ON

………………………………………….OFF

N Registration

Page: 27.5


SUBJECT

27-20-02 Rudder Hydraulic System Pressure Indication Symbol on ECAM F/CTL Page


CAT

No INS

MIN REQ

C

3

0

N Registration


Page: 27.6


SUBJECT

27-21-01 Rudder Pedal Adjustment System

CAT

No INS

MIN REQ

C

2

0

REMARKS OR EXCEPTIONS (O)CAPT and/or F/O may be inoperative provided: a) Associated rudder pedals can be adjusted to a position which is acceptable to the affected crewmember, and b) Full and unrestricted movement of rudder pedals and brake pedal deflection is possible at both pilot stations.

OPERATIONAL (O) 27-21-01 During cockpit preparation : Apply loads simultaneously on both pedals (in rudder control movement direction) to make sure that the secured position is reached. For that purpose, the effort shall be equivalent to a full rudder deflection.


N Registration

Page: 27.7


CAT

No INS

MIN REQ

1) System No. 1

C

1

0

(O) Except for ER operations may be inoperative provided: a) Approach minimums do not require its use, and b) System 2 is verified to operate normally before each departure. NOTE: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.

2) System No. 2

C

1

0

(O) May be inoperative provided: a) Approach minimums do not require its use, and b) System 1 is verified to operate normally before each departure. NOTE: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.

SUBJECT


27-22-01 Rudder Trim Systems

OPERATIONS (O) 27-22-01 1. Verify remaining RUDDER TRIM system operates normally prior to each departure; on the ECAM FLT controls page. Coordinate with ground personnel for visual check of the correct deflection, any time it is required. Coordinate movements LH and RH, between FLT crew and ground personnel. For FLT crews at the gate, The PF presses the PEDAL DISC pushbutton on the nose wheel tiller, and silently applies full left rudder, full right rudder, and neutral. The PNF calls out "full left", "full right", "neutral", as each full travel/neutral position is reached, and coordinate with ground personnel removal of tow bar before the test. 2. Visually verify correct rudder deflection for the remaining Rudder Trim system before each departure.


N Registration

Page: 27.8


SUBJECT

27-22-02 Rudder Manual Trim Reset Function


CAT

No INS

MIN REQ


C

1

0

May be inoperative provided one rudder position indication is available.

N Registration

Page: 27.9

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 27 FLIGHT CONTROLS SUBJECT

CAT

No INS

27-22-03 Rudder Trim Position Indications

C

2

1

One indicator on ECAM or pedestal may be inoperative.

B

2

0

(O) May be inoperative provided: a) Rudder trim is verified to operate normally, b) Rudder position is verified at zero before each departure, and c) Rudder pedals are verified in a neutral position.

ITEM

MIN REQ


OPERATIONS (O) 27-22-03 If both position indicators (ECAM and pedestal) are inoperative: 1. Visually verify that Rudder Trim System is operative. 2. Visually verify Rudder position is at zero and rudder pedals are in neutral before each departure.


N Registration

Page: 27.10


CAT

No INS

27-23-01 Rudder Travel Limiter Systems

C

2

ITEM

MIN REQ

1


NOTE: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.


N Registration

Page: 27.11


SUBJECT

27-23-02 ECAM Rudder Travel Limiter Position Indication (Aircraft with Mod 31040 and Mod 30368)


CAT

No INS

MIN REQ

C

1

0

N Registration


Page: 27.12


CAT

No INS

MIN REQ

1) ECAM Elevator Position Indications

C

2

0

2) ECAM Elevator Actuator Indications

C

4

0

SUBJECT


27-30-01 Elevator Indications on ECAM Flight Control Page


May be inoperative provided a visual verification of affected elevator movement is made before each departure.

N Registration

Page: 27.13


SUBJECT

27-30-02 ECAM Elevator Actuator Indications


CAT

No INS

MIN REQ


N Registration

Page: 27.14


CAT

No INS

27-34-02 Elevator Servo Control Position Transducers

C

8

ITEM

MIN REQ


4

(M) One per servo control must operate normally.

MAINTENANCE (M) 27-34-02 Refer to Aircraft Maintenance Manual (AMM) 27-34-00-040-001


N Registration

Page: 27.15


SUBJECT

27-40-01 ECAM Pitch Trim Position Indication

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS (M)(O) May be inoperative provided a check of pitch trim hand wheel and stabilizer verifies synchronous movement.

OPERATIONS (O) 27-40-01 During cockpit preparation: YELLOW ELEC PUMP ………………………………………………………..ON Establish Communications with ground personnel. Pitch trim hand wheel ………………………….……move to full DN position Visually check that stabilizer moves to full down position. Pitch trim hand wheel …………………………….….move to full UP position Visually check that stabilizer moves to full up position. Pitch trim ………………………………………….set as required YELLOW ELEC PUMP ………………………………………………………OFF MAINTENANCE (M) 27-40-01 Refer to Aircraft Maintenance Manual (AMM) Task Number 27-40-00-040-001 to Check the synchronization between pitch trim handwheel and stabilizer.


N Registration

Page: 27.16


SUBJECT

27-44-01 Stabilizer Actuator Electrical Motors

CAT

No INS

MIN REQ

C

3

2

Motor 3 may be inoperative.

B

3

2

(M) Except for ER operations, Motor 2 may be inoperative provided ELAC 1 is considered inoperative.


OPERATIONAL NOTE (O) 27-44-01 When motor 2 is inoperative ELAC 1 is considered inoperative, refer to 27-93-01. MAINTENANCE (M) 27-44-01 To deactivate the Stabilizer Actuator Electrical Motor n.2 refer to Aircraft Maintenance Manual (AMM)Task Number 27-93-00-040-002.


N Registration

Page: 27.17


SUBJECT

27-44-02 Pitch Trim Hydraulic System Pressure Indication Symbol on ECAM F/CTL Page


CAT

No INS

MIN REQ

C

2

0

N Registration


Page: 27.18


SUBJECT

CAT

No INS

MIN REQ

B

2

1


27-51-01 Slat/Flap Control System (SFCS) 1) FLAP Channel (A318/319ceo/ A320ceo/ A321ceo)

(M)(O) SFCS 2 flap channel may be inoperative provided: a) Slats and flaps operate normally on SFCC 1, b) Operation of SFCC 1 WTBs are confirmed by tests before each departure, c) Electrical supply to SFCC 2 flap channel is inhibited, d) ELAC, SEC, ADIRS, LGCIU, FAC, and RA systems operate normally, e) Spoilers surfaces 2 and 4 operate normally, and. f) The minimum idle on ground function is considered inoperative NOTE: Minimum idle on ground function is inoperative. Refer to 73-20-03.

(A319neo/ A320neo/ A321neo)

B

2

1

(M)(O) SFCS 2 flap channel may be inoperative provided: a) Slats and flaps operate normally on SFCC 1, b) Operation of SFCC 1 WTBs are confirmed by tests before each departure, c) Electrical supply to SFCC 2 flap channel is inhibited, d) ELAC, SEC, ADIRS, LGCIU, FAC, and RA systems operate normally, e) Spoilers surfaces 2 and 4 operate normally, f) The minimum idle on ground function is considered inoperative, and g) The OAT is below ISA+35 degrees C.

2) SLAT Channel

B

2

1

(M)(O) SFCS 2 slat channel may be inoperative provided: a) Slats and flaps operate normally on SFCC 1, b) Operation of SFCC 1 WTBs are confirmed by tests before each departure, c) Electrical supply to SFCC 2 slat channel is inhibited, d) ELAC, SEC, ADIRS, LGCIU, FAC, and RA systems operate normally, and e) Takeoff in CONF 1+F is prohibited.


N Registration

Page: 27.19


SUBJECT

CAT

No INS

MIN REQ


Slat/Flap Control System (SFCS ( Continued) OPERATIONS (O) 27-51-01 -1) FLAP CHANNEL GENERAL INFORMATION ENG 2 APPR IDLE ONLY message is displayed on the STATUS SD page. FLAPS SLOW message is displayed on the STATUS SD page. FLIGHT PREPARATION/LIMITATIONS For aircraft with the RNP AR capability, RNP AR operations are not permitted. DURING COCKPIT PREPARATION Disregard and clear the F/CTL FLAP SYS 2 FAULT alert displayed on the EWD.

OPERATIONS (O) 27-51-01 -2) SLAT Channel GENERAL INFORMATION SLATS SLOW message is displayed on the STATUS SD page. FLIGHT PREPARATION/LIMITATIONS For aircraft with the RNP AR capability, RNP AR operations are not permitted. DURING COCKPIT PREPARATION Disregard and clear the F/CTL SLAT SYS 2 FAULT alert displayed on the EWD. FOR TAKEOFF Takeoff in CONF 1+F is not permitted. Note: When the SFCC 2 Slat channel is deactivated, and if the aircraft is in CONF 1+F, the SFCS 2 Flap channel is unable to crosscheck the airspeed coming from the ADR 1 with the ADR 2 airspeed coming from the SFCS 2 Slat channel. This may lead to an uncommanded flap retraction during the takeoff. As a consequence, takeoff in CONF 1+F is not permitted when the SFCC 2 Slat channel is deactivated

MAINTENANCE (M) 27-51-01 -1) Refer to Aircraft Maintenance Manual (AMM) Task Number 27-51-00-040-001 MAINTENANCE (M) 27-51-01 -2) Refer to Aircraft Maintenance Manual (AMM) Task Number 27-51-00-040-005


N Registration

Page: 27.20


SUBJECT

27-51-02 Flap Wing Tip Brake Solenoids

CAT

No INS

MIN REQ


C

4

2

(M) Solenoids associated with SFCC 2 may be inoperative provided operation of SFCC 1 WTBs is confirmed by test before each flight.



N Registration

Page: 27.21


SUBJECT

27-51-03 Flap Attachment Failure Detection Sensors


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Incorporated into 27-00, sub item 2).

N Registration

Page: 27.22


CAT

No INS

27-54-01 Flap Hydraulic Motors

C

2

1

Green motor may be inoperative.

C

2

1

Yellow motor may be inoperative provided blue slat motor operates normally.

ITEM


MIN REQ


N Registration

Page: 27.23


SUBJECT

27-54-02 Flap PCU Valve Blocks

CAT

No INS

MIN REQ


B

2

1

(M)(O) SFCS 2 Flap PCU Valve Block may be inoperative provided: a) Slats and flaps operate normally on SFCC 1, b) Operation of SFCC 1 WTBs are confirmed by tests before each departure, c) Electrical supply to SFCC 2 flap channel is inhibited, d) ELAC, SEC, ADIRS, LGCIU, FAC, and RA systems operate normally, e) Spoilers surfaces 2 and 4 operate normally, and f) The minimum idle on ground function is considered inoperative NOTE: Minimum idle on ground function is inoperative. Refer to 73-20-03.

OPERATIONS (O) 27-54-02 SFCS 2 Flap PCU valve Block may be inoperative provided: - Slats and Flaps operate normally on SFCC 1, - Operation of SFCC 1 WTBs is confirmed by testing before each departure, - Electrical supply to SFCC 2 Flap channel is inhibited, - ALEC, SEC, ADIRS, LGCIU, FAC and RA system operate normally - Spoiler surfaces 2 and 4 operate normally. - Minimum idle on ground functions are inoperative. Note: -

Disregard and clear the F/CLT FLAPS SYS 2 FAULT caution displayed on ECAM E/WD. Status messages “ ENG 2 APPR IDLE ONLY” and “FLAPS SLOW” are displayed.

MAINTENANCE (M) 27-54-02 Refer to Maintenance Procedure on A319/A320 AVA MEL on item 27-51-01, Subitem 1. Verify SFCC 1 WTB’s in accordance with operational procedure of this item (27-54-02).


N Registration

Page: 27.24


SUBJECT

CAT

No INS

MIN REQ


27-64-01 Spoiler Surfaces 1) A320 without Mod. 26334 or 26335 2) A318/A319/A321 and A320 with Mod. 26334 or 26335) except to A320200 with Sharklet.

Not applicable to Avianca. Avianca fleet has included Mod 26335 C

10

8

(M)(O) One pair of symmetrical surfaces 1 or 3 may be inoperative in the retracted position provided: a) SECs associated with operative spoilers operate normally, and b) AFM performance penalties are applied.

C

10

8

(M)(O) One pair of symmetrical surfaces 5 may be inoperative in the retracted position provided SECs associated with operative spoilers operate normally.

C

10

8

(M)(O) One pair of symmetrical surfaces 2 or 4 may be inoperative in the retracted position provided: a) SECs associated with operative spoilers operate normally, b) SFCS 2 flap channel operates normally, and c) AFM performance penalties are applied.

C

10

6

(M)(O) Two pair of symmetrical surfaces 1 and 2 may be inoperative in the retracted position provided: a) SECs associated with operative spoilers operate normally, b) SFCS 2 flap channel operates normally, and c) AFM performance penalties are applied.

C

10

6

(M)(O) Two pair of symmetrical surfaces 3 and 4 may be inoperative in the retracted position provided: a) SECs associated with operative spoilers operate normally, b) TR 1 and TR 2 are operate normally, c) DC Tie Contactor 1 is verified closed before each departure, d) SFCS 2 flap channel operates normally, and e) AFM performance penalties are applied.


N Registration

Page: 27.25


SUBJECT

CAT

No INS

MIN REQ


27-64-01 Spoiler Surfaces (Continued) 3) A320-200 with Sharklet Mod. 160500/MP J3283 or 160080/MP J3705

Applicable to N477AV, N562A, N603AV, N632AV, N724AV, N728AV, N740AV, N742AV, N743AV, N745AV, N748AV, N750AV, N755AV, N764AV and N765AV. C

10

8

(M)(O) One pair of symmetrical surfaces 1 or 3 may be inoperative in the retracted position provided: a) SECs associated with operative spoilers operate normally, b) AFM performance penalties are applied.

C

10

8

(M)(O) One pair of symmetrical surfaces 5 may be inoperative in the retracted position provided: a) SECs associated with operative spoilers operate normally, and b) The MTOW is limited to 76400 kg (168430 lb).

C

10

8

(M)(O) One pair of symmetrical surfaces 2 or 4 may be inoperative in the retracted position provided: a) SECs associated with operative spoilers operate normally, b) SFCS 2 flap channel operates normally, c) AFM performance penalties are applied, and d) If the pair of spoilers 4 is inoperative, the MTOW is limited to 76400 kg (168430 lb).

C

10

6

(M)(O) Two pair of symmetrical surfaces 1 and 2 may be inoperative in the retracted position provided: a) SECs associated with operative spoilers operate normally, b) SFCS 2 flap channel operates normally, and c) AFM performance penalties are applied.

(Continued)


N Registration

Page: 27.26


SUBJECT

CAT

No INS

MIN REQ

C

10

6


27-64-01 Spoiler Surfaces (Continued) (M)(O) Two pair of symmetrical surfaces 3 and 4 may be inoperative in the retracted position provided: a) SECs associated with operative spoilers operate normally, b) TR 1 and TR 2 are operate normally, c) DC Tie Contactor 1 is verified closed before departure, d) SFCS 2 flap channel operates normally, e) AFM performance penalties are applied, and f) The MTOW is limited to 76400 kg (168430 lb).

OPERATIONAL (O) 27-64-01 Surface 1 or 3 (Applicable to A318/A319/A320/A321 except to A320-200 with Sharklet) FLIGHT PREPARATION/LIMITATIONS The following penalties may be used for takeoff and landing performance determination if no takeoff and landing data (predetermined by using OCTOPUS program or other equivalent program with present failure case) is available. Takeoff performance computation: WARNING Do not use this method for takeoff on wet or contaminated runways. - Determine the Maximum Takeoff Weight and associated speeds in normal conditions on dry runway. - Decrease the Maximum Takeoff Weight by 800 kg (1 770 lb). - Decrease V1, VR, and V2 by 1 kt (Applicable to A318/A319 aircraft) - Decrease V1 by 1 kt. Keep VR and V2 unchanged (Applicable to A320 aircraft). If the actual TOW is lower than the MTOW calculated using above method: The speeds determined without failure and associated with the actual TOW may be retained provided they are all lower than the speeds calculated using above method. Check that the corrected V1 is equal to or above the minimum V1 value shown on the RTOW chart (due to VMCG limitation). If the corrected V1 is lower than the minimum V1: Take this last value as V1 Further decrease the weight by 3 000 kg (6 600 lb) per kt difference between both values. Check that the corrected VR is equal to or above the minimum VR value shown on the RTOW chart (due to VMCA limitation) (Applicable to A318/A319 aircraft). If the corrected VR is lower than the minimum VR (Applicable to A318/A319 aircraft): Takeoff is not possible using this method. (Continued) Revision: 36 June 30, 2017

N Registration

Page: 27.27


SUBJECT

CAT

No INS

MIN REQ


27-64-01 Spoiler Surfaces (Continued) Check that the corrected V2 is equal to or above the minimum V2 value shown on the RTOW chart (due to VMCA limitation). If the corrected V2 is lower than the minimum V2 (Applicable to A318/A319 aircraft): Takeoff is not possible using this method. Check that the corrected V2 is equal to or above the minimum V2 due to VMU limitation. (Refer to FCOM/PER-TOF-TOD-25-20 MINIMUM V2 LIMITED BY VMU/VMCA (KT IAS)) If the corrected V2 is lower than the minimum V2 (Applicable to A318/A319 aircraft): Takeoff is not possible using this method. Landing performance computation: Multiply the landing distances by 1.10 (Applicable to A318/A319 aircraft). Multiply the landing distances by 1.05 (Applicable to A320 aircraft). Multiply the landing distances by 1.05 (Applicable to A321 aircraft). AFTER ENGINE START On the HYD SD page, check the absence of amber data. FOR TAKEOFF If the above method was used for takeoff performance determination: Perform the takeoff using full thrust (TOGA). Surface 1 or 3 (Applicable to A320-200 with Sharklet) FLIGHT PREPARATION/LIMITATIONS Takeoff and landing performance computation: The takeoff and landing performance must be determined by using OCTOPUS program or other equivalent program with present failure case taken into account or refer to Dispatch guide. Launch PEP. Landing performance computation Multiply the landing distances by 1.10. (Applicable to A320-251N neo) Multiply the landing distances by 1.05. (Applicable to A320-200 ceo)

AFTER ENGINE START On the HYD SD page, check the absence of amber data. Surface 5 (Applicable to All aircraft configuration) AFTER ENGINE START On the HYD SD page, check the absence of amber data. Note: No performance penalty applies when the pair of spoilers 5 is inoperative. Surface 2 or 4 (Applicable to All aircraft configuration) FLIGHT PREPARATION/LIMITATIONS For performance penalties, refer to operational procedure 27-64-01 Spoiler 1 or 3 AFTER ENGINE START On the HYD SD page, check the absence of amber data.(Continued) Revision: 36 June 30, 2017

N Registration

Page: 27.28


SUBJECT

CAT

No INS

MIN REQ


27-64-01 Spoiler Surfaces (Continued) Surface 1 and 2 (Applicable to A318/A319/A320/A321 except to A320-200 with Sharklet) FLIGHT PREPARATION/LIMITATIONS The following penalties may be used for takeoff and landing performance determination if no takeoff and landing data (predetermined by using OCTOPUS program or other equivalent program with present failure case) is available. Takeoff performance computation: The method explained hereafter allows the determination of the MTOW and associated speeds (V1, VR, V2), by applying decrements on the MTOW and associated speeds computed in normal conditions (i.e. all systems operative). The method is based on the use of RTOW charts established at optimum V2/VS, optimum V1/VR, minimum V1. WARNING ‐ Do not use this method with takeoff charts computed with other conditions. ‐ Do not use this method for takeoff with tailwind. ‐ Do not use this method for takeoff on wet or contaminated runways. How to proceed? ‐ Read, in 0 kt wind column of the takeoff chart computed in normal condition, the MTOW and associated speeds (V1, VR, V2) corresponding to the actual temperature, even in the case of headwind (the method does not take into account the headwind benefit on takeoff performance). ‐ Apply the QNH and/or bleed corrections, if any, to determine the MTOW. ‐ Enter the following table to determine the MTOW and speed decrements. ‐ Applying these decrements, calculate the MTOW and associated speeds corresponding to the actual temperature. CAUTION Do not extrapolate below the shortest runway length provided by the table. Applicable to A318-111:


N Registration

Page: 27.29


SUBJECT

CAT

No INS

MIN REQ


27-64-01 Spoiler Surfaces (Continued) Applicable to A318-112:

Applicable to A319-112:


N Registration

Page: 27.30


SUBJECT

CAT

No INS

MIN REQ






N Registration

Page: 27.31


SUBJECT

CAT

No INS

MIN REQ



If the actual TOW is lower than the MTOW calculated using above method: The speeds determined without failure and associated with the actual TOW may be retained provided that they are all lower than the speeds calculated using above method. Check that the corrected V1 is equal to or above the minimum V1 value shown on the RTOW chart (due to VMCG limitation). If the corrected V1 is lower than the minimum V1: Take this last value as V1. Further decrease the weight by 3 000 kg (6 600 lb) per kt difference between both values. Check that the corrected VR is equal to or above the minimum VR value shown on the RTOW chart (due to VMCA limitation). If the corrected VR is lower than the minimum VR: Takeoff cannot be performed using this method. Check that the corrected V2 is equal to or above the minimum V2 value shown on the RTOW chart (due to VMCA limitation). If the corrected V2 is lower than the minimum V2: Takeoff cannot be performed using this method. Check that the corrected V2 is equal to or above the minimum V2 due to VMU limitation (Refer to FCOM/PER-TOF-TOD-25-20 MINIMUM V2 LIMITED BY VMU/VMCA (KT IAS)). If the corrected V2 is lower than the minimum V2: Takeoff cannot be performed using this method. Landing performance computation: Multiply the landing distances by 1.05 (Applicable to A318-111). Multiply the landing distances by 1.10 (Applicable to A318-112). Multiply the landing distances by 1.15 (Applicable to A319-112 and A319-132). Multiply the landing distances by 1.20 (Applicable to A319-115). Multiply the landing distances by 1.10 (Applicable to A320-214). Multiply the landing distances by 1.10 (Applicable to A321) (Continued) Revision: 36 June 30, 2017

N Registration

Page: 27.32


SUBJECT

CAT

No INS

MIN REQ


27-64-01 Spoiler Surfaces (Continued.) DURING COCKPIT PREPARATION ‐ SEC 3 pb-sw...........................................................................................................................OFF ‐ FLIGHT CONTROLS/SEC3/SPLY (121VU Q19) C/B.............................................................Pull TAKEOFF If the above method was used for takeoff performance computation: Perform the takeoff using full thrust (TOGA). IN FLIGHT In the case of further failure of SEC 1 and SEC 2: ‐ Autoland is not permitted. ‐ Disengage the AP at 500 ft RA before landing in direct law. As soon as the AP is disengaged when the three SECs are failed, it cannot be engaged again. ‐ Maximum landing capability is CAT 1 Surface 1 and 2 (Applicable to A320-200 with Sharklet) FLIGHT PREPARATION/LIMITATIONS Takeoff and landing performance computation: The takeoff and landing performance must be determined by using OCTOPUS program or other equivalent program with present failure case taken into account or refer to Dispatch guide. Launch PEP. Landing performance computation Multiply the landing distances by 1.10. (Applicable to A320-251N neo) Multiply the landing distances by 1.05. (Applicable to A320-200 ceo)

DURING COCKPIT PREPARATION ‐ SEC 3 pb-sw...........................................................................................................................OFF ‐ FLIGHT CONTROLS/SEC3/SPLY (121VU Q19) C/B.............................................................Pull IN FLIGHT In the case of further failure of SEC 1 and SEC 2:

‐ Autoland is not permitted. ‐ Disengage the AP at 500 ft RA before landing in direct law. As soon as the AP is disengaged when the three SECs are failed, it cannot be engaged again. ‐ Maximum landing capability is CAT 1 Surface 3 and 4 (Applicable to All aircraft configuration) FLIGHT PREPARATION/LIMITATIONS For performance penalties refer to Operational Procedure 27-64-01 Spoilers 1 and 2 DURING COCKPIT PREPARATION Check that the DC TIE contactor 1 is closed: ‐ Supply the electrical network from the APU or the external power. ‐ On the ELEC SD page, check the link between the DC BUS 1 and the DC BAT BUS.


N Registration

Page: 27.33


SUBJECT

CAT

No INS

MIN REQ


27-64-01 Spoiler Surfaces (Continued.) IN FLIGHT Do not use the speedbrakes. MAINTENANCE (M) 27-64-01 To Deactivation of the Spoiler Servo Control refer to Aircraft Maintenance Manual (AMM) 27-64-00-040001.


N Registration

Page: 27.34


SUBJECT

27-64-02 Load Alleviation Function (LAF) (A320-200 without Mod 26334 or 26335)


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable to Avianca. Avianca fleet has included Mod 26335

N Registration

Page: 27.35


SUBJECT

27-64-03 LAF Accumulators (A320200 without Mod 26334 or 26335)


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable to Avianca. Avianca fleet has included Mod 26335

N Registration

Page: 27.36


SUBJECT

27-64-04 Spoilers Hydraulic System Pressure Indication Symbol on F/CTL page


CAT

No INS

MIN REQ

C

3

0

N Registration


Page: 27.37


CAT

No INS

27-81-01 Slat Wing Tip Brakes Solenoids

C

4

ITEM

MIN REQ

2

REMARKS OR EXCEPTIONS (M) Solenoids associated with SFCC 2 may be inoperative provided SFCC 1 WTBs operate normally before each flight.

MAINTENANCE (M) 27-81-01 To Slat WTB Solenoid - WTB Test Procedure refer to Aircraft Maintenance Manual (AMM) 27-81-00-040001.


N Registration

Page: 27.38


CAT

No INS

27-84-01 Slats Hydraulic Motors

C

2

ITEM


MIN REQ

1

N Registration


Page: 27.39


CAT

No INS

27-84-02 Slat PCU Valve Blocks

B

2

ITEM

MIN REQ


1

(M)(O) SFCS 2 Slat PCU Valve Block may be inoperative provided: a) Slats, Flaps, and associated monitoring and protection systems operate normally on SFCC 1, b) Operation of SFCC 1 WTBs are confirmed by tests before each departure, c) Electrical supply to SFCC 2 slat channel is inhibited, d) ELAC, SEC, ADIRS, LGCIU, FAC and RA systems operate normally, and e) Takeoff in CONF 1+F is prohibited.

OPERATIONS (O) 27-84-02 SFCS 2 Slat PCU Valve Block may be inoperative provided: - Slats, Flaps and associated monitoring and protection systems, operate normally on SFCC1, - Operation of SFCC 1 WTBs is confirmed by testing before each departure, - Electrical supply to SFCC 2 slat channel is inhibited - ELAC, SEC, ADIRS, LGCIU, FAC, and RA systems operate normally, and - Takeoff in CONF 1 + F is prohibited. Note: - Disregard and clear the F/CLT FLAP SYS 2 FAULT caution displayed on ECAM E/WD. - Status messages “ENG 2 APPR IDLE ONLY” and “FLAPS SLOW” are displayed. MAINTENANCE (M) 27-84-02 Refer to maintenance procedure on A318/A319/A320 MEL of item 27-51-01 subitem 2. Verify SFCC 1 WTB’s in accordance with operational procedure of this item (27-84-02).


N Registration

Page: 27.40


SUBJECT

CAT

No INS

MIN REQ

C

1

0

(O) May be inoperative provided AFM performance penalties associated with all ground spoilers inoperative are applied.

C

3

2

(O) May be inoperative provided AFM performance penalties associated with one pair or two pairs of ground spoilers inoperative are applied.

27-92-01 Speed Brake Control System 1) Speed Brake 2 or 3 and 4


OPERATIONS (O) 27-92-01 In case of speedbrake 2 failure: -

Apply performance penalties associated with spoiler surface 2 inoperative. Refer to operational procedure on item 27-64-01 for surface 2 or 4

In case of speedbrakes 3 and 4 failure : -

Do not use the speedbrakes. Apply performance penalties associated with two pairs of spoilers inoperative. Refer to operational procedure on item 27-64-01 for surface 1 and 2.

OPERATIONS (O) 27-92-01 -1) Refer to operational procedure on item 27-92-02 2).


N Registration

Page: 27.41


CAT

No INS

27-92-02 Ground Spoiler Control System

A

1

0

1) Spoiler 5

C

2

0

2) Spoilers 1 and 2 or 3 and 4

C

8

4

ITEM

MIN REQ

REMARKS OR EXCEPTIONS (M) (O) May be inoperative provided: a) A check of the thrust reverser system is performed before each flight to ensure that both thrust reversers operate normally, b) Autobrake function is not used, c) Approach minimums do not require its use, d) AFM takeoff and landing performance penalties are applied, and e) Repairs are made within three flight legs. (O) Spoilers 1 and 2 or 3 and 4 may be inoperative provided AFM performance penalties are applied.

PLACARD Install 27-92-02 INOP placard adjacent to lower ECAM display. OPERATIONS (O) 27-92-02 (Applicable to A318/A319/A320/A321 except to A320-200 with Sharklet) GENERAL INFORMATION The autobrake function is not available. Refer to Operational Procedure 32-42-04 AUTO/BRK Function CAUTION One or both thrust reversers may not deploy at landing. Consequently, for performance determination, do not take into account the credit of the thrust reversers. FLIGHT PREPARATION/LIMITATIONS The following penalties may be used for takeoff and landing performance determination if no takeoff and landing data (predetermined by using OCTOPUS program or other equivalent program with present failure case) is available. Takeoff performance computation: The method explained hereafter allows the determination of the MTOW and associated speeds (V1, VR, V2), by applying decrements on the MTOW and associated speeds computed in normal conditions (i.e. all systems operative). WARNING ‐ Do not use this method with takeoff charts computed with other conditions or by using TLC program. ‐ Do not use this method for takeoff with tailwind. ‐ Do not use this method for takeoff on wet or contaminated runways. How to proceed? ‐ Read, in 0 kt wind column of the takeoff chart computed in normal condition, the MTOW and associated speeds (V1, VR, V2) corresponding to the actual temperature, even in the case of headwind (the method does not take into account the headwind benefit on takeoff performance). ‐ Apply the QNH and/or bleed corrections, if any, to determine the MTOW. ‐ Enter the following table to determine the MTOW and speed decrements. ‐ Applying these decrements, calculate the MTOW and associated speeds corresponding to the actual temperature. CAUTION: For runway lengths below 1,500 m, do not use the following table. (Continued) Revision: 36 June 30, 2017

N Registration

Page: 27.42


SUBJECT

CAT

No INS

MIN REQ


27-92-02

Ground Spoiler Control System Continued Applicable to A318-111:




N Registration

Page: 27.43

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 27 FLIGHT CONTROLS ITEM 27-92-02

SUBJECT

CAT

No INS

MIN REQ


Ground Spoiler Control System Continued




(Continued)


N Registration

Page: 27.44


SUBJECT

CAT

No INS

MIN REQ




If the actual TOW is lower than the MTOW calculated using above method: The speeds determined without failure and associated with the actual TOW may be retained provided that they are all lower than the speeds calculated using above method. Check that the corrected V1 is equal to or above the minimum V1 value shown on the RTOW chart (due to VMCG limitation). If the corrected V1 is lower than the minimum V1: Take this last value as V1. Further decrease the weight by 3 000 kg (6 600 lb) per kt difference between both values. Check that the corrected VR is equal to or above the minimum VR value shown on the RTOW chart (due to VMCA limitation). If the corrected VR is lower than the minimum VR: Takeoff cannot be performed using this method. Check that the corrected V2 is equal to or above the minimum V2 value shown on the RTOW chart (due to VMCA limitation). If the corrected V2 is lower than the minimum V2: Takeoff cannot be performed using this method. Check that the corrected V2 is equal to or above the minimum V2 due to VMU limitation (Refer to FCOM/PER-TOF-TOD-25-20 MINIMUM V2 LIMITED BY VMU/VMCA (KT IAS)). If the corrected V2 is lower than the minimum V2: Takeoff cannot be performed using this method. Landing performance computation: Multiply the landing distances by 1.15 (Applicable to A318-111). Multiply the landing distances by 1.30 (Applicable to A318-112). Multiply the landing distances by 1.40 (Applicable to A319-112 and A319-132). Multiply the landing distances by 1.50 (Applicable to A319-115 and A321-253N neo) Multiply the landing distances by 1.35 (Applicable to A320-214). Multiply the landing distances by 1.15 (Applicable to A321-214).


N Registration

Page: 27.45


SUBJECT

CAT

No INS

MIN REQ



TAKEOFF If the above method was used for takeoff performance computation: Perform the takeoff using full thrust (TOGA). OPERATIONS (O) 27-92-02 (Applicable to A320-200 with Sharklet) GENERAL INFORMATION The autobrake function is not available. Refer to Operational Procedure 32-42-04 AUTO/BRK Function. CAUTION One or both thrust reversers may not deploy at landing. Consequently, for performance determination, do not take into account the credit of the thrust reversers. FLIGHT PREPARATION/LIMITATIONS The takeoff and landing performance must be determined by using OCTOPUS program or other equivalent program with present failure case taken into account or refer to Dispatch guide. Launch PEP. Landing performance computation: Multiply the landing distances by 1.40. (Applicable to A320-251N neo) Multiply the landing distances by 1.35. (Applicable to A320-200 ceo)

OPERATIONS (O) 27-92-02-1 FLIGHT PREPARATION/LIMITATIONS

For performance penalties, refer to operational procedure on item 27-64-01 for surface 5 OPERATIONS (O) 27-92-02 -2) FLIGHT PREPARATION/LIMITATIONS

For performance penalty refer to operational procedure on item 27-64-01 for surfaces 1 and 2 or for surfaces 3 and 4. MAINTENANCE (M) 27-92-02 Refer to AMM 78-31-00-710-042 (applicable to CFM engines only) or refer to AMM 78-31-00-710-041 (applicable to IAE engines only).


N Registration

Page: 27.46


SUBJECT

27-92-03 Accelerometer Systems


CAT

No INS

MIN REQ


N Registration

Page: 27.47


SUBJECT

27-92-04 Sidestick Transducer Systems


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Deleted, on MMEL Rev. 4.

N Registration

Page: 27.48


SUBJECT

CAT

No INS

MIN REQ


C

10

9

May be inoperative for an associated inoperative spoiler.

C

10

0

(O) May be inoperative provided a visual check of affected surface movement is made before each departure.

27-92-05 Spoiler/Speed- brake Indications on ECAM F/CTL and Wheel Page

OPERATIONS (O) 27-92-05 During cockpit preparation: -

If surface 1 affected: CAUTION: Aircraft must be stopped. YELLOW ELEC PUMP ………………………………………….……………….ON PTU …………………………….……………….CHECK AUTO SPD BRK ………………………………………………………..FULL Check visually surface 1 slightly extends (approximately 6°). YELLOW ELEC PUMP ………………………………………………………….OFF

-

If surface 3 affected: BLUE ELEC PUMP ………………………………………………CHECK AUTO BLUE PUMP OVRD ……………………………………………………………ON Move the stick from left stop to right stop and check visually the correct movement of surface 3. BLUE ELEC PUMP …………………………………………….OFF then AUTO

-

If surface 2, 4 or 5 affected: YELLOW ELEC PUMP ……………………………………………………………ON PTU ………………………………………………CHECK AUTO Move the stick from left stop to right stop and check visually the correct movement of surfaces 2, 4 and 5. YELLOW ELEC PUMP ………………………………………………………….OFF


N Registration

Page: 27.49


CAT

No INS

MIN REQ

1) Flashing portion of sidestick dual input function in lower half of sidestick priority green light.

D

2

0

2) Aural Warning

D

1

0

SUBJECT


27-92-06 Side Stick Dual Input Warning System


May be inoperative provided sidestick priority function is operative.

N Registration

Page: 27.50


SUBJECT

CAT

No INS

MIN REQ


27-92-07 Thrust Lever Transducers 1) SEC 1

Incorporated into 27-92-02.

2) SEC 2

Incorporated into 27-00, sub item 1).

3) SEC 3



N Registration

Page: 27.51


SUBJECT

CAT

No INS

MIN REQ


27-92-08 SEC Tachometer Inputs 1) SEC 1


2) SEC 2

Incorporated into 27-00, sub item 1).

3) SEC 3



N Registration

Page: 27.52


SUBJECT

27-92-09 Hydraulic Pressure Switches


CAT

No INS

MIN REQ


N Registration

Page: 27.53


SUBJECT

27-92-10 Hydraulic Pressure Transducers


CAT

No INS

MIN REQ


N Registration

Page: 27.54


SUBJECT

27-92-11 STEEP APPR p.b. Switch (With Mod.35542)


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable to Avianca Fleet. Avianca have not Mod 35542 installed

1) ON Light


2) FAULT Light


N Registration

Page: 27.55


SUBJECT

CAT

No INS

MIN REQ


27-93-01 Elevator Aileron Computers (ELAC) (A320-200 without Mod 26334 or 26335) (A318/A319/A321 and A320 with Mod. 26334 or 26335)

Not applicable to Avianca. Avianca fleet has included Mod 26335 B

2

1

(M)(O) Except for ER operation, ELAC 1 or any ELAC 1 function may be inoperative provided: a) Both accelerometers associated with ELAC 2 operate normally, b) All sidestick transducers associated with ELAC 2 and the three SECs operate normally, c) ELAC 2, SECs, ADIRs, SFCCs, LGCIUs, FACs, and Ras operate normally, d) TR 1 and TR 2 operate normally, e) DC TIE contactor 1 is verified closed before each departure, f) All roll spoilers operate normally, g) Elevators and roll spoilers control through the SECs is checked operative before each flight, h) Approach minimums do not require its use, and i) Above FL 200, the use of speed brakes lever is limited to its half Position (A320 without Mod 33317) ( i) instructions not applicable to Avianca, Avianca fleet has incorporated Mod 33317). NOTE1: When the ELAC 1 FAULT alert is displayed (ELAC 1 is not electrically supplied), F/O Take- Over p.b cannot disengage AP1. NOTE 2: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.

OPERATIONS (O) 27-93-01 Note: Maximum landing capability is CAT 3 SINGLE. 1. In case of application of this MEL item following F/CTL ELAC 1 FAULT caution on ECAM E/WD: Note: 1) After the maintenance procedure has been applied, only ELEC C/B TRIPPED ON R ELEC BAY and ELEC C/B TRIPPED ON OVHD PNL remain displayed on ECAM E/WD. 2) After first engine starting, the ECAM caution F/CTL ALTN LAW may be spuriously triggered. It normally disappears after second engine starting. (Continued) Revision: 36 June 30, 2017

N Registration

Page: 27.56


SUBJECT

CAT

No INS

MIN REQ


27-93-01 Elevator Aileron Computers (ELAC) (Continued) During cockpit preparation: 1. Check that elevator and roll spoilers control is operative through the SEC's : YELLOW ELEC PUMP …………………………………………………….……………ON PTU …………………………………………………….CHECK AUTO BLUE ELEC PUMP …………………………………………………….CHECK AUTO BLUE PUMP OVRD ………………………………………………………………….ON ELAC 2 ………………………………………………………………….ON SEC 1, 2 and 3 ………………………………………………………………….ON After 5 seconds do the following checks: 1 a) Check elevator control through SEC 1 and spoilers control through SEC 1 and SEC 3 : BLUE ELEC PUMP ……………………………………………………OFF then AUTO Wait for hydraulic circuit depressurization and check on ECAM F/CTL page that blue elevator actuator symbol becomes amber. After 5 seconds: BLUE PUMP OVRD ………………………………………………………………….ON ELAC 2 …………………………………………………………………OFF SEC 2 …………………………………………………………………OFF Move the CAPT stick from right stop to left stop, then from forward stop to aft stop. Check on ECAM F/CTL page the correct movement of spoilers 2 + 3 + 4 and the full travel of both elevators. If an expected spoiler or elevator movement does not occur, do not attempt any reset: maintenance action is due. Perform same check from F/O Stick. 1 b) Check elevator control through SEC 2 and spoilers control through SEC 2 and SEC 3: ELAC 2 …………………………………………………………………ON SEC 2 …………………………………………………………………ON After 5 seconds: YELLOW ELEC PUMP …………………………………………………………………OFF Wait for hydraulic circuits depressurization and check on ECAM F/CTL page that yellow and green elevator actuators symbols become amber. After 5 seconds: YELLOW ELEC PUMP ………………………………………………………………….ON ELAC 2 ………………………………………………………………..OFF SEC 1 ………………………………………………………………..OFF Move the CAPT stick from right stop to left stop, then from forward stop to aft stop. Check on ECAM F/CTL page the correct movement of spoilers 2 + 5 and the full travel of both elevators. If an expected spoiler or elevator movement does not occur, do not attempt any reset: maintenance action is due. Perform same check from F/0 Stick. 1 c) Return to normal configuration: YELLOW ELEC PUMP …………………………………………………………………OFF BLUE ELEC PUMP ……………………………………………………OFF then AUTO ELAC 1 …………………………………………………………………OFF ELAC 2 …………………………………………………………………..ON SEC 1 …………………………………………………………………..ON (Continued) Revision: 36 June 30, 2017

N Registration

Page: 27.57


SUBJECT

CAT

No INS

MIN REQ


27-93-01 Elevator Aileron Computers (ELAC) (Continued) Before engines start: AP1 …………………………………………………………………..ON CAPT take-over pb ……………………………………………………………...PRESS Check that the red AP OFF message appears on ECAM. If AP1 is used for approach, pilot flying will be the captain. Note: Due to the fact that ELAC 1 is not electrically supplied, F/O take-over pb cannot disengage API. 3 - Check of DC TIE contactor 1 operation. Aircraft supplied either by APU generator or by external power: check on ECAM ELEC page link between DC BUS 1 and DC BAT BUS 2. In case of "ELAC 1 PITCH FAULT" caution on ECAM E/WD: Note: After first engine starting, the ECAM caution F/CTL ALTN LAW may be spuriously triggered during a very short period. It normally disappears after a few seconds when ELAC 2 auto test is accomplished. During cockpit preparation : 1 - Check that elevator and roll spoilers control is operative through the SEC's : YELLOW ELEC PUMP ……………………………………………..……………..ON PTU ………………………………………………CHECK AUTO BLUE ELEC PUMP ………………………………………………CHECK AUTO BLUE PUMP OVRD ……………………………………………………………ON ELAC 1 ……………………………………………………………ON ELAC 2 ……………………………………………………………ON SEC 1, 2 and 3 ……………………………………………………………ON After 5 seconds do the following checks: 1 a) Check elevator control through SEC 1 and spoilers control through SEC 1 and SEC 3 : BLUE ELEC PUMP …………………………………………….OFF then AUTO Wait for hydraulic circuit depressurization and check on ECAM F/CTL page that blue elevator actuator symbol becomes amber. After 5 seconds: BLUE PUMP OVRD ……………………………………………………………ON ELAC 1 …………………………………………………………..OFF ELAC 2 …………………………………………………………..OFF SEC 2 …………………………………………………………..OFF Move the CAPT stick from right stop to left stop, then from forward stop to aft stop. Check on ECAM F/CTL page the correct movement of spoilers 2 + 3 + 4 and the full travel of both elevators. If an expected spoiler or elevator movement does not occur, do not attempt any reset: maintenance action is due. Perform same check from F/O Stick. (Continued) Revision: 36 June 30, 2017

N Registration

Page: 27.58


SUBJECT

CAT

No INS

MIN REQ


27-93-01 Elevator Aileron Computers (ELAC) (Continued) 1 b) Check elevator control through SEC 2 and spoilers control through SEC 2 and SEC 3: ELAC 1 …………………………………………………………ON ELAC 2 …………………………………………………………ON SEC 2 …………………………………………………………ON After 5 seconds: YELLOW ELEC PUMP ………………………………………………………...OFF Wait for hydraulic circuits depressurization and check on ECAM F/CTL page that yellow and green elevator actuators symbols become amber. After 5 seconds: YELLOW ELEC PUMP ………………………………………………………….ON ELAC 1 …………………………………………………………OFF ELAC 2 …………………………………………………………OFF SEC 1 …………………………………………………………OFF Move the CAPT stick from right stop to left stop, then from forward stop to aft stop. Check on ECAM F/CTL page the correct movement of spoilers 2 + 5 and the full travel of both elevators. If an expected spoiler or elevator movement does not occur, do not attempt any reset: maintenance action is due. Perform same check from F/O Stick. 1 c) Return to normal configuration: YELLOW ELEC PUMP …………………………………………………………OFF BLUE ELEC PUMP ……………………………………………OFF then AUTO ELAC 1 …………………………………………………………..ON ELAC 2 …………………………………………………………..ON SEC 1 …………………………………………………………..ON Set ELAC 1 pb sw at OFF only if required by ECAM. 2 -Check of DC TIE contactor 1 operation. Aircraft supplied either by APU generator or by external power: check on ECAM ELEC page link between DC BUS 1 and DC BAT BUS. MAINTENANCE (M) 27-93-01 To Deactivation of the Elevator Aileron Computer refer to Aircraft Maintenance Manual (AMM) 27-93-00040-001.


N Registration

Page: 27.59


CAT

No INS

MIN REQ

1) FAULT Lights

C

2

1

2) OFF Lights

C

2

0

SUBJECT


27-93-02 ELAC p.b. Switch


May be inoperative provided: a) Both FWCs operate normally, and b) ELAC indications operate normally.

N Registration

Page: 27.60


SUBJECT

27-93-03 ECAM ELAC Indications


CAT

No INS

MIN REQ


C

2

1

One may be inoperative for an inoperative ELAC 1.

C

2

0

May be inoperative provided: a) Both FWCs operate normally, and b) ELAC fault light operates normally.

N Registration

Page: 27.61


SUBJECT

CAT

No INS

MIN REQ


27-94-01 Spoiler Elevator Computers (SEC) 1) SEC 1 a) A320 without Mod 26334/MP J1616 or 26335/MP J1617, and A320 without MOD 160500/MP J3283 or 160080/MP J3705

b) A318/A319/A321 and A320 with Mod 26334/MP J1616 or 26335/MP J1617, and A320 without MOD 160500/MP J3283 or 160080/MP J3705 (Without Sharklets)

Not applicable to Avianca. Avianca fleet has included Mod 26335 and 160500

C

1

0

(M)(O) Except for ER operations, SEC 1 may be inoperative provided: a) SEC 1 is deactivated. b) SEC 2 and SEC 3 are operative, c) Sidestick transducers associated with ELACs and operative SECs are verified operative before each flight, d) All ELACs, SFCCs, LGCIUs, RAs, FACs and ADIRs are operative, e) SFCS No. 2 flap channel is operative, f) All aileron servo channels and roll spoilers associated with the operative SECs are operative, g) TR 1 and TR 2 are operative, h) DC TIE contactor 1 is verified closed before each flight, i) Elevators control through SEC 2 and ELACs and roll spoilers control through the operative SECs are verified operative before each flight, and j) AFM performance penalties for two pairs of spoilers inoperative are applied.

(Continued)


N Registration

Page: 27.62


SUBJECT

CAT

No INS

MIN REQ


C

1

0

Applicable to N477AV, N562AV, N603AV, N632AV, N724AV, N728AV, N740AV, N742AV, N743AV, N745AV, N748AV, N750AV, N755AV, N764AV and N765AV (M)(O) Except for ER operations, may be inoperative provided: a) SEC1 is deactivated b) SEC 2 and SEC 3 are operative, c) Sidestick transducers associated with ELACs and operative SECs are verified operative before each flight, d) All ELACs, SFCCs, LGCIUs, RAs, FACs and ADIRs are operative, e) SFCS No. 2 flap channel is operative, f) All aileron servo channels and roll spoilers associated with the operative SECs are operative, g) TR 1 and TR 2 are operative, h) DC TIE contactor 1 is verified closed before each flight, i) Elevators control through SEC 2 and ELACs and roll spoilers control through the operative SECs are verified operative before each flight, j) AFM performance penalties for two pairs of spoilers inoperative are applied, and k) The MTOW is limited to 76400 kg (168430 lb).

27-94-01 Spoiler Elevator Computers (SEC) (Continued)

c) A320-200 with Sharklet Mod. 160500/MP J3283 or 160080/MP J3705

2) SEC 2 a) A320 without Mod 26334/MP J1616 or 26335/MP J1617, and A320 without MOD 160500/MP J3283 or 160080/MP J3705 b) A318/A319/A321 and A320 with Mod. 26334/MP J1616 or 26335/MP J1617, and A320 without MOD 160500/MP J3283 or 160080/MP J3705 (A320-200 without sharklets)

Not applicable to Avianca. Avianca fleet has included Mod 26335 and 160500

C

1

0

(M)(O) May be inoperative provided: a) SEC 2 is deactivated. b) SEC 1 and SEC 3 are operative, c) Sidestick transducers associated with ELACs and operative SECs are verified operative before each flight, d) All ELACs, SFCCs, LGCIUs, RAs, FACs and ADIRs are operative, e) All aileron servo channels and roll spoilers associated with the operative SECs are operative, f) Elevators control through SEC 1 and ELACs and roll spoilers control through the operative SECs are verified operative before each flight.

(Continued)


N Registration

Page: 27.63


SUBJECT

CAT

No INS

MIN REQ

C

1

0


27-94-01 Spoiler Elevator Computers (SEC) (Continued) c) A320-200 with Sharklet Mod. 160500/MP J3283) or 160080/MP J3705

Applicable to N477AV, N562AV, N603AV, N632AV, N724AV, N728AV, N740AV, N742AV, N743AV, N745AV, N748AV, N750AV, N755AV, N764AV and N765AV. (M)(O) May be inoperative provided: a) SEC 2 is deactivated b) SEC 1 and SEC 3 are operative, c) Sidestick transducers associated with ELACs and operative SECs are verified operative before each flight, d) All ELACs, SFCCs, LGCIUs, RAs,FACs and ADIRs are operative, e) All aileron servo channels and roll spoilers associated with the operative SECs are operative, f) Elevators control through SEC 1 and ELACs and roll spoilers control through the operative SECs are verified operative before each flight, and g) The MTOW is limited to 76400 kg (168430 lb).

3) SEC 3

C

1

0

(M)(O) May be inoperative provided: a) SEC 3 is deactivated b) SEC 1 and SEC 2 are operative, c) SFCS No. 2 flap channel is operative, d) All aileron servo channels and roll spoilers associated with the operative SECs are operative, and e) AFM performance penalties for two pairs of spoilers inoperative are applied.

PLACARD Install INOP placard adjacent to FLT CTL control panel. OPERATIONS (O) 27-94-01 -1) SEC 1 Takeoff and landing performance: Apply performance penalties for spoilers 3 and 4. Refer to operational procedure on item 27-64-01 for surfaces 3 and 4. During Cockpit Preparation Note: If the Yellow Electric Pump is not available: - Pressurize the Yellow Hydraulic System with: - A Ground cart, or with - The Yellow Engine 2 Pump with the Engine 2 running. - Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure. (Continued) Revision: 36 June 30, 2017

N Registration

Page: 27.64


SUBJECT

CAT

No INS

MIN REQ


27-94-01 Spoiler Elevator Computers (SEC) (Continued) Note: After application of the maintenance procedure, the C/B TRIPPED R ELEC BAY and the C/B TRIPPED ON OVHD PNL alerts are display on the EWD. Check of the elevator controls through the operative computers: Put the aircraft in the test configuration: - YELLOW ELEC PUMP pb-sw...................................................................................... ON ‐ PTU pb-sw................................................................................................................... AUTO ‐ BLUE ELEC PUMP pb-sw........................................................................................... AUTO ‐ BLUE PUMP OVRD pb................................................................................................ ON ‐ ELAC 1 pb-sw.............................................................................................................. ON ‐ ELAC 2 pb-sw.............................................................................................................. ON ‐ SEC 2 pb-sw................................................................................................................ ON ‐ SEC 3 pb-sw................................................................................................................ ON - Wait 5 s Check of the elevator control through the ELAC 1: - BLUE PUMP OVRD pb-sw........................................................................................... OFF ‐ Wait for hydraulic circuit depressurization. ‐ On the F/CTL SD page, check that blue elevator actuator symbol becomes amber. ‐ Wait 5 s ‐ BLUE PUMP OVRD pb-sw........................................................................................... ON ‐ ELAC 2 pb-sw............................................................................................................... OFF ‐ SEC 2 pb-sw................................................................................................................. OFF ‐ Move the CAPT stick from forward stop to aft stop. ‐ On the F/CTL SD page, check the full travel of both elevators. CAUTION: If an expected elevator movement does not occur, do not attempt any reset. Contact the maintenance. Check of the elevator control through the SEC 2: ‐ ELAC 2 pb-sw.............................................................................................................. ON ‐ SEC 2 pb-sw................................................................................................................ ON ‐ Wait 5 s ‐ YELLOW ELEC PUMP pb-sw...................................................................................... OFF ‐ Wait for hydraulic circuits depressurization. ‐ On the F/CTL SD page, check that the yellow and the green elevator actuators symbols become amber. ‐ Wait 5 s ‐ YELLOW ELEC PUMP pb-sw...................................................................................... ON ‐ ELAC 1 pb-sw.............................................................................................................. OFF ‐ ELAC 2 pb-sw.............................................................................................................. OFF ‐ Move the CAPT stick from right stop to left stop, then from forward stop to aft stop. Each stop must be applied during 3 s (Continued) Revision: 36 June 30, 2017

N Registration

Page: 27.65


SUBJECT

CAT

No INS

MIN REQ


27-94-01 Spoiler Elevator Computers (SEC) (Continued) ‐ On the F/CTL SD page, check the correct movement of the pairs of spoilers 2 and 5 and the full travel of both elevators. ‐ Move the F/O stick from right stop to left stop, then from forward stop to aft stop. Each stop must be applied during 3 s ‐ On the F/CTL SD page, check the correct movement of the pairs of spoilers 2 and 5 and the full travel of both elevators. CAUTION: If an expected spoiler or elevator movement does not occur, do not attempt any reset. Contact the maintenance. Return to normal configuration: ‐ YELLOW ELEC PUMP pb-sw.......................................................................................OFF ‐ BLUE PUMP OVRD pb-sw.......................................................................................... OFF ‐ ELAC 1 pb-sw.............................................................................................................. ON ‐ ELAC 2 pb-sw.............................................................................................................. ON Check that the DC TIE contactor 1 is closed: ‐ Supply the electrical network from the APU or the external power. ‐ On the ELEC SD page, check the link between the DC BUS 1 and the DC BAT BUS. IN FLIGHT Do not use the speedbrakes. If the SEC 2 and the SEC 3 fail during the flight: - Autoland is not permitted. - Maximum landing capability is CAT 1 - Disengage the AP at 500 ft RA before landing in direct law. - When the AP is disengaged with the three SECs failed, it cannot be engaged again. OPERATIONS (O) 27-94-01 -2) SEC 2 During Cockpit Preparation Note: If the Yellow Electric Pump is not available: - Pressurize the Yellow Hydraulic System with: - A Ground cart, or with - The Yellow Engine 2 Pump with the Engine 2 running. - Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure. Note: After application of the maintenance procedure, the C/B TRIPPED REAR PNL N-R alert is displayed on the EWD. (Continued)


N Registration

Page: 27.66


SUBJECT

CAT

No INS

MIN REQ


27-94-01 Spoiler Elevator Computers (SEC) (Continued) Check of the elevator control through the operative computers: Put the aircraft in the test configuration: ‐ YELLOW ELEC PUMP pb-sw...................................................................................... ON ‐ PTU pb-sw................................................................................................................... AUTO ‐ BLUE ELEC PUMP pb-sw........................................................................................... AUTO ‐ BLUE PUMP OVRD pb................................................................................................ ON ‐ ELAC 1 pb-sw.............................................................................................................. ON ‐ ELAC 2 pb-sw.............................................................................................................. ON ‐ SEC 1 pb-sw................................................................................................................ ON ‐ SEC 3 pb-sw................................................................................................................ ON ‐ Wait 5 s Check of the elevator control through the ELAC 1: ‐ BLUE PUMP OVRD pb-sw.......................................................................................... OFF ‐ Wait for hydraulic circuit depressurization. ‐ On the F/CTL SD page, check that blue elevator actuator symbol becomes amber. ‐ Wait 5 s ‐ BLUE PUMP OVRD pb-sw.......................................................................................... ON ‐ ELAC 2 pb-sw.............................................................................................................. OFF ‐ SEC 1 pb-sw................................................................................................................ OFF ‐ Move the CAPT stick from forward stop to aft stop. ‐ On the F/CTL SD page, check the full travel of both elevators. CAUTION: If an expected elevator movement does not occur, do not attempt any reset. Contact the maintenance. Check of the elevator control through the SEC 1: ‐ ELAC 2 pb-sw.............................................................................................................. ON ‐ SEC 1 pb-sw................................................................................................................ ON ‐ Wait 5 s ‐ BLUE PUMP OVRD pb-sw.......................................................................................... OFF ‐ Wait for hydraulic circuits depressurization. ‐ On the F/CTL SD page, check that the blue elevator actuator symbols becomes amber. ‐ Wait 5 s ‐ BLUE PUMP OVRD pb-sw.......................................................................................... ON ‐ ELAC 1 pb-sw............................................................................................................. OFF ‐ ELAC 2 pb-sw............................................................................................................. OFF ‐ Move the CAPT stick from right stop to left stop, then from forward stop to aft stop. Each stop must be applied during 3 s ‐ On the F/CTL SD page, check the correct movement of the pairs of spoilers 2, 3, and 4 and the full travel of both elevators. ‐ Move the F/O stick from right stop to left stop, then from forward stop to aft stop. Each stop must be applied during 3 s ‐ On the F/CTL SD page, check the correct movement of the pairs of spoilers 2, 3, and 4 and the full travel of both elevators. (Continued) Revision: 36 June 30, 2017

N Registration

Page: 27.67


SUBJECT

CAT

No INS

MIN REQ


27-94-01 Spoiler Elevator Computers (SEC) (Continued) CAUTION: If an expected spoiler or elevator movement does not occur, do not attempt any reset. Contact the maintenance. Return to normal configuration: ‐ YELLOW ELEC PUMP pb-sw...................................................................................... OFF ‐ BLUE PUMP OVRD pb-sw.......................................................................................... OFF ‐ ELAC 1 pb-sw.............................................................................................................. ON ‐ ELAC 2 pb-sw.............................................................................................................. ON AFTER ENGINE START Note: The F/CTL ELEV SERVO FAULT alert may be displayed on the EWD if the PTU is inhibited and only one engine is operating. This alert must disappear when the PTU or the second engine is started. IN FLIGHT If the SEC 1 and the SEC 3 fail during the flight: - Autoland is not permitted. - Maximum landing capability is CAT 1 - Disengage the AP at 500 ft RA before landing in direct law. - When the AP is disengaged with the three SECs failed, it cannot be engaged again. OPERATIONS (O) 27-94-01 -3) SEC 3 FLIGHT PREPARATION/LIMITATIONS Apply performance penalties for spoilers 1 and 2. Refer to operational procedure on item 27-64-01 for surfaces 1 and 2. DURING COCKPIT PREPARATION Deactivation of the SEC 3: ‐ SEC 3 pb-sw........................................................................................................................... OFF ‐ FLIGHT CONTROLS/SEC 3/SPLY (121VU Q19) C/B............................................................ Pull IN FLIGHT If the SEC 1 and the SEC 2 fail during the flight: - Autoland is not permitted. - Maximum landing capability is CAT 1 - Disengage the AP at 500 ft RA before landing in direct law. - When the AP is disengaged with the three SECs failed, it cannot be engaged again.


N Registration

Page: 27.68


SUBJECT

CAT

No INS

MIN REQ


27-94-01 Spoiler Elevator Computers (SEC) (Continued) MAINTENANCE (M) 27-94-01 1) and 2) SEC 1 and SEC 2 To Deactivation of the Spoiler Elevator Computer (SEC) 1 or 2 refer to Aircraft Maintenance Manual (AMM) Task number 27-94-00-040-002. MAINTENANCE (M) 27-94-01 3) SEC 3 To deactivation of the Spoiler Elevator Computer 3 (SEC) refer to Aircraft Maintenance Manual (AMM) 2794-00-040-802.


N Registration

Page: 27.69


SUBJECT

CAT

No INS

MIN REQ

C

3

2

One may be inoperative provided associated SEC caution operates normally.

C

3

0

May be inoperative provided: a) FWCs operate normally, and b) ECAM SEC indications operate normally.

C

3

0


27-94-02 SEC p.b. Switch 1) FAULT Lights

2) OFF Lights


N Registration

Page: 27.70


SUBJECT

27-94-03 SEC Indication on ECAM F/CTL Page.


CAT

No INS

MIN REQ


C

3

0

May be inoperative provided SEC p.b switch fault light system operates normally.

N Registration

Page: 27.71


SUBJECT

27-95-01 Flight Control Data Concentrators (Without Mod. 35542)

CAT

No INS

MIN REQ

C

2

1

(With Mod. 35542)

REMARKS OR EXCEPTIONS (O) FCDC 2 may be inoperative.


OPERATIONS (O) 27-95-01 C/B FLIGHT CONTROLS/FCDC2/SPLY (121VU Q20)


N Registration

…………………………………………PULL

Page: 27.72

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 28 FUEL ITEM 28-00

SUBJECT

CAT

No INS

MIN REQ


CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) Fault(s) Indicated by FUEL

C NOTE 1: Dispatch with this MAINT STS message displayed on ECAM is permitted without CFDS interrogation. NOTE 2: The systems are designed to be fault tolerant for a period of time given on the category column in accordance with MEL preamble information. Quantities are not required for this item while the idea is to allow these fault indication.


N Registration

Page: 28.1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 28 FUEL ITEM

SUBJECT

CAT

No INS

MIN REQ

C

2

0

(O) One or both may be damaged or missing provided the inner tank fuel temperature is monitored.

C

2

0

(M) (O) One or both may be damaged or missing provided: a) The associated transfer valves are latched in open position and b) The associated transfer valves are verified in the open position prior to each flight.


28-12-01 Overpressure Protectors 1) A318/A319/A320 a) Between Inner and Outer Tank.

NOTE: After Transfer Valves have been electrically latched open; any refueling, repowering or opening of the refuel door will cause the Transfer Valves to unlatch and close requiring that the Transfer Valves be electrically latched open again. b) In Vent Surge Tank

C

2

0

c) In Additional Center Tank(s) (With ACT(s))

(M)(O) May be damage or missing. Not applicable to Avianca fleet. Avianca A318/A319/A320 does not have Additional Center Tank.

2) A321 a) In Vent Surge Tank

C

2

0

b) In Additional Center Tank(s) (With ACT(s))

C

1

0

(M)(O) May be damaged or missing. (M) (O) May be open provided:

C

1

0

C

1

0

a) Manual transfer from ACT(s) to center tank is verified to operate normally, and b) ACT(s) fuel quantity indications (both FQI if both ACTs installed) and center tank fuel quantity indications are operative on ECAM FUEL page. May be open provided there is no fuel in any ACT. (M)(O) May be open provided: a) Fuel in any ACT is considered unusable and included in ZFW and C.G. calculations, and b) ACT transfer valve is secured closed.

OPERATIONS (O) 28-12-01 -1) Between inner and outer cell The dispatch condition results in an unusual distribution of fuel quantity: outer cell of affected wing will be partially empty with transfer valves normally closed. Fuel management should be performed with care . Revision: 29 October 23, 2014

N Registration

Page: 28.2

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 28 FUEL ITEM 28-12-01

SUBJECT

CAT

No INS

MIN REQ


Overpressure Protectors (Continued)

After a long taxi or if outside air temperature is high, FUEL OUTER TK Hl TEMP caution may be displayed on ECAM E/WD. In that case, disregard the FUEL OUTER TK Hl TEMP caution and apply following procedure: - The Inner Tank Fuel Temperature during taxi and in flight is to be monitored to make sure that is decreases and remains within temperature limitations. - In the event of the Inner Tank Fuel Temperature exceeding temperature limitations, perform Hl TEMP procedure as per the operational procedure associated with MEL item 28-40-09. For fuel temperature limitations, refer to Flight Manual. OPERATIONS (O) 28-12-01 -2) In vent surge tank Lateral accelerations should be avoided in order to reduce the possibility of fuel spill during taxi and climb out. When established in cruise check that no fuel spillage occurred and that sufficient FOB is available to destination with adequate reserve. OPERATIONAL (O) 28-12-01 1) (A321) Applicable to item 1: Overpressure Protectors Between Inner and Outer tank Overpressure protectors in vent surge tank: On Ground and In Flight -Avoid Lateral acceleration in order to reduce the possibility of fuel spill during taxi and climb out. -In cruise check that not fuel spillage occurred -Check that the FOB is sufficient to reach the destination with the adequate reserve. OPERATIONAL (O) 28-12-01 2) (A321) Applicable to item 2: Overpressure Protectors In Additional Center Tank(s) (With ACT (s)), first set of provisos Refer to operational procedure of MEL item 28-28-01. Applicable to item 2: Overpressure Protectors In Additional Center Tank(s) (With ACT (s)), third set of provisos Refer to Operational Procedure of MEL item 28-28-01 MAINTENACE (M) 28-12-01 -1) a) Refer to Aircraft Maintenance Manual (AMM) Task Number 28-12-00-040-003. MAINTENACE (M) 28-12-01 -1 b) and -2) a) -Refer to Aircraft Maintenance Manual (AMM) Task Number 28-12-00-040-802-A for De-activation of the Overpressure Protector. -Refer to Aircraft Maintenance Manual (AMM) Task Number 28-12-00-440-802-A for Re-activation of the Overpressure Protector. MAINTENANCE (M) 28-12-01 2) (A321) Applicable to item 2: Overpressure Protectors In Additional Center Tank(s) (With ACT (s)), first set of provisos Ref. to Maintenance Procedure of MEL, item 28-28-01. Note: Dispatch Concurrence required due to aircraft operation range may be affected. Applicable to item 2: Overpressure Protectors In Additional Center Tank(s) (With ACT (s)), third set of provisos Ref. to Maintenance Procedure of MEL, item 28-28-01.. Revision: 34 May 26, 2016

N Registration

Page: 28.3


SUBJECT

CAT

No INS

MIN REQ

C

2

0

(O) May be inoperative open.

C

2

0

(O) Both may be inoperative closed provided LH outer tank fuel is considered unusable.

C

2

1

(M) (O) One may be inoperative closed provided: a) The operative LH wing outer to inner tank transfer valve is latched in the open position, and b) Verify the operative LH wing outer to inner tank transfer valve is in the open position prior to each flight.


28-15-01 Outer to Inner TK Transfer Valves 1) A318/A319/A320 a) LH Wing

NOTE: After Transfer Valves have been electrically latched open; any refueling, repowering or opening of the refuel door will cause the Transfer Valves to unlatch and close requiring that the Transfer Valves be electrically latched open again.

b) RH Wing

C

2

1

(O) One may be inoperative closed provided the LH outer tank fuel is considered as unusable for flight planning.

C

2

0

(O) May be inoperative open.

C

2

0

(O) Both may be inoperative closed provided RH outer tank fuel is considered unusable.

C

2

1

(M)(O) One may be inoperative closed provided a) The operative RH wing outer to inner tank transfer valve is latched in the open position, and b) Verify the operative RH wing outer to inner tank transfer valve is in the open position prior to each flight. NOTE: After Transfer Valves have been electrically latched open; any refueling, repowering or opening of the refuel door will cause the Transfer Valves to unlatch and close requiring that the Transfer Valves be electrically latched open again.

C

2

1

(O) One may be inoperative closed provided the RH outer tank fuel is considered as unusable for flight planning.

PLACARD If valve is indicated closed: - install 28-15-01 CLOSED placard adjacent to lower ECAM display Revision: 29 October 23, 2014

N Registration

(Continued) Page: 28.4


SUBJECT

CAT

No INS

MIN REQ


28-15-01 Outer to Inner TK Transfer Valves (A318/A319/A320) (Continued) If valve is indicated open: - install 28-15-01 OPEN placard adjacent to lower ECAM display. OPERATIONS (O) 28-15-01 A) LH WING First and Third proviso The dispatch condition results in an unusual distribution of fuel quantity: outer tank of affected wing will not be full with inner tank not empty. Continuous Transfer of fuel between Outer and Inner tank will be present. Second and Fourth provisos Flight preparation: Notify Dispatch The fuel in affected outer tank should be considered as unusable for the flight planning. B) RH WING First and Third proviso The dispatch conditions results in unusual distribution of fuel quantity: outer tank of affected wing will not be full with inner tank not empty. Continuous Transfer of fuel between Outer and Inner tank will be present. Second and Fourth provisos Flight preparation: Notify Dispatch The fuel in affected outer tank should be considered as unusable for the flight planning. MAINTENANCE (M) 28-15-01 LH Wing Refer to Aircraft Maintenance Manual (AMM) 28-15-00-040-001-A MAINTENANCE (M) 28-15-01 RH Wing Refer to Aircraft Maintenance Manual (AMM) 28-15-00-040-002

Revision: 35 November 24, 2016

N Registration

Page: 28.5


SUBJECT

CAT

No INS

MIN REQ

C

1

0


28-20-01 Automatic Fuel Feed System.

Feed System for A318/A319/A320 without Mod. 154327/MP J3527 a) With Mod. 37508/MP J2832 b) Without Mod. 37508/MP J2832

(O) May be inoperative provided alternate procedures are established and used. Not applicable to Avianca fleet. Avianca fleet has incorporated Mod 37508.

OPERATIONS (O) 28-20-01 a) ON GROUND: If the center tank is empty for the flight: FUEL MODE SEL CTR TK PUMP 1 AND 2

……………………………………………………………MAN ……………………………………………………………OFF

If the center tank is not empty apply following procedure: Before engines start: FUEL MODE SEL ……………………………………………………………MAN 3 minutes after engines start: CTR TK PUMP 1 AND 2 ……………………………………………………………OFF IN FLIGHT: If the center tank is not empty for the flight: After slats retraction and when fuel in one wing less than 5000 kg (11000 Ib): CTR TK PUMP 1 AND 2 ……………………………………………………………..ON When CTR TK PUMP LO PR warning illuminates: CTR TK PUMP 1 AND 2 …………………………………………………………….OFF


N Registration

Page: 28.6


SUBJECT

CAT

No INS

MIN REQ

C

4

3

One pump may be inoperative provided JP4/Jet B is not used.

C

4

3

(M) One pump 2 may be inoperative when JP4/Jet B is used provided: a) Prior to each flight, fuel return valve is verified to operate normally, and b) Takeoff ECAM fuel temperature is less than 30 degrees C.

C

4

3

One pump may be inoperative provided JP4/Jet B is not used.

C

4

3

One pump 2LH or 2RH may be inoperative when JP4/Jet B is used provided takeoff fuel temperature is less than 30 degrees C.


28-21-01 Wing Tank Pumps (Aircraft fitted with Mod. 36387/MP J2487 or Aircraft not specified in Service Bulletin A320-28-1102) 1) CFM Engines

2) IAE Engines

MAINTENANCE (M) 28-21-01 Refer to Aircraft Maintenance Manual (AMM) 28-21-00-040-001


N Registration

Page: 28.7


SUBJECT

28-21-02 Center Tank Systems 1) Pumps a) A318/A319/A320 Without ACT and without Mod. 154327/MP J3527

CAT

No INS

MIN REQ

C

2

1


Applicable to A318/A319/A320 only. (O) One may be inoperative provided (when center tank fuel is required) a suitable alternate airport exists within range of wing tanks fuel loading.

C

2

0

(O) May be inoperative provided: a) Center tank pumps remain OFF, and b) Center tank remains empty.

C

2

0

(O) May be inoperative provided fuel in center tank is considered unusable, and is included in ZFW and C.G. calculations.

b) A319/A320 With ACT(s) and without Mod. 154327/MP J3527

Not applicable to Avianca Fleet. Avianca A319/A320 does not have Additional Center Tank.

2) Transfer Valves a) A321 without ACT or A319/A320 without ACT and with Mod. 154327/MP J3527

C

2

1

Applicable to N728AV, N740AV, N741AV, N742AV, N743AV, N745AV, N748AV, N750AV, N751AV, N753AV, N755AV, N764AV and N765AV. (O) One may be inoperative in closed position provided (when center tank fuel is required) a suitable alternate airport exists within range of wing tanks fuel loading.

b) A321 with ACT(s) or A319/A320 with ACT(s) and with Mod. 154327/MP J3527

C

2

0

(O) May be inoperative in closed position provided center tank remains empty.

C

2

0

(O) May be inoperative in closed position provided fuel in center tank is considered unusable and is included in ZFW and C.G. calculations.

C

2

1

(O) May be inoperative in open position provided center tank remains empty.

C

2

1

Applicable to A321 only. (O) One may be inoperative in closed position provided (when center tank fuel is required) a suitable alternate airport exists within range of wing tanks fuel loading.

C

2

0

(M)(O) May be inoperative in closed position provided center tank and ACTs remain empty.


N Registration

Page: 28.8


SUBJECT

CAT

No INS

MIN REQ


C

2

0

(M)(O) May be inoperative in closed position provided: a) Fuel in center tank and ACTs is considered unusable and is included in ZFW and C.G. calculations, and b) ACT transfer valve is secured closed.

C

2

0

(M)(O) May be inoperative in open position provided center tank and ACTs remain empty.

C

2

0

(M)(O) May be inoperative in open position provided: a) Center tank remains empty, b) Fuel in any ACT is considered unusable and is included in ZFW, and C.G. calculations, and c) ACT transfer valve is secured closed.

Center Tank Systems (Continued) b) A321 with ACT(s) or A319/A320 with ACT(s) and with Mod. 154327/MP J3527 (Continued)

OPERATIONS (O) 28-21-02 1) a) FLIGHT PREPARATION/LIMITATIONS In the case of dispatch with fuel in the center tank, the remaining center tank pump failure must be considered for the flight planning. Operator has to ensure that, from any point of the first part of the route where the center tank is not empty the aircraft may reach a suitable airport considering the fuel quantity (FQ) contained in the center tank as definitely not usable for the flight planning (as a consequence of the failure of the remaining center tank pump). DURING COCKPIT PREPARATION ‐ X FEED pb-sw.............................................................................................................CHECK OFF ‐ Affected CTR TK PUMP pb-sw.............................................................................................. OFF ‐ Operative CTR TK PUMP pb-sw............................................................................................OFF IN FLIGHT If the fuel quantity in the center tank is less than 200 kg (440 lb): Operative CTR TK PUMP pb-sw........................................................................... MAINTAIN OFF

(Continued) Revision: 35 November 24, 2016

N Registration

Page: 28.9


SUBJECT

CAT

No INS

MIN REQ


28-21-02 Center Tank Systems (Continued) If the fuel quantity in the center tank is more than 200 kg (440 lb): The fuel in the center tank can be completely used if the operative center tank pump does not fail before the center tank is empty. If the operative center tank pump fails before the center tank is empty, consider the fuel quantity remaining and the time to destination to decide either to continue the flight or to divert. When the fuel quantity in one wing inner tank is less than 4 500 kg (10 000 lb): Operative CTR TK PUMP pb-sw......................................................................................ON X FEED pb-sw..................................................................................................................ON When the fuel quantity in one wing inner tank increases above 5 500 kg (12 000 lb): X FEED pb-sw.................................................................................................................. OFF Operative CTR TK PUMP pb-sw....................................................................................OFF Note: Repeat the previous two steps as many times as necessary until the center tank is empty. The operative center tank pump will switch off automatically When the fuel quantity in the center tank is less than 250 kg (550 lb): X FEED pb-sw.................................................................................................................. OFF OPERATIONAL PROCEDURE (O) 28-21-02 a) Second and third set of provisos Flight Preparation/Limitations: CTR TK PUMP 1 and 2 pb-sw ……………………………………………………………….OFF OPERATIONAL PROCEDURE (O) 28-21-02 2) a) all provisos IN FLIGHT ‐ Disregard the FUEL CTR L(R) XFR FAULT alert displayed on the EWD. ‐ MODE SEL pb-sw...................................................................................................................Auto ‐ Operative CTR TK L(R) XFR pb-sw......................................................................................... On ‐ Affected CTR TK L(R) XFR pb-sw......................................................................................... OFF When differences between fuel quantities in two wings is above 1 500 kg (3 300 lb): Monitor the fuel imbalance.

Note: Apply the FUEL IMBALANCE FCOM procedure as required provided that no fuel leak is suspected. Refer to FCOM/PRO-ABN-28 FUEL IMBALANCE. (Continued)


N Registration

Page: 28.10


SUBJECT

CAT

No INS

MIN REQ


28-21-02 Center Tank Systems (Continued) OPERATIONAL PROCEDURE (A321) Applicable to item 2: Transfer Valves, all set of provisos In Flight Disregard the FUEL L(R) XFR VALVE FAULT alert displayed on the EWD MODE SEL pb-sw …………………………………………………………………………AUTO Operative CTR TK L(R) XFR pb-sw …………………………………….……………...ON Affected CTR TK L(R) XFR pb-sw ……………………………………………………….OFF When difference between fuel quantities in two wings is above 1500 kg (3300 lb): Monitor Fuel imbalance. Note: apply the FUEL IMBALANCE FCOM procedure as required provided that no fuel leak is suspected. Refer to FCOM/PRO-ABN-28 FUEL IMBALANCE Until the fuel is balanced: L(R) TK PUMPS (on the lighter side) ………………………………………………………OFF MAINTENANCE (M) 28-21-01 (A321) Refer to Maintenance Procedure of MEL item 28-28-01


N Registration

Page: 28.11


SUBJECT

28-21-03 Wing Tank Pump Sequence Valves (A318/A319/A320) without Mod. 154327/MP J3527

CAT

No INS

MIN REQ

C

4

3

REMARKS OR EXCEPTIONS Applicable to A318/A319/A320 only (O) One may be inoperative provided the associated pump is switched off when center tank is feeding.

OPERATIONS (O) 28-21-03 1- Turn associated pump OFF when feeding from center tank. 2- Turn associated pump ON when center tank is empty. NOTE: For take-off and landing turn the associated wing fuel pump ON, and turn it OFF after slats retraction.


N Registration

Page: 28.12


SUBJECT

28-23-01 CROSSFEED p.b. Switch ON Light


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Incorporated into revised item28-23-02.

N Registration

Page: 28.13


CAT

No INS

MIN REQ

1) ON Light

C

1

O

May be inoperative provided X FEED indication on ECAM FUEL page operates normally.

2) OPEN Light

C

1

0

May be inoperative provided X FEED indication on ECAM FUEL page operates normally.

SUBJECT


28-23-02 CROSSFEED p.b. Switch


N Registration

Page: 28.14

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 28 FUEL SUBJECT

CAT

No INS

28-24-01 Engine LP Fuel Valve Electrical Motor (with Mod. 25537)

C

4

ITEM

MIN REQ


2

(M) One may be inoperative on each valve provided: a) Affected valve motor is deactivated, and b) Remaining valve motor is checked operative.

MAINTENANCE (M) 28-24-01 To Functional Test of Engine LP Fuel Valve with a Defective Actuator Motor refer to AMM 28-24-00-040002.


N Registration

Page: 28.15


SUBJECT

28-25-01 Fuel Quantity Preselector System


CAT

No INS

MIN REQ

C

1

0

N Registration


Page: 28.16


CAT

No INS

28-25-02 Fuel Quantity Indicator (Refueling Panel)

C

1

ITEM

MIN REQ

0

REMARKS OR EXCEPTIONS (M) One or more indications may be inoperative provided alternate means of refueling are used.

MAINTENANCE (M) 28-25-02 Refer to Aircraft Maintenance Manual (AMM) Task Number 28-25-00-040-007, Fuel Quantity Panel System (Refueling).


N Registration

Page: 28.17


SUBJECT

CAT

No INS

MIN REQ

C

1

0


28-25-03 High Level Fuel Detection System 1) A318/A319/A320/A321 without ACT

May be inoperative provided an acceptable means of monitoring fuel loading is used.

2) A319/A320 with ACT a) Inner Tank

Not applicable to Avianca fleet Avianca A319/A320 does not have Additional Center Tank.

b) Center Tank

Not applicable to Avianca fleet. Avianca A319/A320 does not have Additional Center Tank.

c) Additional Center Tank(s)

Not applicable to Avianca fleet. Avianca A319/A320 does not have Additional Center Tank.

3) A321 with ACT(s) a) Wing Tank

C

1

0

May be inoperative provided an acceptable means of monitoring fuel loading is used.

b) Center Tank

C

1

0

(M)(O) May be inoperative provided: a) An acceptable means of monitoring fuel loading is used, b) Manual transfer from ACT(s) to center tank is verified to operate normally, and c) ACT(s) and center fuel indications on ECAM FUEL page are operative.

C

1

0

May be inoperative provided: a) An acceptable means of monitoring fuel loading is used, and b) There is no fuel in any ACT.

C

1

0

C

1

0

(M)(O) May be inoperative provided: a) An acceptable means of monitoring fuel loading is used, b) Fuel in any ACT is considered unusable and included in ZFW and C.G. calculations, and c) ACT transfer valve is secured closed. May be inoperative provided an acceptable means of monitoring fuel loading is used.

3) Additional Center Tank(s)

(Continued) Revision: 35 November 24, 2016

N Registration

Page: 28.18


SUBJECT

CAT

No INS

MIN REQ


28-25-03 High Level Fuel Detection System (A318/A319/A320/A321 without ACT) (Continued) OPERATIONAL (O) 28-25-03 2) First set of provisos (Only for A321) DURING COCKPIT PREPARATION 1. The refuel panel door must be open to check the operation of the manual transfer on the ground using the FUEL SD page. Establish ground communications and ensure that the refuel panel door is open during following check and closed after the check is done. 2. The manual transfer may be performed only if the center tank is not full (center tank high level sensor dry). If the center tank is full, the high level sensor may be overridden by keeping pressed in the HI LVL pb test of the refuel panel. When the high level sensor is overridden, take care to not overfill the center tank. Otherwise, fuel may spill out from the surge tanks. ‐ ACT pb-sw..............................................................................................................................FWD ‐ On the FUEL SD page, check that the fuel is transferred from one ACT (from ACT 2 if ACT 2 is installed and not empty) to the center tank. ‐ ACT pb-sw............................................................................................................................AUTO 30 MIN AFTER TAKEOFF ‐ ACT pb-sw..............................................................................................................................FWD ‐ On the FUEL SD page, check that the fuel is transferred from the ACTs to the center tank. ‐ If necessary perform a descent to FL 270. When ACT (both ACTs if two ACTs installed) is empty: ACT pb-sw..........................................................................................................................AUTO OPERATIONAL (O) 28-25-03 2) Third set of provisos (Only for A321) ON GROUND OR IN FLIGHT When there is less than 3 000 kg (6 700 lb) of fuel in the center tank: Disregard and clear the FUEL ACT XFR FAULT alert displayed on the EWD. MAINTENANCE (M) 28-25-03 2) First set of proviso (Only for A321) Refer to Maintenance Procedure of MEL, item 28-28-01 MAINTENANCE (M) 28-25-03 2) Third set of proviso (Only for A321) Refer to Maintenance Procedure of MEL, item 28-28-01


N Registration

Page: 28.19


SUBJECT

28-25-04 Refuel Valves

CAT

No INS

MIN REQ

C

3

0

REMARKS OR EXCEPTIONS (M) May be inoperative provided alternate procedures are developed and used.

MAINTENANCE (M) 28-25-04 Refuel Valve - Refuel Procedure Using Manual Plunger Override refer to AMM 28-25-00-040-005


N Registration

Page: 28.20


CAT

No INS

28-25-05 Transfer Defuel Valve

C

1

ITEM

MIN REQ

0

REMARKS OR EXCEPTIONS (M) May be inoperative provided valve is secured in the closed position.

MAINTENANCE (M) 28-25-05 To Deactivation of the Transfer Defuel Valve refer to AMM 28-25-00-040-004


N Registration

Page: 28.21


CAT

No INS

MIN REQ


a) Aircraft without Mod 20164/MP J0022 or 22760/MP J0835)

C

1

0

Applicable to N195AV, N454AV, N477AV, N519AV, N536AV, N538AV, N557AV, N562AV, N567AV, N599AV, N603AV, N632AV, N690AV, N694AV, N695AV, N696AV, N723AV, N724AV, N725AV, N726AV, N728AV, N729AV, N730AV, N740AV, N741AV, N742AV, N743AV, N744AV, N745AV, N746AV, N748AV, N750AV, N751AV, N753AV, N755AV, N759AV, N761AV, N763AV, N764AV, N765AV, N789AV, N821AV, N862AV and N939AV. (M) May be inoperative provided alternate procedures are established and used.

b) Aircraft with Mod 20164/MP J0022 or 22760/MP J0835)

C

1

0

Applicable to A318, A319, A320 and A321 fleet except to N195AV, N454AV, N477AV, N519AV, N536AV, N538AV, N557AV, N562AV, N567AV, N599AV, N603AV, N632AV, N690AV, N694AV, N695AV, N696AV, N723AV, N724AV, N725AV, N726AV, N728AV, N729AV, N730AV, N740AV, N741AV, N742AV, N743AV, N744AV, N745AV, N746AV, N748AV, N750AV, N751AV, N753AV, N755AV, N759AV, N761AV, N763AV, N764AV, N765AV, N789AV, N821AV, N862AV and N939AV. (O) May be inoperative provided that the cockpit fuel quantity pre-selector is operative.

C

1

0

(M) May be inoperative provided alternate procedures are established and used.

D

1

0

Applicable to A318, A319, A320 and A321 fleet except to N195AV, N454AV, N477AV, N519AV, N536AV, N538AV, N557AV, N562AV, N567AV, N599AV, N603AV, N632AV, N690AV, N694AV, N695AV, N696AV, N723AV, N724AV, N725AV, N726AV, N728AV, N729AV, N730AV, N740AV, N741AV, N742AV, N743AV, N744AV, N745AV, N746AV, N748AV, N750AV, N751AV, N753AV, N755AV, N759AV, N761AV, N763AV, N764AV, N765AV, N789AV, N821AV, N862AV and N939AV.

SUBJECT

28-25-06 Refuel/Defuel Control Panel 1) Exterior Control Panel

2) Cockpit Control Panel (Aircraft with Mod 20164/MP J0022 or 22760/MP J0835)

PLACARD Install 28-25-06 INOP placard adjacent to Exterior Control Panel or Cockpit Control Panel as required. OPERATIONAL (O) 28-25-06 1) The cockpit fuel quantity preselector shall be used for refueling operations, contact to maintenance staff or dispatch to preselected total fuel quantity. MAINTENANCE (M) 28-25-06 To Refuel/Defuel Control Panel - Manual Refuel refer to AMM task 28-25-00-040-008. Revision: 36 June 30, 2017

N Registration

Page: 28.22


SUBJECT

28-28-01 Auto Transfer System Additional Center Tank(s) (ACT) (applicable to A321 Fleet Only)

CAT

No INS

MIN REQ

C

1

0

May be inoperative provided there is no fuel in any ACT.

C

1

0

C

1

0

(M)(O) May be inoperative provided: a) Fuel in any ACT is considered unusable and included in ZFW and C.G. calculations, and b) ACT transfer valve is secured closed. (O) May be inoperative provided: a) Manual transfer from ACT(s) to center tank is checked before each flight, and b) ACT(s) and center tank fuel quantity indications on ECAM FUEL page are operative.


OPERATIONAL (O) 28-28-01 2) On Ground Or In Flight When there is less than 3 000 kg (6 700 lb) of fuel in the center tank: Disregard and clear the FUEL ACT XFR FAULT alert displayed on the EWD. OPERATIONAL (O) 28-28-01 3) During Cockpit Preparation 1. The refuel panel door must be open to check the operation of the manual transfer on the ground using the FUEL SD page. Establish ground communications and ensure that the refuel panel door is open during following check and closed after the check is done. 2. The manual transfer may be performed only if the center tank is not full (center tank high level sensor dry). If the center tank is full, the high level sensor may be overridden by keeping pressed in the HI LVL pb test of the refuel panel. When the high level sensor is overridden, take care to not overfill the center tank. Otherwise, fuel may spill out from the surge tanks. ‐ ACT pb-sw..............................................................................................................................FWD ‐ On the FUEL SD page, check that the fuel is transferred from one ACT (from ACT 2 if ACT 2 is installed and not empty) to the center tank. ‐ ACT pb-sw............................................................................................................................AUTO 30 Min After Takeoff ‐ ACT pb-sw..............................................................................................................................FWD ‐ On the FUEL SD page, check that the fuel is transferred from the ACTs to the center tank. ‐ If necessary perform a descent to FL 270. When ACT (both ACTs if two ACTs installed) is empty: ACT pb-sw..........................................................................................................................AUTO MAINTENANCE (M) 28-28-01 2) To Auto Transfer System Additional Center Tank, refer to Aircraft Maintenance Manual (AMM) 28-28-00040-009 Revision: 35 November 24, 2016

N Registration

Page: 28.23


SUBJECT

28-28-02 Transfer Valve Additional Center Tank(s) (applicable to A321 Fleet Only)

CAT

No INS

MIN REQ

C

1

0

May be inoperative in closed position provided there is no fuel in any ACT.

C

1

0

C

1

0

(M)(O) May be inoperative in closed position provided: a) Fuel in any ACT is considered unusable and included in ZFW and C.G. calculations, and b) ACT transfer valve is secured closed. (M) May be inoperative in open position provided an alternate procedure is used for refueling ACT(s).


OPERATIONAL (O) 28-28-02 2) On Ground Or In Flight When there is less than 3 000 kg (6 700 lb) of fuel in the center tank: Disregard and clear the FUEL ACT XFR FAULT alert displayed on the EWD. MAINTENANCE (M) 28-28-02 2) Transfer Valve Additional Center Tank, refer to Aircraft Maintenance Manual (AMM) 28-28-00-040-010 MAINTENANCE (M) 28-28-02 3) Transfer Valve Additional Center Tank, refer to Aircraft Maintenance Manual (AMM) 28-28-00-040-001


N Registration

Page: 28.24


SUBJECT

28-28-03 Transfer Pump Additional Center Tank(s) (applicable to A321 Fleet Only)


CAT

No INS

MIN REQ

C

1

0

N Registration


Page: 28.25


SUBJECT

28-28-04 Air Shutoff Valve Additional Center Tank(s) (applicable to A321 Fleet Only)

CAT

No INS

MIN REQ

C

1

0

May be inoperative closed provided there is no fuel in any ACT.

C

1

0

C

1

0

(M)(O) May be inoperative closed provided: a) Fuel in any ACT is considered unusable and included in ZFW and C.G. calculations, and b) ACT transfer valve is secured closed. (O) May be inoperative closed provided: a) Manual transfer from ACT(s) to center tank is verified to operate normally, and b) ACT(s) and center tank fuel quantity indications on ECAM FUEL page are operative.


OPERATIONAL (O) 28-28-04 2) On Ground Or In Flight When there is less than 3 000 kg (6 700 lb) of fuel in the center tank: Disregard and clear the FUEL ACT XFR FAULT alert displayed on the EWD. OPERATIONAL (O) 28-28-04 3) During Cockpit Preparation 1. The refuel panel door must be open to check the operation of the manual transfer on the ground using the FUEL SD page. Establish ground communications and ensure that the refuel panel door is open during following check and closed after the check is done. 2. The manual transfer may be performed only if the center tank is not full (center tank high level sensor dry). If the center tank is full, the high level sensor may be overridden by keeping pressed in the HI LVL pb test of the refuel panel. When the high level sensor is overridden, take care to not overfill the center tank. Otherwise, fuel may spill out from the surge tanks. ‐ ACT pb-sw..............................................................................................................................FWD ‐ On the FUEL SD page, check that the fuel is transferred from one ACT (from ACT 2 if ACT 2 is installed and not empty) to the center tank. ‐ ACT pb-sw............................................................................................................................AUTO 30 Min After Takeoff ‐ ACT pb-sw..............................................................................................................................FWD ‐ On the FUEL SD page, check that the fuel is transferred from the ACTs to the center tank. ‐ If necessary perform a descent to FL 270. When ACT (both ACTs if two ACTs installed) is empty: ACT pb-sw..........................................................................................................................AUTO MAINTENANCE (M) 28-28-04

2)

To Auto Transfer System Additional Center Tank, refer to Aircraft Maintenance Manual (AMM) 28-28-00040-009 Revision: 35 November 24, 2016

N Registration

Page: 28.26


SUBJECT

28-28-05 Inward Pressure Relief Valve Additional Center Tank(s) (applicable to A321 Fleet Only)


CAT

No INS

MIN REQ


C

1

0

May be inoperative open provided there is no fuel in any ACT.

N Registration

Page: 28.27


SUBJECT

28-28-06 Vent Valve Additional Center Tank(s) (applicable to A321 Fleet Only)

OPERATIONAL (O) 28-28-06

CAT

No INS

MIN REQ

C

1

0

May be inoperative provided there is no fuel in any ACT.

C

1

0

C

1

0

(M)(O) May be inoperative provided: a) Fuel in any ACT is considered unusable and included in ZFW and C.G. calculations, and b) ACT transfer valve is secured closed. (M)(O) May be inoperative provided: a) Manual transfer from ACT(s) to center tank is verified to operate normally, b) ACT(s) and center tank fuel quantity indications on ECAM FUEL page are operative, and c) Associated ACT vent valve is secured open.


2)

On Ground Or In Flight When there is less than 3 000 kg (6 700 lb) of fuel in the center tank: Disregard and clear the FUEL ACT XFR FAULT alert displayed on the EWD. OPERATIONAL (O) 28-28-06

3)

During Cockpit Preparation 1. The refuel panel door must be open to check the operation of the manual transfer on the ground using the FUEL SD page. Establish ground communications and ensure that the refuel panel door is open during following check and closed after the check is done. 2. The manual transfer may be performed only if the center tank is not full (center tank high level sensor dry). If the center tank is full, the high level sensor may be overridden by keeping pressed in the HI LVL pb test of the refuel panel. When the high level sensor is overridden, take care to not overfill the center tank. Otherwise, fuel may spill out from the surge tanks. ‐ ACT pb-sw..............................................................................................................................FWD ‐ On the FUEL SD page, check that the fuel is transferred from one ACT (from ACT 2 if ACT 2 is installed and not empty) to the center tank. ‐ ACT pb-sw............................................................................................................................AUTO 30 Min After Takeoff ‐ ACT pb-sw..............................................................................................................................FWD ‐ On the FUEL SD page, check that the fuel is transferred from the ACTs to the center tank. ‐ If necessary perform a descent to FL 270. (Continued)


N Registration

Page: 28.28


SUBJECT

CAT

No INS

MIN REQ


Vent Valve AdditionalCenter Tank(s) (applicable to A321 Fleet Only) (Continued)

When ACT (both ACTs if two ACTs installed) is empty: ACT pb-sw..........................................................................................................................AUTO MAINTENANCE (M) 28-28-06 2) To vent valve additional center Tanks, refer to Aircraft Maintenance Manual (AMM) 28-28-00-040-011 MAINTENANCE (M) 28-28-06 3) To vent valve additional center Tanks, refer to Aircraft Maintenance Manual (AMM) 28-28-00-040-003


N Registration

Page: 28.29


SUBJECT

28-28-07 Refuel Valve Additional Center Tank(s) ) (applicable to A321 Fleet Only)

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS (M) May be inoperative in the closed position. NOTE: The (M) procedure only needs to be accomplished at each ACT re-fueling.

C

1

0

May be inoperative in open position.

MAINTENANCE (M) 28-28-07: If the refuel valve is inoperative in the closed position, the ACT can be manually refueled. Refer to AMM task 28-25-00-040-005.


N Registration

Page: 28.30


SUBJECT

CAT

No INS

MIN REQ

C

1

0

C

1

0

C

1

0


28-28-08 Inlet Valve Additional Center Tank(s) (applicable to A321 Fleet Only) 1) ACT 1

2) ACT 2


ACT 1 inlet valve may be inoperative in closed position provided there is no fuel in any ACT. (M)(O) ACT 1 inlet valve may be inoperative in closed position provided: a) Fuel in any ACT is considered unusable and included in ZFW and C.G. calculations, and b) ACT transfer valve is secured closed. (M) ACT 1 inlet valve may be inoperative in open position provided: a) ACT 2 is not installed or is empty, and b) Transfer valve is verified operative prior to each flight when ACT 1 is used. Not applicable to Avianca A321 fleet.

1) Second

On Ground Or In Flight When there is less than 3 000 kg (6 700 lb) of fuel in the center tank: Disregard and clear the FUEL ACT XFR FAULT alert displayed on the EWD. MAINTENANCE (M) 28-28-08 1) Second To Inlet Valve Additional Center Tank, refer to Aircraft Maintenance Manual (AMM) 28-28-00-040-008 MAINTENANCE (M) 28-28-08 1) Third To Inlet Valve Additional Center Tank, refer to Aircraft Maintenance Manual (AMM) 28-28-00-040-004


N Registration

Page: 28.31


CAT

No INS

MIN REQ

1) Wing

C

2

1

One may be inoperative provided all flight deck fuel quantity indicators are operative.

2) Additional Center Tank (applicable to A321 Fleet Only)

C

1

0

C

1

0

C

1

0

(M)(O) May be inoperative provided: a) Manual transfer from ACT to center tank is verified to operate normally, b) ACT(s) and center tank fuel quantity indications on ECAM FUEL page are operative, and c) There is no fuel in ACT 2. May be inoperative provided there is no fuel in any ACT. (M)(O) May be inoperative provided: a) Fuel in any ACT is considered unusable and included in ZFW and C.G. calculations, and b) ACT transfer valve is secured closed.

SUBJECT


28-40-01 Low Level Detection Systems


2) First

On Ground Or In Flight When there is less than 3 000 kg (6 700 lb) of fuel in the center tank: Disregard and clear the FUEL ACT XFR FAULT alert displayed on the EWD. OPERATIONAL (O) 28-40-01

2) Third

During Cockpit Preparation 1. The refuel panel door must be open to check the operation of the manual transfer on the ground using the FUEL SD page. Establish ground communications and ensure that the refuel panel door is open during following check and closed after the check is done. 2. The manual transfer may be performed only if the center tank is not full (center tank high level sensor dry). If the center tank is full, the high level sensor may be overridden by keeping pressed in the HI LVL pb test of the refuel panel. When the high level sensor is overridden, take care to not overfill the center tank. Otherwise, fuel may spill out from the surge tanks. ‐ ACT pb-sw..............................................................................................................................FWD ‐ On the FUEL SD page, check that the fuel is transferred from one ACT (from ACT 2 if ACT 2 is installed and not empty) to the center tank. ‐ ACT pb-sw............................................................................................................................AUTO (Continued)


N Registration

Page: 28.32


SUBJECT

CAT

No INS

MIN REQ


Low Level Detection Systems (Continued)

30 Min After Takeoff ‐ ACT pb-sw..............................................................................................................................FWD ‐ On the FUEL SD page, check that the fuel is transferred from the ACTs to the center tank. ‐ If necessary perform a descent to FL 270. When ACT (both ACTs if two ACTs installed) is empty: ACT pb-sw..........................................................................................................................AUTO MAINTENANCE (M) 28-40-01 2) First Refer to Maintenance procedure of MEL item 28-28-01 MAINTENANCE (M) 28-40-01 2) Third Refer to Maintenance procedure of MEL item 28-28-01


N Registration

Page: 28.33


SUBJECT

CAT

No INS

MIN REQ

A

2

1


28-40-02 Fuel Quantity Indicating Computer System 1) Channels A321 without MOD 155635 / MP J3702 or A319/A320 without MOD 37508 / MP J2832 or MOD 155636 / MP J3703

Except for ER operations, one may be inoperative provided: a) Low level warning system operates normally, and b) Repairs are made within two flight days.

A319 with MOD 37508 / MP J28322 and MOD 28238 / MP J19933 and without MOD 155636 / MP J3703 A321 with MOD 155635 / MP J3702 or A319/A320 with MOD 37508 / MP J2832 and MOD 155636 / MP J3703

Applicable to A321, A319, A320 except to N742AV, N743AV, N744AV, N745AV, N748AV, N750AV, N751AV, N753AV, N755AV, N759AV and N761AV

Not applicable to Avianca Fleet. Avianca fllet has not included Mod 28238.

A

2

1

Applicable to N742AV, N743AV, N744AV, N745AV, N748AV, N750AV, N751AV, N753AV, N755AV, N759AV and N761AV only (M) Except for ER operations, one may be inoperative provided: a) Low level warning system operates normally, b) Repairs are made within two flight days, and c) Alternate procedures are developed and used.

MAINTENANCE (M) 28-40-02 2) Third Refer to AMM Task 12-11-28-650-004


N Registration

Page: 28.34


CAT

No INS

MIN REQ

1) TK PUMP FAULT Lights

C

6

0

(O) May be inoperative provided associated pump is switched off when tank is empty.

2) CTR TK XFR FAULT Lights (A321 or A319/A320 with Mod. 154324/MP J3527)

C

2

0

(O) May be inoperative provided associated transfer valve is switched off when tank is empty.

SUBJECT


28-40-03 TK PUMP and CTR TK XFR FAULT Lights

OPERATIONS (O) 28-40-03 1) Set associated TANK PUMP SWITCH to OFF position when tank is empty. OPERATIONS (O) 28-40-03 2) Set associated transfer valve to OFF position when tank is empty


N Registration

Page: 28.35


CAT

No INS

MIN REQ

1) TK PUMP OFF Lights

C

6

0

May be inoperative provided corresponding pump indication is available on ECAM.

2) CTR TK XFR OFF Lights(A321 or A319/A320 with Mod. 154324/MP J3527)

C

2

0

May be inoperative provided corresponding transfer valve indication is available on ECAM.

SUBJECT


28-40-04 TK PUMP and CTR TK XFR OFF Lights


N Registration

Page: 28.36


SUBJECT

CAT

No INS

MIN REQ

C

1

0


28-40-05 Fuel Transfer Control 1) MODE SEL FAULT Light a) A318 or A319/A320 without Mod. 154327/MP J3527

Applicable to N195AV, N281AV N345AV, N398AV, N401AV, N411AV, N426AV, N446AV, N451AV, N454AV, N481AV, N519AV, N536AV, N538AV, N557AV, N562AV, N599AV, N632AV, N664AV, N690AV, N691AV, N695AV, N723AV, N724AV, N726AV, N730AV, N789AV, N821AV, N862AV, N939AV, N980AV, N992AV, N284AV, N416AV, N422AV, N477AV, N567AV, N603AV, N647AV, N694AV, N763AV and N961AV (O) May be inoperative provided all tank pump indications on ECAM FUEL page are operative.

b) A321 or A319/A320 with Mod. 154327/MP J3527

C

1

0

Applicable to all A321 N741AV, N745AV, N751AV, N748AV, N753AV, N750AV, N728AV, N755AV, N740AV, N764AV, N742AV, N765AV and N743AV May be inoperative provided all wing tank pumps and center tank transfer valves indications on ECAM FUEL page are operative.

2) ACT p.b. Switch Additional Center Tank(if installed) (applicable to A321 Fleet Only) a) FAULT Light

C

1

0

b) FWD Light

C

1

0

(O) May be inoperative provided ACT and center tank fuel quantity indications on ECAM FUEL page are operative.

OPERATIONS (O) 28-40-05 1) After Engine Start If there is fuel in the center tank and with the slats retracted: On the FUEL SD page, check that the center tank pumps indications are in line.


N Registration

Page: 28.37


SUBJECT

CAT

No INS

MIN REQ


28-40-05 Fuel transfer Control (Continued) With the slats extended: On the FUEL SD page, check that the center tank pumps indications are cross line. After Takeoff If there is fuel in the center tank and with the slats retracted: On the FUEL SD page, check that the center tank pumps indications are in line. OPERATIONS (O) 28-40-05 2) IN FLIGHT If a manual transfer from the ACT to the CTR tank is necessary: ‐ Refer to FCOM/PRO-ABN-28 FUEL ACT XFR FAULT (If Installed). ‐ On the FUEL SD page, monitor the fuel transfer.


N Registration

Page: 28.38


SUBJECT

CAT

No INS

MIN REQ

C

6

0


28-40-06 ECAM FUEL PAGE Indications 1) A318/A319/A320) a) Tank Pumps i) A318 or A319/A320 without Mod. 154324/MP J3527 ii) Wing Tank Pumps and Center Tank Transfer Valves (A319/A320 with Mod. 154324/MP J3527)

Applicable to A318/A319/A320 only Not applicable to Avianca fleet Modification 154324 is not embodied in Avianca fleet

b) APU LP Valve

C

1

0

(M)(O)May be inoperative provided: a) Valve is secured closed, and b) APU is not used.

c) Cross Feed

C

1

0

(M)May be inoperative provided operation of the cross feed valve is verified before first flight of each day and for ER operations, is verified before each flight.

d) Transfer Valves

C

2

0

(M)(O)May be inoperative provided: a) Associated inner and outer cells fuel quantity indicators are operative, and b) Transfer valve operation is verified before each departure.

e) Fuel Temperature

C

4

2

One in each wing, or both in one wing may be inoperative.

f) Fuel On Board

C

1

0

May be inoperative provided: a) Associated indication is available on the MCDU, and b) Fuel Used indications operate normally.

g) Fuel Quantity Indications(All Tanks)

D

4

0

(O)The last two digits may be displayed dashed (degraded mode) provided the loss of accuracy is accounted for in fuel planning. NOTE 1: Fuel quantity is considered operative. NOTE 2: Fuel On Board display will also be in degraded (dashed) mode.

h) Fuel Quantity Outer Tank


C

2

1

(M)One may be inoperative provided: a) Fuel quantity in associated tank is verified after each refueling by manual magnetic indicators or by corresponding fuel quantity indicator on refuel/defuel panel, b) Associated fuel used indicator operates normally, and c) Associated inner tank indications is operative. (Continued)

N Registration

Page: 28.39


SUBJECT

CAT

No INS

MIN REQ


C

2

1

(M)One may be inoperative provided: a) High level fuel detection system is verified operative before refueling the aircraft, b) Alternate procedure is used for refueling the aircraft, c) Associated fuel used indicator operates normally, and d) Associated inner tank indication is operative.

B

2

1

(M)One may be inoperative provided: a) Fuel quantity in associated tank is verified after each refueling by manual magnetic indicators or by corresponding fuel quantity indicator on refuel/defuel panel, and b) Associated fuel used indicator operates normally.

B

2

1

(M)One may be inoperative provided: a) High level fuel detection system is verified operative before refueling the aircraft, b) Alternate procedure is used for refueling the aircraft, and c) Associated fuel used indicator operates normally.

C

2

1

(M)One may be inoperative provided: a) Fuel quantity in associated tank is verified after each refueling by manual magnetic indicators, or by corresponding fuel quantity indicator on refuel/defuel panel b) Associated fuel used indicator operates normally, and c) Associated outer tank indication is operative.

28-40-06 ECAM FUEL PAGE Indications (Continued) h) Fuel Quantity Outer Tank (Continued)

i) Fuel Quantity Inner Tank

(Continued)


N Registration

Page: 28.40


SUBJECT

CAT

No INS

MIN REQ

B

2

1

(M)One may be inoperative provided: a) Fuel quantity in associated tank is verified after each refueling by manual magnetic indicator, or by corresponding fuel quantity indicator on refuel/defuel panel, and b) Associated fuel used indicator operates normally.

C

1

0

(M)May be inoperative provided: a) Fuel quantity in associated tank is verified after each refueling, b) All wing tank quantity indicators operate normally, and c) Both fuel used indicators operate normally. OR

C

1

0

May be inoperative provided the tank remains empty.

C

1

0

May be inoperative provided fuel is considered unusable and is included in computing ZFW and C.G. calculations.


28-40-06 ECAM FUEL PAGE Indications (Continued) i) Fuel Quantity Inner Tank (Continued)

j) Fuel Quantity Center Tank i) A318/A319/A320 Without ACT

ii) A319/A320 With ACT(s)


k) Fuel Quantity Additional Center Tank(s) (A319/ A320 With ACT(s))


l) ACT to CTR Tank Transfer Indication (Arrow) Additional Center Tank(A319/A320 With ACT(s))



N Registration

Page: 28.41


CAT

No INS

MIN REQ

m) Engine LP Valve Indication

C

2

0

(M) May be inoperative provided associated LP valve(s) is checked operative before each flight.

n) FUEL FLOW 1+2 (With MOD 30368/MP P6578)

C

1

0

May be inoperative.

o) FUEL USED

C

2

0

May be inoperative provided associated fuel used indication on ENG SD page is considered inoperative.

p) FUEL USED 1+2 (with MP P7092)

C

1

0

May be inoperative.

a) Wing Tank Pumps and Center Tank Transfer Valves

C

6

0

b) APU LP Valve

C

1

0

(M)(O) May be inoperative provided: a) Valve is secured closed, and b) APU is not used.

c) Cross Feed

C

1

0

(M) May be inoperative provided operation of the cross feed valve is verified before first flight of each day and for ER operations, is verified before each flight.

d) Fuel Temperature

C

2

1

One may be inoperative.

e) Fuel On Board

C

1

0


f) Fuel Quantity Wing Tank

C

2

1

(M) One may be inoperative provided: a) Fuel quantity in associated tank is verified after each refueling, and b) Associated fuel used indicator operates normally.

SUBJECT


28-40-06 ECAM FUEL PAGE Indications (Continued)

2) A321

(Continued)


N Registration

Page: 28.42


SUBJECT

CAT

No INS

MIN REQ


D

4

0

(O) The last two digits may be displayed dashed (degraded Mode) provided the loss of accuracy is accounted for in fuel planning.

28-40-06 ECAM FUEL PAGE Indications (Continued) g) Fuel Quantity Indications (All Tanks)

NOTE 1: Fuel quantity is considered operative. NOTE 2: Fuel On Board display will also be in degraded (dashed) Mode. h) Fuel Quantity Center i)

Tank (A321 Without ACT)

ii) A321 With ACT(s))

Not applicable by make and model.

C

1

0

(M)(O) May be inoperative provided: a) Fuel quantity in center tank is verified after each refueling, b) All wing tank and ACT quantity indicators are operative, c) Both fuel used indicators operate normally, and d) Forward transfer from ACT(s) to center tank is monitored during flight.

C

1

0

May be inoperative provided: a) Center tank remains empty or fuel is considered unusable, and is included in ZFW and C.G. calculations, and b) There is no fuel in any ACT.

C

1

0

(M)(O) May be inoperative provided: a) Center tank remains empty or fuel is considered unusable, and is included in ZFW and C.G. calculations, and b) Fuel in any ACT is considered unusable and included in ZFW and C.G. calculations, and c) The ACT transfer valve is secured closed.

NOTE: This failure will result in inhibition or erroneous triggering of the ECAM caution FUEL ACT XFR FAULT while automatic transfer is still operative. (Continued)


N Registration

Page: 28.43


SUBJECT

CAT

No INS

MIN REQ

C

1

0

(M)(O) One may be inoperative provided: a) All wing tanks, center tank and other ACT fuel quantity indicators (if installed) are operative, b) Both fuel used indicators operate normally, c) Forward transfer from ACT(s) to center tank is monitored during flight, and d) Tank is serviced with a known quantity.

C

1

0

(M) May be inoperative provided ACT(s) is verified empty after each refueling.


28-40-06 ECAM FUEL PAGE Indications (Continued) i) Fuel Quantity Additional Center Tank(s) i)

A321 With ACT(s)

NOTE: This failure will result in inhibition or erroneous display of the ECAM caution FUEL ACT XFR FAULT. j) ACT to CTR Tank Transfer Indication (Arrow) Additional Center Tank i)

A321 with ACT(s)

C

1

0

May be inoperative provided ACT(s) and center tank fuel quantity indications on ECAM FUEL page are operative.

k) Engine LP Valve Indication

C

2

0

(M) May be inoperative provided associated LP valve(s) is checked operative before each flight.

l) FUEL FLOW 1+2 with MOD 30368/ MP P6578

C

1

0

May be inoperative.

m) FUEL USED

C

1

0

May be inoperative provided associated fuel used indication on ENG SD page is considered inoperative.

n) FUEL FLOW 1+2 with MP P7092

C

1

0

May be inoperative.

(Continued)


N Registration

Page: 28.44


SUBJECT

CAT

No INS

MIN REQ


28-40-06 ECAM FUEL PAGE Indications (Continued) OPERATIONS (O) 28-40-06 -b) Ensure that the APU LP Valve is secured in close position. Consider APU INOP. Notify Dispatch. OPERATIONS (O) 28-40-06 -d) Transfer Valve Indication When any inner cell fuel quantity reaches 750 kg (1650 Ib), check associated outer cell transfer on ECAM fuel page. OPERATIONS (O) 28-40-06 -g) Fuel Quantity Indication If, on upper ECAM E/WD, the FOB indication is displayed with two dashes across the last two digits, the FQI is in degraded mode. In this case, the ECAM FUEL page must be called on ECAM lower display to determine which tank is affected. The resulting loss of accuracy must be taken into account by using the two following parameters :  . Fq : The extra fuel quantity to be loaded.  . W : The weight to be added to the total fuel weight for TOW calculation only. Fq and W parameters are given as follows :

-

Preselect the fuel quantity required for the mission :  .Fm When the auto refuel stops, enter the table and determine Fq and W values for the affected tank. (Continued)


N Registration

Page: 28.45


SUBJECT

CAT

No INS

MIN REQ


28-40-06 ECAM FUEL PAGE Indications (Continued) -

The auto refuel must be started again with the new preselected quantity which corresponds to the total FOB : . Fm + Fq

Note: If all tanks reach high level before having loaded the complete Fq value, this shows that all tanks are volumetrically full but the necessary fuel mass for the mission is not guaranteed since the fuel quantity indication varies with fuel density. Therefore the mission or the aircraft load must be amended to match the minimum fuel quantity known to be onboard. -

-When the auto refuel stops again, the FOB value to be considered for TOW calculation is: . FOB = Fm + Fq + W

Note: 1) If all tanks reach high level before having loaded Fq value, then the extra fuel quantity known to be onboard is : . - Fq* with : Fq* < Fq and, the FOB value to be considered for TOW calculation is : . FOB = Fm + Fq* + W - If the resulting TOW is higher than the MTOW, the aircraft load must be reduced. a) Outer Cell Refer to FCOM/PER-LOD-FUL-FUEL b) Inner Cell Refer to FCOM/PER-LOD-FUL-FUEL c) Center Tank Refer to FCOM/PER-LOD-FUL-FUEL ECAM FUEL PAGE INDICATIONS OPERATIONAL PROCEDURES FOR A321 OPERATIONAL PROCEDURE 28-40-06 -b) (A321) Ensure that the APU LP Valve is secured in close position. Consider APU INOP. Advise dispatch OPERATIONAL PROCEDURE 28-40-06 -g) (A321) On Ground The FQI is in degraded mode when the FOB indication is displayed with two dashes across the two last digits on the EWD (Continued) Revision: 36 June 30, 2017

N Registration

Page: 28.46


SUBJECT

CAT

No INS

MIN REQ


28-40-06 ECAM FUEL PAGE Indications (Continued) When the FQI is in degraded mode: On the FUEL SD page determine which tank is affected. The resulting loss of accuracy must be taken into account by using the two following parameters: 1. Fq : The extra fuel quantity to be loaded. 2. W: The weight to be added to the total fuel weight for TOW calculation only. Fq and W parameters are given as follows:

-When the auto refuel stops: Preselect the fuel quantity required for the mission: Fm Enter the table and determine Fq and W values for the affected tank. Start again the auto refuel with the new preselected quantity which corresponds to the total FOB: Fm + Fq Note: If all tanks reach high level before having loaded the complete Fq value, this shows that all tanks are volumetrically full but the necessary fuel mass for the mission is not guaranteed since the fuel quantity indication varies with the fuel density. Therefore the mission or the aircraft load must be amended to match the minimum fuel quantity known to be onboard. -When the auto refuel stops again: The FOB value to be considered for TOW calculation is: FOB = Fm + Fq + W If all tanks reach high level before having loaded Fq value: The extra fuel quantity known to be onboard is: Fq* with: Fq* < Fq The FOB value to be considered for TOW calculation is: FOB = Fm + Fq * + W If the resulting TOW is higher than the MTOW The aircraft load must be reduced

(Continued)


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Page: 28.47


SUBJECT

CAT

No INS

MIN REQ


28-40-06 ECAM FUEL PAGE Indications (Continued) OPERATIONAL PROCEDURE 28-40-06 -h) (A321) All Set of Provisos After Refueling To check the fuel quantity in the associated tank: Refer to FCOM/PER-LOD-FUL-FUEL-A. GENERAL INFORMATION At Top Of Climb -Check on the FUEL SD page that the fuel is transferred from one additional center tank to the center tank -Check that the fuel quantity in one additional center tank has decreased If the automatic transfer has not started: After 30 minutes of flight: ACT pb-sw ……………………………………FWD If necessary, descend to FL 270. When ACT (both ACTs if two ACTs installed)empty: ACT pb-sw …………………………………………..AUTO OPERATIONAL PROCEDURE 28-40-06 -i) (A321) At top of climb Check of the fuel transfer from one additional center tank (from ACT 2 if ACT 2 is installed and not empty) to center tank: On the FUEL SD page, check that the transfer indication (arrow) is displayed or check that the total fuel indicated is above the actual fuel indicated after refuel minus FU. If automatic transfer has not started: After 30 minutes of flight: ACT pb-sw ……………………………………FWD If necessary perform a descent to FL 270. When ACT (both ACTs if two ACTs installed) empty: ACT pb-sw …………………………………………..AUTO MAINTENANCE (M) 28-40-06 -b) To APU LP Valve Indication - Valve Closure Procedure refer to AMM 28-40-00-040-001. MAINTENANCE (M) 28-40-06 -c) To Crossfeed Valve Indication - Valve Operating Procedure refer to AMM 28-40-00-040-002 (Continued)


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Page: 28.48


SUBJECT

CAT

No INS

MIN REQ


28-40-06 ECAM FUEL PAGE Indications (Continued) MAINTENANCE (M) 28-40-06 -d) To Transfer Valve Indication - Intercell Transfer refer to AMM 28-40-00-040-004 MAINTENANCE (M) 28-40-06 –h, i), j) All Provisos To check of the Fuel Quantity Indicating System, When an Outer Tank Indication is Unserviceable refer to AMM 28-40-00-040-003. MAINTENANCE (M) 28-40-06 j) proviso ii (May be inoperative provided the tank remains empty) Deactivate the Center fuel Tank (Refer to AMM TASK 28-21-00-040-002) including defuel of center tank (Refer to AMM Task 28-25-00-650-001). MAINTENANCE (M) 28-40-06 j) proviso iii (May be inoperative provided fuel is considered unusable and is included in computing ZFW and C.G. calculations.) Deactivate the center tank without the center tank defuelled (Refer to AMM Task 28-21-00-040-003). Inform to the crew and Make an entry in the aircraft technical log with the remaining fuel quantity in the fuel center tank to compute the ZFW and C.G. of the aircraft. MAINTENANCE (M) 28-40-06 -m) To Engine LP Valve Indication - When ECAM Display Inoperative refer to AMM Task 28-40-00-040-009 ECAM FUEL PAGE Indications Maintenance Procedures for A321 MAINTENANCE (M) 28-40-06 -b) (A321) Refer to MEL item: 49-30-02 MAINTENANCE (M) 28-40-06 -c) (A321) Refer to MEL AMM supplement: AMM task 28-40-00-040-002-A MAINTENANCE (M) 28-40-06 -f) (A321) Refer to MEL AMM supplement: AMM task 28-40-00-040-005-A MAINTENANCE (M) 28-40-06 -h) (A321) First set of provisos Refer to MEL AMM supplement: AMM task 28-40-00-040-006-A MAINTENANCE (M) 28-40-06 -h) (A321) Third set of provisos Refer to MEL AMM supplement: AMM task 28-28-00-040-008-A MAINTENANCE (M) 28-40-06 -i) (A321) All set of provisos Refer to MEL AMM supplement: AMM task 28-40-00-040-010-A MAINTENANCE (M) 28-40-06 -k) (A321 Refer to MEL AMM supplement: AMM task 28-24-00-040-001-A and AMM task 28-40-00-040-009-A


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Page: 28.49


SUBJECT

CAT

No INS

MIN REQ

C

7

0

Applicable to N696AV, N725AV, N729AV, N744AV, N746AV, N759AV, N761AV, One or more may be inoperative provided fuel quantity is determined by acceptable means.

C

9

0

Applicable to A319 and A320 except, N647AV, N664AV, N691AV, N398AV, N451AV, One or more may be inoperative provided fuel quantity is determined by acceptable means.

C

11

0

Applicable to N589AV, N590EL, N591EL, N592EL, N593EL, N594EL, N595EL, N596EL, N597EL, N598EL, N647AV, N664AV, N691AV, N398AV, N451AV. One or more may be inoperative provided fuel quantity is determined by acceptable means


28-40-07 Manual Magnetic Indicators


N Registration

Page: 28.50


SUBJECT

28-40-08 Fuel Quantity Attitude Monitor


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable to Avianca Avianca fleet has not installed Fuel Quantity Attitude Monitor.

N Registration

Page: 28.51


SUBJECT

CAT

No INS

MIN REQ


C

4

2

(O) One in each wing or both in one wing may be inoperative provided fuel temperature indications on the ECAM FUEL system page are available for the non affected tank(s) and fuel temperature is monitored prior to takeoff and during the flight.

28-40-09 Cautions on ECAM 1) TK HI TEMP(Left, Right, Inner, Outer Wing Tank (A318/A319/A320)

NOTE: For fuel temperature limitations, refer to AFM. C

4

0

(O) May be inoperative provided fuel temperature indications on the ECAM FUEL system page are available and fuel temperature is monitored prior to takeoff and during flight. NOTE: For fuel temperature limitations, refer to AFM.

2) TK HI TEMP(Left, Right Wing Tank) (A321)

C

2

1

(O) One may be inoperative provided fuel temperature indications on the ECAM FUEL system page are available for the non affected tank and fuel temperature is monitored prior to takeoff and during the flight. NOTE: For fuel temperature limitations, refer to AFM/LIM-28 Fuel Temperature Limits

C

2

0

(O) May be inoperative provided fuel temperature indications on the ECAM FUEL system page are available and fuel temperature is monitored prior to takeoff and during flight. NOTE: For fuel temperature limitations, refer to AFM/LIM-28 Fuel Temperature Limits

3) TK LO TEMP(Left, Right, Inner, Outer) Wing Tank) (A318/A319/320)

C

4

2

(O) One in each wing or both in one wing may be inoperative provided fuel temperature indications on the ECAM FUEL system page are available for the non affected tanks and fuel temperature is monitored prior to takeoff and during the flight. NOTE: For fuel temperature limitations, refer to AFM.

C

4

0

(O) May be inoperative provided fuel temperature indications on the ECAM FUEL system page are available and fuel temperature is monitored prior to takeoff and during flight.

NOTE: For fuel temperature limitations, refer to AFM. (Continued) Revision: 36 June 30, 2017

N Registration

Page: 28.52


SUBJECT

CAT

No INS

MIN REQ

C

2

1


28-40-09 Cautions on ECAM (Continued) 4) TK LO TEMP(Left, Right Wing Tank) a) A321

(O) One may be inoperative provided fuel temperature indications on the ECAM FUEL system page are available for the non affected tank and fuel temperature is monitored prior to takeoff and during the flight. NOTE: For fuel temperature limitations, refer to AFM/LIM-28 Fuel Temperature Limits

C

2

0

(O) May be inoperative provided fuel temperature indications on the ECAM FUEL system page are available and fuel temperature is monitored prior to takeoff and during flight. NOTE: For fuel temperature limitations, refer to AFM/LIM-28 Fuel Temperature Limits

5) ACT XFR FAULT Additional Center Tank(s) (Applicable to A321 only)

C

1

0

(O) May be inoperative provided forward transfer from ACT (s) to center tank is monitored during flight if ACT (s) is fueled.

OPERATIONS (O) 28-40-09 -1), and -2) TK HI TEMP: Refer to AFM for fuel temperature limits. Monitor fuel temperature on ECAM FUEL system page prior to takeoff and periodically during the flight. If fuel temperature reaches limits: - Before takeoff, delay takeoff and shutdown engine of affected side. - In flight, increase engine fuel flow of affected side and if necessary use APU GEN and switch off IDG of affected side if opposite GEN is available. OPERATIONS (O) 28-40-09 -3), and -4) TK LO TEMP: Refer to AFM for fuel temperature limits. Monitor fuel temperature on ECAM FUEL SYSTEM page prior to takeoff and periodically during the flight. If fuel temperature reaches limits: - Before takeoff, delay takeoff. - In flight, consider descending to a lower altitude and/or increasing mach to increase TAT. OPERATIONS (O) 28-40-09 -5) Refer to Operational Procedure MEL item 28-40-06 subitem 8 A321 Revision: 36 June 30, 2017

N Registration

Page: 28.53


SUBJECT

CAT

No INS

MIN REQ

C

1

0


28-40-10 Indication on ECAM E/WD 1) Fuel On Board(FOB)



N Registration

Page: 28.54

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 29 HYDRAULIC POWER ITEM 29-00

SUBJECT

CAT

No INS

MIN REQ


CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) Pre Mod. 23119 Fault(s) Indicated by BLUE RSVR


C

Applicable to A321 Only Dispatch not permitted with this MAINT. STATUS message displayed on ECAM.

N Registration

Page: 29.1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 29 HYDRAULIC POWER ITEM

SUBJECT

CAT

No INS

MIN REQ

C

2

1


29-10-01 Engine Driven Pump Systems 1) Depressurization Function

May be inoperative on one pump.

PLACARD Install 29-10-01 INOP placard adjacent to appropriate Engine Hydraulic Pump switch on overhead Hydraulics panel


N Registration

Page: 29.2


SUBJECT

CAT

No INS

MIN REQ

C

1

0


29-10-02 Blue System Electric Pump 1) Automatic Control

(O) May be inoperative provided: a) Pump can be manually operated, and b) Indications of blue hydraulic system are verified normal.

PLACARD Install 29-10-02 INOP placard adjacent to the Blue Hydraulic switch on overhead Hydraulics panel

OPERATIONS (O) 29-10-02 On ground: - If blue electric pump runs continuously : At electrical power supply application : BLUE ELEC PUMP ………………………………………………………………..OFF After engines start : BLUE ELEC PUMP

………………………………………………………………AUTO

After engines shut-down : BLUE ELEC PUMP

………………………………………………………………..OFF

- If blue electric pump does not start automatically : After engines start : BLUE ELEC PUMP ………………………………………………………………AUTO BLUE PUMP OVRD ………………………………………………………………….ON Check blue hydraulic pressure available on ECAM HYD page. After engines shut-down : BLUE ELEC PUMP


………………………………………………………………..OFF

N Registration

Page: 29.3


SUBJECT

CAT

No INS

MIN REQ

C

3

1


29-10-03 Hydraulic System Accumulators

1) Pre Mod. 21414

Applicable to all A319/A320/A321 except N759AV, N751AV, N764AV and N765AV (M) One or two may be inoperative provided: a) Blue hydraulic generation accumulator is operative, and b) The affected accumulator is deactivated.

2) Post Mod. 21414

C

3

0

Applicable to all A318 and N759AV, N751AV, N764AV and N765AV (M) May be inoperative provided the affected accumulator is deactivated. NOTE : For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.

PLACARD Install 29-10-03 INOP placard adjacent to the associated Hydraulic switch on overhead panel MAINTENANCE (M) 29-10-03 -For deactivation of the Green Power Accumulator, refer to AMM 29-10-00-040-004A -For deactivation of the Blue Power Accumulator, refer to AMM 29-10-00-040-005A -For deactivation of the Yellow Power Accumulator, refer to AMM 29-10-00-040-006A -Hydraulic System Accumulators, refer to Aircraft Maintenance Manual (AMM) 29-10-00-040-007.


N Registration

Page: 29.4


SUBJECT

29-10-04 System Filters


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Incorporated into 29-10-07, sub item 1).

N Registration

Page: 29.5


SUBJECT

29-10-05 Case Drain Filters


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Incorporated into 29-10-07, sub item 2).

N Registration

Page: 29.6


CAT

No INS

MIN REQ

1) System Filters

C

8

7

One LP, or one reservoir filling filter may be inoperative.

2) Case Drain Filters

C

3

2

(M) One may be inoperative provided it is removed.

SUBJECT


29-10-07 Filters

PLACARD Install 29-10-07 INOP placard adjacent to the lower ECAM display MAINTENANCE (M) 29-10-07 -

To deactivation of the Case Drain Filter of the Engine Driven Pump of the Green Hydraulic System refer to AMM TASK 29-10-00-040-001-A

-

To deactivation of the Case Drain Filter of the Engine Driven Pump of the Yellow Hydraulic System refer to AMM TASK 29-10-00-040-002-A

-

To deactivation of the Case Drain Filter of the Electric Pump of the Blue Hydraulic System refer to AMM TASK 29-10-00-040-003-A


N Registration

Page: 29.7

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 29 HYDRAULIC POWER ITEM 29-20-01

SUBJECT Hydraulic Reservoir Quantity Indicator (Green Servicing Panel)

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS (M) May be inoperative provided hydraulic fluid quantity is monitored during servicing of the hydraulic reservoir using the visual quantity gauge.

PLACARD Install 29-20-01 INOP placard adjacent to the lower ECAM display and reservoir. MAINTENANCE (M) 29-20-01 To deactivate Hydraulic Reservoir Quantity-Indicator refer to Maintenance Manual (AMM) Task Number 29-31-00-040-003.


N Registration

Page: 29.8


SUBJECT

29-20-02 Hydraulic Reservoir Four Way Selector Valve on Ground Service Panel

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS (M) May be inoperative provided associated system is serviced using the HP ground connection.

PLACARD Install 29-20-02 INOP placard adjacent to the lower ECAM display and reservoir. MAINTENANCE (M) 29-20-02 To deactivate Manual Selector Valve refer to Maintenance Manual (AMM) Task Number 29-16-00-040001.


N Registration

Page: 29.9


SUBJECT

CAT

No INS

MIN REQ


B

1

0

(O) May be inoperative (PTU runs continuously) provided: a) System pressure indication on ECAM operates normally, b) Power transfer can be stopped when PTU pb sw is placed OFF, and c) Operation of the PTU in both directions is verified before first flight of each day.

29-23-01 Power Transfer Unit 1) Automatic Activation Function

PLACARD Install 29-23-01 INOP placard adjacent to PTU p.b switch on the overhead Hydraulics panel. OPERATIONS (O) 29-23-01 After both engines start: GREEN ENG 1 PUMP …………………………………..………………….OFF Check that green system pressure is correct (3000 PSI ± 200 PSI) and check the PTU arrow indication. GREEN ENG 1 PUMP …………………………………..…….……………..ON PTU ….………………………………..………………….OFF YELLOW ENG 2 PUMP ..………………………..……………………………OFF YELLOW ELEC PUMP …………………………………..…………CHECK OFF Let the pressure in the yellow hydraulic system decrease to 200 psi or less, then : PTU …………………………………..……………………ON Check that yellow system pressure is correct (3000 PSI ± 200 PSI) and check the PTU arrow indication. YELLOW ENG 2 PUMP …………………………………..…………………….ON Note: 1) The PTU pressurizes the system to a nominal value of 3000 PSI ± 200 PSI, but if no consumers are operated the pressure is not constant. The PTU operates in a cycle which keeps the pressure in the hydraulic system between 2100 and 3200 PSI. 2) For passengers comfort, PTU may be switched off during the taxi after landing provided both hydraulic engine pumps are operative and running. PTU must be selected AUTO before leaving the aircraft.


N Registration

Page: 29.10

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 29 HYDRAULIC POWER SUBJECT

CAT

No INS

29-24-01 Yellow System Electric Pump

C

1

ITEM

MIN REQ

0

REMARKS OR EXCEPTIONS (M) May be inoperative provided associated pb sw is selected OFF.

PLACARD Install 29-24-01 INOP placard adjacent to the Yellow Hydraulic switch on the overhead hydraulics panel. MAINTENANCE (M) 29-24-01 To deactivate Yellow Electric Pump refer to Maintenance Manual (AMM) Task Number 29-24-00-040-001.


N Registration

Page: 29.11


SUBJECT

CAT

No INS

MIN REQ

C

4

0


29-30-01 Pump p.b. Switch 1) FAULT Lights

May be inoperative provided the associated reservoir quantity indication operates normally. NOTE: Illumination of two lights (one from the Blue ELEC PUMP p.b. and one from ENG 1(2) PUMP p.b.) with engines off, may be due to a failed engine oil low pressure switch. In this case, the ENG OIL LO PRESS warning is inoperative.

2) OFF Lights

C

3

0

3) ON Light

C

1

0

PLACARD Install 29-30-01 INOP placard adjacent to associated Fault Light p.b on the overhead Hydraulics panel


N Registration

Page: 29.12


CAT

No INS

MIN REQ

1) FAULT Light

C

1

0

2) OFF Light

C

1

0

SUBJECT


29-30-02 PTU p.b. Switch May be inoperative provided yellow and green reservoir quantity indicators operate normally.

PLACARD Install 29-30-02 INOP placard adjacent to the PTU Light on the overhead Hydraulics panel


N Registration

Page: 29.13


CAT

No INS

MIN REQ


1) Reservoir Quantity

C

3

2

(M)One may be inoperative provided: a) The associated reservoir quantity is verified adequate before each departure, and b) Associated RSVR LO LVL caution on ECAM operates normally.

2) Fire Valve

C

2

0

3) Yellow Elec Pump

C

1

0

4) PTU

C

1

0

5) System Label

C

3

0

(O)May be inoperative provided: a) Associated system pressure is verified before each departure, and b) Associated spoilers availability is verified before each departure.

6) System Pressure

C

3

2

(O) One may be inoperative provided associated System Label indication operates normally.

7) Pumps

C

3

0

8) RAT

C

1

0

SUBJECT

29-30-03 ECAM HYD Page Indications

(O) May be inoperative provided RAT is verified stowed before each departure.

PLACARD Install 29-30-03 INOP placard adjacent to lower ECAM display. OPERATIONS (O) 29-30-03 -5) System labels During cockpit preparation : YELLOW ELEC PUMP …………………………………………………………..ON BLUE ELEC PUMP ……………………………………………..CHECK AUTO BLUE PUMP OVRD …………………………………………………………..ON PTU ……………………………………………..CHECK AUTO Move the stick left or right and check spoilers movement on ECAM FLT CTL page. YELLOW ELEC PUMP …………………………………………………………OFF BLUE ELEC PUMP ……………………………………………OFF then AUTO (Continued) Revision: 29 October 23, 2014

N Registration

Page: 29.14


SUBJECT

CAT

No INS

MIN REQ


29-30-03 ECAM HYD Page Indications (Continued) OPERATIONS (O) 29-30-03 -6) System pressure During cockpit preparation: - If blue system affected : Check on ECAM HYD page that BLUE system label is amber. BLUE ELEC PUMP ……………………………………………….CHECK AUTO BLUE PUMP OVRD …………………………………………………………….ON Check that BLUE system label is white and arrow is green. BLUE ELEC PUMP ………………………………………………OFF then AUTO -

If yellow system affected Note: PTU FAULT warning is on.

YELLOW ELEC PUMP ……………………………………………………………OFF Check on ECAM HYD page that YELLOW system label is amber. YELLOW ELEC PUMP ……………………………………………………………..ON Check that YELLOW system label is white and arrow is green. YELLOW ELEC PUMP ……………………………………………………………OFF -

If green system affected Note: PTU FAULT warning is on.

Check on ECAM HYD page that GREEN system label is amber. YELLOW ELEC PUMP …………………………………………………………….ON PTU ……………………………………………….CHECK AUTO Check that GREEN system label is white and arrow is green. YELLOW ELEC PUMP ……………………………………………………………OFF OPERATIONS (O) 29-30-03 -8) RAT Visually verify RAT is stowed before each departure. MAINTENANCE (M) 29-30-03 -1) To deactivation of the Reservoir Quantity Indication of the Green and Blue Hydraulic Systems on the ECAM refer to AMM TASK 29-31-00-040-001-A. To deactivation of the Reservoir Quantity Indication of the Yellow Hydraulic System on the ECAM refer to AMM TASK 29-31-00-040-002-A (Continued)


N Registration

Page: 29.15


SUBJECT

CAT

No INS

MIN REQ

C

3

2


29-30-04 ECAM Warnings & Cautions 1) RSVR LO AIR PR a) A320 Pre-mod 23119, A320 Postmod 23119 and 27189, and A318/A319/A321 b) A320 Post-mod 23119 and Pre-mod 27189

(M) One may be inoperative provided air pressure is verified on the reservoir before each departure

Not applicable to Avianca Avianca Fleet A320 has incorporated Mod 23119 and Mod 27189

2) RSVR OVHT

C

3

2

Either green or yellow RSVR OVHT may be inoperative.

3) ELEC PUMP OVHT

C

2

0

a) ELEC PUMP LO PR

C

2

0

(O) May be inoperative provided: a) Associated system pressure indication operates normally, and b) Operation of electric pumps is checked before each departure.

b) ENG PUMP LO PR

C

2

0

(O) May be inoperative provided: a) Associated system pressure indication operates normally, and b) Operation of engine pumps is checked before each departure.

C

3

2

(M) One may be inoperative provided: a) Associated reservoir quantity indication operates normally, and b) Quantity is verified adequate before each departure.

4) PUMP LO PR

5) RSVR LO LVL

NOTE: If blue reservoir is affected, EMER GEN may appear on ECAM STATUS INOP SYS before engines are running. 6) SYS LO PR

C

3

0

(O) May be inoperative provided: a) Associated system pressure is verified before each departure, and b) Associated spoiler availability is verified before each departure. (Continued)


N Registration

Page: 29.16


CAT

No INS

MIN REQ

7) PTU FAULT

C

1

0

(O) May be inoperative provided the PTU is verified to operate normally before each departure.

8) RAT FAULT

C

1

0

(M) May be inoperative provided RAT integrity is not affected.

SUBJECT


29-30-04 ECAM Warnings & Cautions (Continued)

OPERATIONS (O) 29-30-04 –4)a) ELEC PUMP LO PR Before each flight check on ECAM HYD page that associated hydraulic pressure is correct (3000  200 PSI) OPERATIONS (O) 29-30-04 –4)b) ENG PUMP LO PR -

If warning is erroneously displayed :

After both engines start : PTU …………………………………………………………….…..OFF Check that green and yellow hydraulic systems pressure is correct (3000 PSI ± 200 PSI) on the ECAM HYD page. PTU

……………………………………………………………….AUTO Note: PTU remains indicated running on the ECAM HYD page.

OPERATIONS (O) 29-30-04 -6) SYS LO PR During cockpit preparation : YELLOW ELEC PUMP …………………………………………………………………ON BLUE ELEC PUMP ……………………………………………………CHECK AUTO BLUE PUMP OVRD …………………………………………………………………ON PTU ……………………………………………………CHECK AUTO Move the stick left or right and check spoilers movement on ECAM FLT CTL page. YELLOW ELEC PUMP ………………………………………………………………..OFF BLUE ELEC PUMP …………………………………………………OFF then AUTO (Continued) Revision: 29 October 23, 2014

N Registration

Page: 29.17


SUBJECT

CAT

No INS

MIN REQ


29-30-04 ECAM Warnings & Cautions (Continued) OPERATIONS (O) 29-30-04 -7) PTU FAULT During cockpit preparation: YELLOW ELEC PUMP ………………………………………………………………ON PTU …………………………………………………CHECK AUTO Check on ECAM HYD page that green hydraulic pressure (if indication available) is normal. If hydraulic pressure indication is not available, check on ECAM HYD page that GREEN system label is white and arrow is green. YELLOW ELEC PUMP ……………………………………………………………..OFF MAINTENANCE (M) 29-30-04 -1) To deactivation of the Reservoir Air Pressure Switches and Check of the Reservoir Air Pressure of the Green and Yellow Hydraulic System refer to AMM TASK 29-34-00-040-001-A To deactivation of the Reservoir Air Pressure Switch and Check of the Reservoir Air Pressure of the Blue Hydraulic System refer to AMM TASK 29-34-00-040-002-A. MAINTENANCE (M) 29-30-04 -5) To deactivate Reservoir Low-Level Warning refer to Maintenance Manual (AMM) Task Number 29-30-00040-003. MAINTENANCE (M) 29-30-04 -8) To Integrity Check of the RAT after RAT FAULT Warning refer to AMM 29-30-00-040-001.


N Registration

Page: 29.18


SUBJECT

CAT

No INS

MIN REQ

C

3

0


29-30-05 LEAK MEASUREMENT VALVE p.b. Switches 1) OFF Lights

PLACARD Install 29-30-05 INOP placard adjacent to lower ECAM display


N Registration

Page: 29.19


SUBJECT

CAT

No INS

MIN REQ




N Registration

Page: 29.20

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 30 ICE AND RAIN PROTECTION ITEM 30-00

SUBJECT

CAT

No INS

MIN REQ


CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) Fault(s) Indicated by ICE DETECT

C

2) Fault(s) Indicated by ENG 1(2) A.ICE (A319neo/A320neo/A321 neo)

C

Applicable to N759AV, N761AV, N764AV and N765AV only

NOTE 1: Dispatch with this MAINT STS message displayed on ECAM is permitted without CFDS interrogation. NOTE 2: The systems are designed to be fault tolerant for a period of time given on the category column in accordance with MEL preamble information. Quantities are not required for this item while the idea is to allow these fault indication.


N Registration

Page: 30.1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 30 ICE AND RAIN PROTECTION SUBJECT

CAT

No INS

MIN REQ


30-11-01 Wing Anti-ice Control Valves

C

2

1

(M)(O) RH valve may be inoperative in the OPEN position provided: a) Engine No. 1 is started first, b) X BLEED selector is shut when starting the NO. 1 engine, c) "CROSS BLEED START" procedure is used when starting the NO. 2 engine, and d) Alternate procedures are established and used, and e) Appropriate performance penalties are applied.

C

2

0

(M) Except for ER operations beyond 120 minutes, may be inoperative secured CLOSED provided the aircraft is not operated in known or forecast icing conditions.

ITEM

PLACARD 30-11-01 Install INOP placard adjacent to affected Anti-Ice switch on overhead Anti-Ice panel OPERATIONS (O) 30-11-01

FLIGHT PREPARATION/LIMITATIONS Flight planning: Increase fuel consumption by: Applicable to A318-111:



Applicable to A319-115 except N723AV and N726AV:

Applicable to A319-115, Only for N723AV AND N726AV:


(Continued) Revision: 33 September 03, 2015

N Registration

Page: 30.2

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 30 ICE AND RAIN PROTECTION ITEM 30-11-01

SUBJECT

CAT

No INS

MIN REQ


Wing Anti-ice Control Valves ( Continued )


Applicable to A320-200 with Sharklets except A320-251N (NEO):


Applicable to A320-251N ( NEO)



Applicable to A321-253N (NEO)

Single engine cruise: Decrease drift down ceilings by: Applicable to A318-111 and A318-112: 900 ft when OAT ≤ ISA 3 200 ft when OAT > ISA Applicable to A319-115 and N723AV AND N726AV 600 ft when OAT ≤ ISA - 5 °C 5 000 ft when OAT > ISA - 5 °C


N Registration

Applicable to A319-112: 900 ft when OAT ≤ ISA 3 300 ft when OAT > ISA Applicable to A319-132: 1 300 ft when OAT ≤ ISA + 15 °C 5 200 ft when OAT > ISA + 15 °C

Page: 30.3

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 30 ICE AND RAIN PROTECTION ITEM

SUBJECT

CAT

No INS

MIN REQ


30-11-01

Wing Anti-ice Control Valves ( Continued ) Single engine cruise: Decrease drift down ceilings by: Applicable to Applicable to A320-200 with Sharklets except for A320-251N (NEO): 1 400 ft when OAT ≤ ISA 4 600 ft when OAT > ISA Applicable to A320-251N ( NEO) Applicable to A320-233: 600 ft when OAT ≤ ISA + 0 °C 1500 ft when OAT ≤ ISA +20°C 2400 ft when OAT ≤ ISA + 0 °C 4000 ft when >ISA + 20°C Applicable to A320-211: Applicable to A321-231: 500 ft when OAT ≤ ISA 1 500 ft when OAT ≤ ISA + 20 °C 2 300 ft when >ISA 2 700 ft when OAT > ISA + 20 °C Applicable to A321-253N ( NEO) 550 ft when OAT ≤ ISA + 0 °C 2680 ft when OAT ≤ ISA + 0 °C Applicable to A320-214: 1 100 ft when OAT ≤ ISA 4 500 ft when OAT > ISA

Approach climb performance: When the engine bleed air supply system is closed: No penalty. When the engine bleed air supply system is open: Decrease maximum climb limiting weight by: Applicable to A318-111

Applicable to A318-112

700 kg (1 600 lb) when OAT ≤ ISA + 20 °C


3 700 kg (8 200 lb) when OAT > ISA + 20 °C








Applicable to A319-115 (N723AV AND N726AV)






Applicable to A320-251N ( NEO) 400kg (890 lb) when OAT ≤ ISA + 5 °C 3100kg (6840 lb) when OAT > ISA + 5 °C

Applicable to A321-253N ( NEO) 570 KG (1257 lb) when OAT ≤ ISA + 5 °C 3070 kg (6788 lb) when OAT > ISA + 5 °C

Applicable to Applicable to A320-200 with Sharklets except for A320-251N ( NEO)



1 100 kg (2 500 lb) when OAT ≤ ISA +5 °C


4 300 kg (9 500 lb) when OAT >ISA +5 °C

Applicable to A319-132, A320-233 and A321-231 2 300 kg (5 100lb)


N Registration

Page: 30.4


SUBJECT

CAT

No INS

MIN REQ


Wing Anti-ice Control Valves ( Continued )

DURING COCKPIT PREPARATION After application of the maintenance procedure: On the BLEED SD page, check that the anti-ice arrow symbol is displayed. The anti-ice arrow symbol may be displayed amber or green. The WING ANTI ICE L(R) HI PR alert must not be displayed on the EWD. BEFORE ENGINE START ‐ Maintain the X BLEED selector at SHUT before engine start when the APU bleed is used. ‐ Start the engine 1. Maintain the X BLEED selector at SHUT during the start of engine 1. ‐ Use the CROSS BLEED ENGINE START (Refer to FCOM/PRO-NOR-SUP-ENG Crossbleed Engine Start) procedure to start the engine 2. ‐ Apply the procedure associated with the WING ANTI ICE R VALVE OPEN alert displayed on the EWD. AFTER TAKEOFF When above 1 500 ft: Apply the automatic recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the EWD. IN FLIGHT In the case of failure of a Bleed Air Supply System: PACK (affected side) pb-sw..................................................................................................OFF AFTER LANDING Apply the automatic recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the EWD. MAINTENANCE (M) 30-11-01 (First Proviso) Deactivation of the RH Wing Anti-Ice Control Valve to the OPEN position refer to AMM 30-11-00-040-004. MAINTENANCE (M) 30-11-01 (Second Proviso) Deactivation of the Wing Anti-Ice Control Valve to the CLOSED position refer to AMM 30-11-00-040-001.


N Registration

Page: 30.5


SUBJECT

CAT

No INS

MIN REQ

C

1

0

(O) May be inoperative provided the anti-ice "arrow" on ECAM BLEED page operates normally.

C

1

0

(M) Except for ER operations beyond 120 minutes, may be inoperative provided: a) Wing anti-ice control valves are deactivated closed and considered inoperative, and b) Airplane is not operated in known or forecast icing conditions.

C

1

0


30-11-02 Wing Anti-Ice 1) FAULT Light

2) ON Light PLACARD

30-11-02 Install INOP placard adjacent to affected Anti-Ice light on overhead Anti-Ice panel OPERATIONAL (O) 30-11-02 DURING COCKPIT PREPARATION Check of the anti-ice "arrow" symbol: - Make sure that the APU bleed air supply system is available. - ANTI ICE WING pb-sw……………………………………………………………. ON - On the BLEED SD page, check that the anti-ice "arrow" symbols are displayed amber and disappear after 30 s. - ANTI ICE WING pb-sw……………………………………………………………. OFF MAINTENANCE (M) 30-11-02 Refer to MEL Maintenance procedure item 30-11-01 “First Proviso deactivation in CLOSED position”.


N Registration

Page: 30.6


CAT

No INS

MIN REQ

1) ANTI-ICE

C

2

0

2) ARROW

C

2

0

SUBJECT


30-11-03 ECAM BLEED Page Indications



N Registration

Page: 30.7


CAT

No INS

MIN REQ


30-21-01 Engine Anti-Ice Valves (A318/A319ceo/ A320ceo/A321ceo)

C

2

1

(M) Except for ER operations beyond 120 minutes, one may be inoperative secured closed provided the airplane is not operated in known or forecast icing conditions.

(A318/A319ceo/ A320ceo/A321ceo)

C

2

0

(M)(O) May be inoperative open provided AFM performance penalties are applied.

(A319neo/A320neo/ A321neo)

C

4

2

(O) Except for ER operations beyond 120 minutes, one or two NAI valves on the same engine may be inoperative in the closed position provided the aircraft is not operated in known or forecast icing conditions.


C

4

2

(M) One NAI valve per engine may be inoperative provided it is deactivated in the open position.

(A319neo/A320neo/ A321neo with CFM LEAP1-A engines)

C

4

2

(M)(O) Except for ER operations beyond 120 minutes, two may be inoperative on the same engine provided: a) Affected NAI valves are deactivated in the closed position, and b) Aircraft is not operated in known or forecast icing conditions.

ITEM

PLACARD 30-21-01 Install INOP placard adjacent to affected Engine Anti-Ice switch on overhead Anti-Ice panel OPERATIONAL (O) 30-21-01 (Applicable to A318, A319, A320 and A321 aircraft except to A320-200 with Sharklets) A321-253N (neo) GENERAL INFORMATION A higher idle speed is set on both engines when an engine anti-ice valve is inoperative in the open position. FLIGHT PREPARATION/LIMITATIONS Note 1: The following decrements may be used for takeoff performance determination only for dry runways if no takeoff data (predetermined by using OCTOPUS program or other equivalent program with present failure case taken into account) is available. Note 2: Performance penalties apply whatever one or both valves are inoperative. Takeoff performance: Perform the takeoff using full thrust. Apply the following reductions on the MTOW and the speeds: Applicable to A318-111:


N Registration

Page: 30.8


SUBJECT

CAT

No INS

MIN REQ




Applicable to A319-115 except N723AV and N726AV


Applicable to A319-132, A320-233, A321-231, A321-211, N723AV and N726AV The takeoff performance must be determined by using OCTOPUS program or other equivalent program with present failure case taken into account.

Flight planning: Increase fuel consumption by: Applicable to A318-111:




N Registration

Page: 30.9


SUBJECT

CAT

No INS

MIN REQ


Engine Anti-Ice Valves (Continued)

Applicable to A319-115 except N723AV and N726AV:

Applicable to N723AV and N726AV:





N Registration

Page: 30.10


SUBJECT

CAT

No INS

MIN REQ


30-21-01 Engine Anti-Ice Valves (Continued) Applicable to A320-233:


Single engine cruise: Decrease drift down ceilings by: Applicable to A318-111 and A318-112: 200 ft when OAT ≤ ISA + 5 °C 2 600 ft when OAT > ISA + 5 °C Applicable to A319-115 except N723AV and N726AV 200 ft when OAT ≤ ISA + 5 °C 4 200 ft when OAT > ISA + 5 °C Applicable to A319-132: 1 300 ft when OAT ≤ ISA + 20 °C 4 900 ft when OAT > ISA + 20 °C Applicable to A320-233: 1300 ft when OAT ≤ ISA + 20 °C 4000 ft when OAT > ISA + 20 °C

Applicable to A319-112: 200 ft when OAT ≤ ISA + 5 °C 2 300 ft when OAT > ISA + 5 °C Applicable to N723AV and N726AV 250 ft when OAT ≤ ISA + 5 °C 4 100 ft when OAT > ISA + 5 °C Applicable to A320-214: 400 ft when OAT ≤ ISA + 5 °C 3 700 ft when OAT > ISA + 5 °C

Applicable to A321-231: 1 300 ft when OAT ≤ ISA + 15 °C 3 000 ft when OAT > ISA + 15 °C

Applicable to A321-211: 300 ft when OAT ≤ ISA + 5 °C 2 400 ft when OAT > ISA + 5 °C

Approach climb performance: Decrease maximum climb limiting weight by: Applicable to A318-111, A318-112 and A319-112: 300 kg (700 lb) when OAT ≤ ISA + 25 °C 3 500 kg (7 800 lb) when OAT > ISA + 25 °C Applicable to A319-115: 400 kg (900 lb) when OAT ≤ ISA + 25 °C 3 900 kg (8 600 lb) when OAT > ISA + 25 °C


N Registration

Page: 30.11


SUBJECT

CAT

No INS

MIN REQ


30-21-01 Engine Anti-Ice Valves (Continued) Applicable to A319-132: No penalty when OAT ≤ ISA + 25 °C 3 700 kg (8 200 lb) when OAT > ISA + 25 °C Applicable to A320-214: 300 kg (700 lb) when OAT ≤ ISA + 10 °C 4 400 kg (9 700 lb) when OAT > ISA + 10 ° Applicable to A320-233: No penalti When OAT ≤ ISA+10 °C 4500 kg/9900 lb when OAT > ISA + 10°C Applicable to A321-231: No penalty when OAT ≤ ISA + 10 °C 5 500 kg (12 100 lb) when OAT > ISA + 10 °C

Applicable to A321-211: No penalty when OAT ≤ ISA + 10 °C 5 500 kg (12 100 lb) when OAT > ISA + 10 °C

DURING COCKPIT PREPARATION ANTI ICE ENG (affected) pb-sw................................................................................................... ON AFTER ENGINE START The FADEC commands the continuous ignition on the affected engine. OPERATIONAL (O) 30-21-01 (Applicable to A320-200 with Sharklets except A320 neo) GENERAL INFORMATION An higher idle speed is set on both engines when an engine anti-ice valve is inoperative in the open position. FLIGHT PREPARATION/LIMITATIONS Same performance penalties apply with one or two valves inoperative. Takeoff performance: The takeoff performance must be determined by using OCTOPUS program or other equivalent program with present failure case taken into account or refer to Dispatch guide. Launch PEP. Flight planning: Increase fuel consumption by:


N Registration

Page: 30.12


SUBJECT

CAT

No INS

MIN REQ


30-21-01 Engine Anti-Ice Valves (Continued) Single engine cruise: Decrease drift down ceilings by: 600 ft when OAT ≤ ISA + 5 °C 4 200 ft when OAT > ISA + 5 °C Approach climb performance: Decrease maximum climb limiting weight by: 300 kg (700 lb) when OAT ≤ ISA + 10 °C 4 500 kg (9 900 lb) when OAT > ISA + 10 °C DURING COCKPIT PREPARATION ANTI ICE ENG (affected) pb-sw................................................................................................... ON AFTER ENGINE START The FADEC commands the continuous ignition on the affected engine. OPERATIONAL (O) 30-21-01 (Applicable to A320-251N neo and A321-253N neo DURING COCKPIT PREPARATION ANTI ICE ENG (affected) pb-sw ................................................................................................OFF

MAINTENANCE (M) 30-21-01 To Deactivation of the Engine Anti-Ice Valve in CLOSED Position refer to Aircraft Maintenance Manual (AMM) 30-21-00-040-001. To Deactivation of the Engine Anti-Ice Valve in the OPEN Position refer to Aircraft Maintenance Manual (AMM) 30-21-00-040-002.

MAINTENANCE (M) 30-21-01 applicable to A320 neo and A321 neo only To deactivate the NAI refer to Aircraft Maintenance Manual (AMM) 30-21-00-040-805


N Registration

Page: 30.13


CAT

No INS

MIN REQ

1) FAULT Lights

C

2

0

May be inoperative

2) ON Lights

C

2

0


SUBJECT


30-21-02 Engine Anti-ice

PLACARD 30-21-02 Install INOP placard adjacent to affected Engine Anti-Ice fault light on overhead Anti-Ice panel OPERATIONS (O) 30-21-02 Verify ENG ANTI-ICE on ECAM MEMO display and check IGNITION memo appears on the ECAM before each flight or if forecast icing conditions are known.


N Registration

Page: 30.14


SUBJECT

CAT

No INS

MIN REQ

30-21-03 ANTI-ICE ENG 1(2) CTL FAULT Cautions on ECAM E/WD (A319neo/A320neo/ A321neo)

REMARKS OR EXCEPTIONS Applicable to N759AV, N761AV, N764AV and N765AV only

C

2

0

(O) May be inoperative provided: a) Associated ENG 1(2) A.ICE VALVE OPEN is displayed on the EWD, and b) AFM performance penalties are applied

C

2

1

Except for ER operations beyond 120 minutes, one may be inoperative provided: a) Associated ENG 1(2) A.ICE MON FAULT is displayed on the EWD, and b) Aircraft is not operated in known or forecast icing conditions.

PLACARD 30-21-03 Install INOP placard adjacent to ECAM E/WD Display OPERATIONS 32-21-03 GENERAL INFORMATION A higher idle speed is set on both engines when the alert ANTI-ICE ENG 1(2) CTL FAULT is displayed on EWD with the ENG 1(2) A.ICE VALVE OPEN subtitle displayed. FLIGHT PREPARATION/LIMITATIONS Takeoff performance: The takeoff performance must be determined by using OCTOPUS program or other equivalent program with present failure case taken into account. Launch PEP. Flight planning: Increase fuel consumption by: (Continued)


N Registration

Page: 30.15


SUBJECT

CAT

No INS

MIN REQ


30-21-03 ANTI-ICE ENG 1(2) CTL FAULT Cautions on ECAM E/WD (A319neo/A320ne o/ A321neo) (Continued) Applicable to A321-253N ( NEO)

Applicable to A320-251N (NEO)

Single engine cruise Decrease drift down ceilings by: A321-253N ( NEO) 45 ft when OAT OAT ≤ ISA + 5 °C

A320-251N ( NEO) 40 ft when OAT OAT ≤ ISA + 5 °C

1180 ft when OAT > ISA + 5 °C

1700 ft when OAT > ISA + 5 °C

(Continued)


N Registration

Page: 30.16


SUBJECT

CAT

No INS

MIN REQ


30-21-03 ANTI-ICE ENG 1(2) CTL FAULT Cautions on ECAM E/WD (A319neo/A320neo/ A321neo) (Continued)

Approach climb performance: Decrease maximum climb limiting weight by:

A321-253N ( NEO)

A320-251N ( NEO)

50 kg (110 lb) when OAT ≤ ISA + 10 °C 1 470 kg (3 241 lb) when OAT > ISA + 10 °C

150 kg (340 lb) when OAT ≤ ISA + 15 °C 1 400 kg (3 090 lb) when OAT > ISA + 15 °C

DURING COCKPIT PREPARATION ANTI ICE ENG (affected) pb-sw................................................................................................... ON


N Registration

Page: 30.17


CAT

No INS

MIN REQ


30-31-01 Probe Heat Computers

C

3

2

C

3

2

(M) One may be inoperative provided associated heater is verified to operate normally prior to each flight . (M)(O) F/O's may be inoperative provided: a) ADRs, heaters and failure warnings associated with the operative units are verified to operate normally, and b) Takeoff in CONFIG 1+F is prohibited (in icing conditions) with ADR 2-OFF.

C

3

2

ITEM

(M) Except for ER operations beyond120 minutes, STBY may be inoperative provided: a) ADRs, heaters and failure warnings associated with operative units are verified to operate normally, b) Airplane is not operated in visible moisture, or known or forecast icing conditions, and c) Ambient temperature at the departure airport is above 5 degrees C when taxiways or runways are covered with water or slush.

PLACARD 30-31-01 Install INOP placard adjacent to associated Probe Heat switch on overhead Anti-Ice panel OPERATIONS (O) 30-31-01 DURING COCKPIT PREPARATION AIR DATA selector……………………………………………………………………………F/O 3 IN FLIGHT If icing conditions are encountered: ADR 2 pb-sw…………………………………………………………………………………..OFF CAUTION: When ADR 2 is set to OFF, ‐ Takeoff in CONF 1+F is not permitted, and ‐ Maximum landing capability is CAT 3 SINGLE. The ADR 2 pb-sw must remain set to OFF for the remainder of the flight. In the case of double failure of the alpha probe heaters, Refer to QRH/DOUBLE AOA HEAT FAILURE


N Registration

Page: 30.18


SUBJECT

CAT

No INS

MIN REQ


30-31-01 Probe Heat Computers (Continued) MAINTENANCE (M) 30-31-01 (First Proviso associated probe heating operative) To Check of the Operation of the Probe Heating Channel Refer to AMM 30-31-00-040-001 MAINTENANCE (M) 30-31-01 (Second Proviso F/O PHC inoperative or Third Proviso STBY PHC inoperative) To Check of the ADRS, Heaters and Failure Alerts related to the Probes refer to AMM 30-31-00-040-002.


N Registration

Page: 30.19


SUBJECT

30-31-02 Pitot Heaters

CAT

No INS

MIN REQ

B

3

2

(M)(O) F/O's may be inoperative provided: a) ADR, heaters and failure warnings associated with CAPT and STBY probes (pitot static, AOA, TAT) are verified to operate normally, and b) Takeoff in CONF 1+F is prohibited (in icing conditions) with ADR 2-OFF.

B

3

2

(M) Except for ER operations beyond 120 minutes, CAPT heater may be inoperative provided: a) ADR, heaters and failure warnings associated with F/O and STBY probes (pitot, static, AOA, TAT) are verified to operate normally, and b) Airplane is not operated in visible moisture, or in known or forecast icing conditions.

B

3

2

(M) Except for ER operations beyond 120 minutes, STBY heater may be inoperative provided: a) ADR, heaters and failure warnings associated with CAPT and F/O probes (pitot, static, AOA, TAT) are verified to operate normally, and b) Airplane is not operated in visible moisture, or in known or forecast icing conditions.


PLACARD 30-31-02 Install INOP placard adjacent to associated Heater switch on overhead Anti-Ice panel OPERATIONS (O) 30-31-02 Refer to operational procedure on AVA A318/A319/A320/A321 MEL item 30-31-01. MAINTENANCE (M) 30-31-02 Refer to maintenance procedure on AVA A318/A319/A320/A321 MEL item 30-31-01 TEST OF TWO OPERATIVE PROBE HEAT SYSTEMS.


N Registration

Page: 30.20


SUBJECT

30-31-03 Static Port Heaters

CAT

No INS

MIN REQ

C

6

5

One STBY heater may be inoperative.

C

6

4

(M)(O)CAPT heaters may be inoperative provided: a) ADR, heaters and failure warnings associated with the operative units are verified to operate normally, and b) Ambient temperature at the departure airport is greater than 5 degrees C when runway is contaminated with water or slush.

C

6

4

(M)(O)F/O heaters may be inoperative provided: a) ADR, heaters and failure warnings associated with the operative units are verified to operate normally, and b) Takeoff in CONF 1+F is prohibited (in icing conditions) with ADR 2-OFF.

C

6

4

(M)Except for ER operations beyond 120 minutes, STBY heaters may be inoperative provided: a) ADR, heaters and failure warnings associated with operative units are verified to operate normally, and b) Ambient temperature at the departure airport is greater than 5 degrees C when runway is contaminated with water or slush. NOTE: If CAPT or F/O heaters are inoperative, do not conduct RVSM operations


PLACARD 30-31-03 Install INOP placard adjacent to associated Static Port Heater switch on overhead Anti-Ice panel OPERATIONS (O) 30-31-03 Refer to operational procedure on AVA A318/A319/A320/A321 MEL item 30-31-01. MAINTENANCE (M) 30-31-03 Refer to maintenance procedure on AVA A318/A319/A320/A321 MEL item 30-31-01 TEST OF TWO OPERATIVE PROBE HEAT SYSTEMS.


N Registration

Page: 30.21


CAT

No INS

MIN REQ

30-31-04 Angle of Attack Probe Heaters

C

3

2

(M) F/O's heater may be inoperative provided ADR heaters and failure warnings associated with CAPT and STBY probes (pitot, static, AOA, TAT) are verified to operate normally.

C

3

2

(M) STBY heater may be inoperative provided ADR heaters and failure warnings associated with CAPT and F/O probes (pitot, static, AOA, TAT) are verified to operate normally.

C

3

2

(M) Except for ER operations beyond 120 minutes, CAPT's heater may be inoperative provided: a) ADR, heater and failure warnings associated with F/O and STBY probes (pitot, static, AOA, TAT) are verified to operate normally, and b) Airplane is not operated in visible moisture, or in known or forecast icing conditions.

ITEM


PLACARD 30-31-04 Install INOP placard adjacent to applicable AOA Heater switch on overhead Anti-Ice panel MAINTENANCE (M) 30-31-04 Refer to maintenance procedure on AVA A318/A319/A320/A321 MEL item 30-31-01 TEST OF TWO OPERATIVE PROBE HEAT SYSTEM.


N Registration

Page: 30.22


SUBJECT

30-31-05 TAT Probe Heaters

CAT

No INS

MIN REQ

C

2

1

C

2

0


Except for ER operations beyond 120 minutes, may be inoperative provided airplane is not operated in visible moisture, or in known or forecast icing conditions.

PLACARD 30-31-05 Install INOP placard adjacent to appropriate TAT Probe Heater switch on overhead Anti-Ice panel


N Registration

Page: 30.23


SUBJECT

30-42-01 Window Heat Computers

CAT

No INS

MIN REQ


C

2

1

(M) Except for ER operations beyond 120 minutes, one may be inoperative provided: a) All heaters and failure warnings on the front, and sliding windows associated with operative systems are verified to operate normally, and b) Airplane is not operated in known or forecast icing conditions. c) Approach minimums do not require its use

PLACARD 30-42-01 Install INOP placard adjacent to affected Window Heater switch on overhead Anti-Ice panel MAINTENANCE (M) 30-42-01 1.

On ANTI ICE panel 25 VU make certain that PROBE/WINDOW /HEAT /AUTO /ON pushbutton switch is released (ON legend is off)

2.

On MCDU 1 or 2 select CFDS MENU, SYSTEM REPORT TEST, ICE and RAIN select WHC 1(2). WHC 1(2) MENU is displayed perform TEST (test must be OK).


N Registration

Page: 30.24


SUBJECT

30-42-02 Fixed Lateral Window and Sliding Window Heating Systems

CAT

No INS

MIN REQ

C

4

0


PLACARD 30-42-02 Install INOP placard adjacent to affected Window Heater switch on overhead Anti-Ice panel


N Registration

Page: 30.25


SUBJECT

30-42-03 Windshield Heating Systems

CAT

No INS

MIN REQ

C

2

1

REMARKS OR EXCEPTIONS Except for ER operations beyond 120 minutes, one may be inoperative provided: a) Airplane is not operated in known or forecast icing conditions, and b) Approach minimums do not require its use NOTE: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.

PLACARD 30-42-03 Install INOP placard adjacent to affected Windshield Heater switch on overhead Anti-Ice panel


N Registration

Page: 30.26


CAT

No INS

MIN REQ


1) AUTO Control

C

1

0

May be inoperative provided PROBES/WINDOW HEAT system is manually selected.

2) ON Light

C

1

0

May be inoperative provided the PROBES/WINDOW HEAT automatic system is operative.

SUBJECT

30-42-04 Probes/Window Heat pb-sw

PLACARD Install 30-42-04 INOP placard adjacent to Probe/window Heater p.b switch affected


N Registration

Page: 30.27


SUBJECT

30-45-01 Windshield Wiper Systems

CAT

No INS

MIN REQ

C

2

0

REMARKS OR EXCEPTIONS (O) May be inoperative provided : a) Airplane is not operated in precipitation within 5 SM of the airport of takeoff or intended landing, and b) Approach minimums do not require its use. NOTE: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.

B

2

1

One may be inoperative provided: Associated rain repellent system is installed and operative.

1) Fast Speed

C

2

0

May be inoperative provided slow speed operates normally and approach minimums do not require its use.

2) Slow Speed

C

2

0

May be inoperative provided fast speed operates normally.

0

0

Not applicable to Avianca Fleet. Avianca fleet does not have Mod. 20319 incorporated.

C

2

0

May be inoperative provided affected wiper can be located in a position that will not obstruct forward vision.

C

2

0

(M) May be inoperative provided affected wiper is removed and considered inoperative..

3) Intermittent Speed (Aircraft with Mod. 20319) 4) PARK Function

PLACARD 30-45-01 Install INOP placard adjacent to affected Windshield Wiper Control switch on overhead panel OPERATIONS (O) 30-45-01 NOTE: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL. MAINTENANCE (M) 30-45-01 Refer to AMM TASK 30-45-00-040-003 Deactivation of the Windshield Wiper.


N Registration

Page: 30.28


SUBJECT

30-45-02 Rain Repellant Systems

CAT

No INS

MIN REQ

D

2

0


NOTE: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL. PLACARD 30-45-02 Install INOP placard adjacent to affected Rain Repellent Control switch on overhead panel


N Registration

Page: 30.29


SUBJECT

30-71-01 Waste Water Drain Mast Heating System

CAT

No INS

MIN REQ


C

2

0

(M)(O) May be inoperative provided: a) Associated lavatory and galley water supplies are secured off, b) Associated galley sink and lavatory washbasin drains are blocked to prevent their use, and c) Procedures are established to periodically monitor associated galley sinks and lavatory washbasins to ensure they remain blocked.

C

2

0

(M) May be inoperative provided: a) Associated galley and lavatory are not used, and b) The Pilot-in-Command will determine if flight duration is acceptable with a FWD lavatory unusable, and c) Associated lavatory door(s) is secured closed and placarded, "INOPERATIVE – DO NOT ENTER". NOTE: These provisions are not intended to prohibit inspections by crewmembers.

OPERATIONS (O) 30-71-01 The pilot-in-Command will determine if flight duration is acceptable with a FWD/Upper Deck lavatory unusable. MAINTENANCE (M) 30-71-01 To Deactivation of the Waste-Water Drain Mast Heating-System refer to AMM 30-71-00-040-001.


N Registration

Page: 30.30


SUBJECT Waste Water Drain Line Protection System


CAT

No INS

MIN REQ

D

1

0

N Registration


Page: 30.31


SUBJECT

30-71-03 Cargo Compartment Drain Line & Drain Mast Ice Protection System


CAT

No INS

MIN REQ

D

1

0

N Registration


Page: 30.32


SUBJECT

30-81-01 Visual Ice Detector


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS DELETED, on MMEL Revision 13.

N Registration

Page: 30.33


CAT

No INS

MIN REQ

30-81-02 Ice Detection System

D

1

0

ITEM


N Registration


Page: 30.34


SUBJECT

30-81-03 External Visual Ice Indicador Lighting


CAT

No INS

MIN REQ

D

1

0

N Registration


Page: 30.35


SUBJECT

CAT

No INS

MIN REQ




N Registration

Page: 30.36

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 31 INDICATING/RECORDING SYSTEMS ITEM 31-00

SUBJECT

CAT

CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) Fault(s) Indicated by QAR 2) Fault(s) Indicated by DMU

3) Fault(s) Indicated by DAR 4) Faults Indicated by CFDIU 5) Faults Indicated by ACMS

6) Faults Indicated by DMC 1/3 a) With Mod. 31283/MP P7125 b) With Mod. 151269/MP P11819 7) Faults indicated by DMC 2/3 (With Mod. 31283/MP P7125 or with Mod. 151269/MP P11819) 8) Faults indicated by DFDR ACCEL (With Mod 161365 / MP P14629)

A

No INS

MIN REQ


Not applicable. Applicable to aircraft with QAR installed. Not applicable to Avianca. NOTE: The failure of DMU part of FDIMU is indicated by a MAINTENANCE message on ECAM STATUS page. Refer to 31-00 5). Refer to 31-00 5) Faults Indicated by ACMS

C A

Refer to MEL 31-30-03 Note: When the Aircraft arrives to BOG or when the aircraft is dispatched from BOG must proceed with the following: -Upload FDIMU software according to AMM 3133-00-710-013. -When the uploading is not satisfactory, proceed to the replacement unit its respective software upload according to AMM 31-36-34-002 AMM 31-36-34-402.

C

C

May be displayed provided DMC 2/3 MAINTENANCE message is not displayed simultaneously on ECAM STATUS page. May be displayed on ECAM STATUS page.

C

May be displayed on ECAM STATUS page.

A

Applicable to A320neo and A321neo Refer to Item 31-30-02 1) FDR Recording Parameters Required by FAR (129.20 /121.344)/RAC NOTE 1: Dispatch with any of the above maintenance status messages displayed on ECAM is permitted without CFDS interrogation. NOTE 2: The systems are designed to be fault tolerant for a period of time given on the category column in accordance with MEL preamble information. Quantities are not required for this item while the idea is to allow these fault indication.


N Registration

Page: 31.1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 31 INDICATING/RECORDING SYSTEMS ITEM

SUBJECT

31-21-01 Clock System

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS (O) May be inoperative provided: a) Time base from CFDIU is available on ECAM, and b) Chrono indication is available on one Navigation Display (ND).

PLACARD 31-21-01 Install INOP placard adjacent to affected clock on right center instrument panel OPERATIONS (O) 31-21-01 After any electrical power interruption (loss of UTC on ECAM lower display), initialize UTC and date through the MCDU (Refer to FCOM/DSC-45-20).


N Registration

Page: 31.2


SUBJECT

31-27-01 Flight Number Reminder

CAT

No INS

MIN REQ

D

1

0




N Registration

Page: 31.3


SUBJECT

31-30-01 Centralized Fault Display System (CFDS)

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS May be inoperative provided CFDS system is available when required for specified maintenance tasks.

PLACARD 31-30-01 Install INOP placard adjacent to Captain’s Multi purpose Control Display Unit MCDU


N Registration

Page: 31.4


CAT

No INS

MIN REQ


Includes FDR function of Combined Voice and Flight Data Recorder (CVFDR)

A

1

0

May be inoperative provided: a) Cockpit voice Recorder (CVR) operates normally, b) Airplane is not dispatched from BOG unless: 1. The FDR failure occurs after pushback but prior to takeoff, or 2. The FDR repair was attempted but was not successful. c) In those cases where repair is attempted but not successful, the aircraft may be dispatched on a flight or series of flights until next arrival to BOG where repair must be accomplished prior to dispatch and d) Repairs are made within three flight days.

1) FDR Recording Parameters Required by FAR (129.20 and 121.344) / RAC

A

91

88

Up to three (3) parameters may be inoperative provided: a) Cockpit voice recorder (CVR) operates normally, and b) Repairs are made within 20 calendar days.

2) FDR Recording Parameters not Required by FAR/RAC

A

400 360 May be inoperative provided repairs are made prior to completion of next heavy maintenance visit.

SUBJECT

31-30-02 Flight Data Recorder (FDR) System

PLACARD 31-30-02 Install INOP placard adjacent to overhead RCDR panel Note: See on the next page the list of FDR recording parameters required by FAR and RAC (item 31-3002 –1).

(Continued)


N Registration

Page: 31.5


SUBJECT

CAT

No INS

MIN REQ


31-30-02 Flight Data Recorder (FDR) System (Continued) Time

47

2

Pressure altitude

48

3

Indicated airspeed

49

Selected speed (when an information source is installed)

4

Heading

50

Selected mach (when an information source is installed)

5

Vertical acceleration

51

6

Pitch attitude

52

7

Roll attitute

53

8

Manual radio transmitter keying

54

9

Thust/power of each engine

55

10

Autopilot engagement

56

11

Longitudinal accelerations

57

12

Pitch control input

58

13

Lateral control input

59

14

Rudder pedal input

60

15

Primary pitch control surface position

61

16

Primary lateral control surface position

62

17

Primary yaw control surface position

63

18

Lateral acceleration

64

Selected vertical speed (when an information source is installed) Selected heading (when an information source is installed) Selected flight path (when an information source is installed) Selected decision height (when an information source is installed) EFIS display format Multi-function/engine/alerts display format Thrust command (when an information source is installed) Thrust target (when an information source is installed) Fuel quantity in CG trim tank (when an information source is installed) Primary Navigation System Reference

19

Pitch trim surface position

65

20

Trailing edge flaps

66

Icing (when an information source is installed) Engine warning each engine vibration (when an information source is installed) Engine warning each engine over temp (when an information source is installed) Engine warning each engine oil pressure low (when an information source is installed) Engine warning each engine over speed (when an information source is installed) Yaw trim surface position

21

Leading edge flaps

67

Roll trim surface position

22

Each thrust reverser position

68

Brake pressure

23

Ground spoiler position

69

24

Outside or total air temperature

70

25

Automatic flight control system modes and engagement status, including autothrottle

71

26

Radio altitude (when an information source is installed)

72

27

Localizer deviation, mls azimuth

73

28

Glideslope deviation, mls elevation

74

Brake pedal application Yaw or sideslip angle (when an information source is installed) Engine bleed valve position (when an information source is installed) De-icing or anti-icing system selection (when an information source is installed) Computed center of gravity (when an information source is installed) AC electrical bus status

29

Marker beacon passage

75

30

Master warning

76

31

Air/ground sensor

77

DC electrical bus status APU bleed valve position (when an information source is installed) Hydraulic pressure

32

Angle of attack (when an information source is installed)

78

Loss of cabin pressure

33

Hydraulic pressure low

79

34

Ground speed (when an information source is installed)

80

35

Ground proximity warning system

81

Computer failure Heads-up display (when an information source is installed) Para-visual display (when an information source is installed)

36 37 38 39 40 41


Selected barometric setting (when an information source is installed) Selected altitude (when an information source is installed)

1

Landing gear position or landing gear cockpit control selection Drift angle (when an information source is installed Wind speed and direction (when an information source is installed) Latitude and longitude (when an information source is installed) Stick shaker/pusher (when an information source is installed) Windshear (when an information source is installed)

82

Cockpit trim control input position--pitch

83

Cockpit trim control input position--roll

84

Cockpit trim control input position--yaw

85

Trailing edge flap and cockpit flap control position

86

Leading edge flap and cockpit flap control position

87

Ground spoiler position and speed brake selection All cockpit flight control input forces (control wheel, control column, rudder pedal) Yaw damper status

42

Throttle/power lever position

88

43

Additional engine parameters

89

44

Traffic alert and collision avoidance system

90

Yaw damper command

45

DME 1 and 2 distances

91

Standby rudder valve status

46

Nav 1 and 2 selected frequency

N Registration

Page: 31.6


SUBJECT

31-30-03 Flight Data Interface Unit (FDIU) or Flight Data Interface function of the Flight Data Interface and Management Unit (FDIMU)

CAT

No INS

MIN REQ

A

1

0

REMARKS OR EXCEPTIONS May be inoperative provided: a) Cockpit voice Recorder (CVR) operates normally, b) Airplane is not dispatched from BOG unless: 1. The FDR failure occurs after pushback but prior to takeoff, or 2. The FDR repair was attempted but was not successful. c) In those cases where repair is attempted but not successful, the aircraft may be dispatched on a flight or series of flights until next arrival to BOG where repair must be accomplished prior to dispatch and d) Repairs are made within three flight days. Note: In the event of failures related to the “PCMCIA cards slot” in the FDIMU or connector pins of this, the aircraft dispatch remains also governed under this item. This device is an integral part of the unit FDIU (Flight Data Interface Unit)

PLACARD 31-30-03 Install INOP placard adjacent to overhead RCDR panel

Revision:32 June 30, 2015

N Registration

Page: 31.7


SUBJECT

31-30-04 RCDR System


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS DELETED, MMEL Revision 3.

N Registration

Page: 31.8


SUBJECT

31-30-05 Quick Access Recorder


CAT

No INS

MIN REQ

D

1

0

N Registration


Page: 31.9

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 31 INDICATING/RECORDING SYSTEMS SUBJECT

CAT

No INS

MIN REQ

31-30-06 Digital AIDS Recorder System

D

1

0

ITEM


N Registration


Page: 31.10


SUBJECT

31-30-07 Data Management Unit (DMU) or Data Management function of the FDIMU


CAT

No INS

MIN REQ


A

1

0

Refer to MEL 31-30-03 Note: When the Aircraft arrives to BOG or when the aircraft is dispatched from BOG must proceed with the following: -Upload FDIMU software according to AMM 3133-00-710-013. -When the uploading is not satisfactory, proceed to the replacement unit its respective software upload according to AMM 31-36-34-002 / AMM 31-36-34-402.

N Registration

Page: 31.11


SUBJECT

31-30-08 Printer


CAT

No INS

MIN REQ

D

1

0

N Registration


Page: 31.12


CAT

No INS

MIN REQ

1) DATA LOADING SELECTOR

D

1

0

2) Multipurpose Disk Drive Unit (MDDU)

D

1

0

3) Data Loading Routing Box (DLRB)

D

1

0

SUBJECT


31-38-01 Up and down Data Loading system Acquisition/Interface

PLACARD 31-38-01 Install INOP placard adjacent to Data Loader


N Registration

Page: 31.13


SUBJECT

CAT

No INS

MIN REQ

B

2

1


31-53-01 Flight Warning Computers (FWC) 1) Without Mod 35542 2) With Mod 35542

FWC 2 may be inoperative provided approach minimums do not require its use. Not applicable to Avianca. NOTE 1: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.


N Registration

Page: 31.14


SUBJECT

31-55-01 System Data Acquisition Concentrator Units (SDAC)

CAT

No INS

MIN REQ

C

2

1

REMARKS OR EXCEPTIONS SDAC 2 may be inoperative.

PLACARD 31-55-01 Install INOP placard adjacent to Upper ECAM Display


N Registration

Page: 31.15


CAT

No INS

MIN REQ

1) System Page MANUAL CALL. p.b.

C

11

0

2) CLR p.b.

C

2

1

3) T/O CONFIG p.b.

C

1

0

SUBJECT


31-56-01 ECAM Control Panel

(O) May be inoperative provided T/O configuration is verified before each departure.

PLACARD 31-56-01 Install INOP placard adjacent to ECAM Control Unit OPERATIONS (O) 31-56-01 ECAM control panel G) TO CONFIG pb When aligned on the runway PARKING BRK ………………………………………………………………….ON THRUST LEVERS ………………………………………………….SET AT 50 % N1 ONE THRUST LEVER …………………………………………………………FLX or TO Check that ECAM warning CONFIG PARK BRAKE ON appears. THRUST LEVER ……………………………………………RETARD TO 50 % N1 PARKING BRK ………………………………………………………….RELEASE Proceed with takeoff procedure.


N Registration

Page: 31.16


CAT

No INS

MIN REQ

1) Lights

C

2

1

2) CANCEL Functions

C

2

1

SUBJECT


31-58-01 Master Warn System

PLACARD 31-58-01 Install INOP placard adjacent to Master Warning Switch


N Registration

Page: 31.17


CAT

No INS

MIN REQ

1) Lights

C

2

1

2) CANCEL Functions

C

2

1

SUBJECT


31-58-02 Master Caution System

PLACARD 31-58-02 Install INOP placard adjacent to affected Master Caution light


N Registration

Page: 31.18


CAT

No INS

MIN REQ

1) ATT HDG

C

1

0

(M)May be inoperative provided: a) NORM mode operates normally, and b) Switch remains in the normal position.

2) AIR DATA

C

1

0


SUBJECT


31-61-01 EIS Switching Systems

NOTE: If EIS AIR DATA switching is inoperative, do not conduct RVSM operations. 3) EIS DMC

C

1

0


4) ECAM/ND XFR

C

1

0

May be inoperative provided: a) It operates normally in the Normal position, and b) Both ECAM DUs operate normally.

5) PFD/ND XFR

C

2

0

(O)May be inoperative provided: a) PFD and ND units are operative, and b) PFD to ND automatic switching is checked operative on the flying pilot side before each flight.

PLACARD 31-61-01 Install INOP placard adjacent to associated switch on forward switching panel OPERATIONS (O) 31-61-01 EIS switching system (PFD/ND XFR) -

During cockpit preparation:

On the side where the PFD/ND pb is inoperative : PFD Brightness control knob Check that the PFD image is automatically transferred on ND. PFD Brightness control knob

…………………………………….OFF ………………………………………ON

CAUTION: If the PFD image is not automatically transferred on the associated ND unit, the affected side cannot be used by the Pilot Flying. (Continued)


N Registration

Page: 31.19

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 31 INDICATING/RECORDING SYSTEMS ITEM 31-61-01

SUBJECT

CAT

No INS

MIN REQ


EIS Switching Systems (Continued)

On the side where the PFD to ND automatic switching is inoperative : PFD Brightness control knob …………………………………………………..OFF EIS DMC Transfer Sel (Affected side) ………………………………………….CAPT (F/O) Check that the PFD image is transferred on the associated ND unit. PFD Brightness control knob ……………………………………………………ON EIS DMC Transfer Sel (Affected side) ………………………………………………..NORM -

In flight:

If a PFD unit fails with no automatic transfer to associated ND unit : PFD Brightness control knob …………………………………………………..OFF EIS DMC Transfer Sel (Affected side) ………………………………………….CAPT (F/O) Check that the PFD image is transferred on the associated ND unit. MAINTENANCE (M) 31-61-01 -1) To deactivate ATT HDG Selector Switch refer to Aircraft Maintenance Manual (AMM) Task Number 31-6800-040-004.

MAINTENANCE (M) 31-61-01 -2) To deactivate AIR DATA Selector Switch refer to Aircraft Maintenance Manual (AMM) Task Number 3168-00-040-002. MAINTENANCE (M) 31-61-01 -3) To deactivate EIS DMC Selector Switch refer to Aircraft Maintenance Manual (AMM) Task Number 31-6800-040-003.


N Registration

Page: 31.20


CAT

No INS

MIN REQ


1) PFDU 2

C

1

0

(O) May be inoperative provided: a) PFDU1, NDU1, E/WDU, SDU and NDU2 are operative, and b) Approach minimums do not require its use.

2) NDU 1

C

1

0

(O) May be inoperative provided: a) PFDU1, NDU2, E/WDU, SDU and PFDU2 are operative, and b) Approach minimums do not require its use.

3) NDU 2

C

1

0

(O) May be inoperative provided: a) PFDU1, NDU1, E/WDU, SDU and PFDU2 are operative, and b) Approach minimums do not require its use.

A

1

0

Applicable to A318, A319, A320 and A321 except to N281AV, N284AV, N345AV, N398AV, N401AV, N411AV, N416AV, N422AV, N426AV, N446AV, N451AV, N481AV, N567AV, N599AV, N647AV, N664AV, N691AV, N729AV, N740AV, N741AV, N742AV, N743AV, N744AV, N745AV, N746AV, N748AV, N750AV, N7451AV, N753AV, N755AV, N759AV, N761AV, N763AV, N764AV N765AV, N961AV, N980AV, N992AV, aircraft only.

SUBJECT

31-63-01 Display Units (DU)

4) SDU a) Without Mod 36414/MP K11047 or Mod 38111/MP K11684)

(M)(O) May be inoperative provided: a) PFDU1, NDU1, E/WDU, PFDU2 and NDU2 are operative, b) AC ESS FEED control is verified operative once each day, and c) AC ESS FEED FAULT light is verified operative once each day. d) Repairs are made within three flight days.

(Continued)


N Registration

Page: 31.21


SUBJECT

CAT

No INS

MIN REQ


A

1

0

Applicable to N281AV, N284AV, N345AV, N398AV, N401AV, N411AV, N416AV, N422AV, N426AV, N446AV, N451AV, N481AV, N567AV, N599AV, N647AV, N664AV, N691AV, N729AV, N740AV, N741AV, N742AV, N743AV, N744AV, N745AV, N746AV, N748AV, N750AV, N751AV, N753AV, N755AV, N759AV, N761AV, N763AV, N961AV, N764AV, N765AV, N980AV, N992AV aircraft only.

31-63-01 Display Units (DU) (Continued) SDU b) With Mod 36414/MP K11047 or Mod 38111/MP K11684)

(M)(O) May be inoperative provided: a) PFDU1, NDU1, E/WDU, PFDU2 and NDU2 are operative, b) AC ESS FEED control is verified operative once each day, c) AC ESS FEED FAULT light is verified operative once each day, d) Repairs are made within three flight days, and e) The CDSS is considered inoperative (Refer to item 23-90-02) NOTE 1: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL. NOTE 2: For PBN operations refer to Appendix PBN (RNAV- RNP) operations of this MEL. PLACARD 31-63-01 Install INOP placard adjacent to associated Display Unit OPERATIONS (O) 31-63-01 1), 2) and 3) Select the corresponding knob OFF. OPERATIONS (O) 31-63-01 4) Select the corresponding knob OFF. In the case of alerts being displayed on the EWD: Use the ECAM/ND SWITCHING selector to display the system page on the selected NDU. In the case of failure of the AC BUS 1: If all the Display Units are lost: Apply the ELEC AC ESS BUS FAULT alert procedure: Refer to FCOM/PRO-ABN-24-ELECTRICAL-ELEC AC ESS BUS FAULT. Note: The AC ESS BUS is recovered when the AC ESS FEED pb-sw is set to ALTN. MAINTENANCE (M) 31-63-01 4) To Deactivation of the Lower ECAM DU when AC ESS FEED control is operative refer to Aircraft Maintenance Manual (AMM) 31-68-00-040-006. Revision: 36 June 30, 2017

N Registration

Page: 31.22


SUBJECT

CAT

No INS

MIN REQ


31-63-02 Display Management Computers 1) DMC 1 a) Aircraft with Mod. 21678/MP K1806 (AC/DC ESS PWR for ETOPS). b) Aircraft with Mod. 21678/MP K1806 (AC/DC ESS PWR for ETOPS) and Mod 34571/MP P8671 (EIS2 S42), or with Mod 36725/MP P9824 (EIS2 S7). 2) DMC 2 a) Aircraft with Mod 34571/MP P8671 (EIS2 S4-2), or with Mod 36725/MP P9824 (EIS 2 S7), or without Mod 37317/MP P10098 (AC ESS FEED Auto Switching)

Not Applicable to Avianca fleet.

C

1

0

(O) May be inoperative provided DMC 2 and DMC 3 are operative.

C

1

0

b) Aircraft without Mod 34571/MP P8671 (EIS2 S42), or without Mod 36725/MP P9824 (EIS2 S7), or with Mod 37317/MP P10098 (AC ESS FEED Auto Switching) 3) DMC 3 a) Aircraft with Mod 34571/MP P8671 (EIS2 S4-2), or Mod 36725/MP P9824 (EIS2 S7)

Applicable to A318, A319, A320 and A321

(M)(O) DMC 2 may be inoperative provided: a) AC ESS Feed Control is verified operative once each flight day, and b) AC ESS Feed Fault Light is verified operative once each flight day, and c) DMC 1 and DMC 3 are operative.

Not applicable to Avianca fleet.

C

1

0

May be inoperative provided DMC 1 and DMC 2 are operative.

C

1

0

(O) May be inoperative provided DMC 1 and DMC 2 are operative.

PLACARD Install 31-63-02 INOP placard adjacent to EIS DMC switch on switching panel (Continued) Revision: 34 May 26, 2016

N Registration

Page: 31.23


SUBJECT

CAT

No INS

MIN REQ


31-63-02 Display Management Computers (Continued) OPERATIONS (O) 31-63-02 1) ON GROUND OR IN FLIGHT In the case of multiple undue ECAM alerts concerning ENG 1(2) N1(N2) (EGT)(FF) OVER LIMIT Or ENG 1(2) N1(N2)(EGT)(EPR)(FF) DISCREPANCY Or NAV ATT(ALT1)(HDG) DISCREPANCY Or NAV FM/GPS POS DISAGREE Or FUEL F.USED/FOB DISAGREE or MINIMUM or HUNDRED ABOVE callouts, possibly associated with EFIS red flags, apply the below procedure: ‐ Crosscheck the affected parameters on the EWD, PFD, ND, or on the related SD page to confirm that the alerts are undue. ‐ EIS DMC SWITCHING selector................................................................................... NORM Note: CAPT PFD and ND ae lost when EIS DMC SWITCHING selector is set to NORM. If the undue ECAM alerts stop: ‐ Pull EIS/DMC3/SPLY (121 VU Q09) C/B and EIS/DMC3/STBY/SPLY (49 VU E10) C/B for more than 5 s and push them back. ‐ EIS DMC SWITCHING selector ..........................................................................CAPT 3 If the undue ECAM alerts continue: ‐ EIS DMC SWITCHING selector...........................................................................CAPT 3 ‐ Wait for CAPT PFD and ND recovery. ‐ Pull EIS/DMC2/SPLY (121 VU Q08) C/B for more than 5 s and push it back. OPERATIONS (O) 31-63-02 2) Applicable to A318, A319, A320 and A321 In the case of multiple undue ECAM alerts concerning ENG 1(2) N1 (N2) (EGT)(FF) OVER LIMIT Or ENG 1(2) N1 (N2)(EGT)(EPR)(FF) DISCREPANCY Or NAV ATT (ALT1)(HDG) DISCREPANCY Or NAV FM/GPS POS DISAGREE Or FUEL F.USED/FOB DISAGREE (Continued)


N Registration

Page: 31.24


SUBJECT

CAT

No INS

MIN REQ


31-63-02 Display Management Computers (Continued) Or MINIMUM or HUNDRED ABOVE callouts, possibly associated with EFIS red flags, apply the below procedure: ‐ Crosscheck the affected parameters on the EWD, PFD, ND, or on the related SD page to confirm that the alerts are undue. ‐ EIS DMC SWITCHING selector................................................................................... NORM Note: F/O PFD and ND are lost when EIS DMC SWITCHING selector is set to NORM. If the undue ECAM alerts stop: ‐ Pull EIS/DMC3/SPLY (121 VU Q09) C/B and EIS/DMC3/STBY/SPLY (49 VU E10) C/B for more than 5 s and push them back. ‐ EIS DMC SWITCHING selector ............................................................................. F/O 3 If the undue ECAM alerts continue: ‐ EIS DMC SWITCHING selector...............................................................................F/O 3 ‐ Wait for F/O PFD and ND recovery. ‐ Pull EIS/DMC1/SPLY (49 VU E11) C/B for more than 5 s and push it back. OPERATIONS (O) 31-63-02 3) ON GROUND OR IN FLIGHT In the case of multiple undue ECAM alerts concerning ENG 1(2) N1(N2) (EGT)(FF) OVER LIMIT Or ENG 1(2) N1(N2)(EGT)(EPR)(FF) DISCREPANCY Or NAV ATT(ALT1)(HDG) DISCREPANCY Or NAV FM/GPS POS DISAGREE Or FUEL F.USED/FOB DISAGREE or MINIMUM or HUNDRED ABOVE callouts, possibly associated with EFIS red flags, apply the below procedure: ‐ Crosscheck the affected parameters on the EWD, PFD, ND, or on the related SD page to confirm that the alerts are undue. ‐ EIS DMC SWITCHING selector..................................................................................CAPT 3 Note: CAPT PFD and ND are lost when EIS DMC SWITCHING selector is set to CAPT 3. If the undue ECAM alerts stop: ‐ Pull EIS/DMC1/SPLY (49 VU E11) C/B a for more than 5 s and push it back. ‐ EIS DMC SWITCHING selector ............................................................................NORM If the undue ECAM alerts continue: ‐ EIS DMC SWITCHING selector.............................................................................NORM ‐ Wait for CAPT PFD and ND recovery. ‐ Pull EIS/DMC2/SPLY (121 VU Q08) C/B for more than 5 s and push it back. MAINTENANCE (M) 31-63-02 2) To Deactivation of the DMC2 when AC ESS FEED control is operative refer to Aircraft Maintenance Manual (AMM) 31-68-00-040-005. Revision: 27 May 20, 2014

N Registration

Page: 31.25

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 31 INDICATING/RECORDING SYSTEMS SUBJECT

CAT

No INS

MIN REQ

31-63-03 ECAM Memo Display

C

2

0

ITEM

REMARKS OR EXCEPTIONS Indications may be inoperative.



N Registration

Page: 31.26


SUBJECT

31-63-04 ECAM Permanent Data Display

CAT

No INS

MIN REQ

C

3

0

REMARKS OR EXCEPTIONS Indications may be inoperative provided TAT or SAT temperature is available.



N Registration

Page: 31.27


SUBJECT

CAT

No INS

MIN REQ




N Registration

Page: 31.28

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 32 LANDING GEAR ITEM 32-00

SUBJECT

CAT

No INS

MIN REQ


CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) Fault(s) Indicated by BRAKES


Deleted, MMEL REV 21.

N Registration

Page: 32.1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 32 LANDING GEAR SUBJECT

CAT

No INS

32-11-01 Torque Link Dampers

A

2

ITEM


MIN REQ

0

REMARKS OR EXCEPTIONS May be inoperative provided repairs are made within seven flights legs.

N Registration

Page: 32.2

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 32 LANDING GEAR ITEM

SUBJECT

CAT

No INS

MIN REQ

C

2

0


32-12-01 MAIN GEAR DOORS 1) Ground Opening Cables

(M) May be broken or missing.

MAINTENANCE (M) 32-12-01 To Preparation of the Aircraft for Flight with a Failed or Missing Ground Door Opening Cable refer to AMM 32-12-00-040-006.


N Registration

Page: 32.3


SUBJECT

32-31-00 Landing Gear Retraction System

CAT

No INS

MIN REQ


B

1

0

(M)(O) Except for ER operations, may be inoperative provided the airplane is operated with landing gear down in accordance with the AFM supplement for gear down flight.

OPERATIONS (O) 32-31-00 Notify Dispatch Landing Gear retracting system Refer to FCOM/PRO-SPO-25-FLIGHT WITH GEAR DOWN. MAINTENANCE (M) 32-12-01 To deactivation of the Landing Gear Retracting System refer to AMM 32-31-00-040-803.


N Registration

Page: 32.4


CAT

No INS

MIN REQ


(A318/A319ceo/ A320ceo/A321ceo)

A

1

0

(M)(O) LGCIU No.2 may be inoperative provided: a) Both radio altimeter systems operate normally, b) Both FCU channels operate normally, c) All ELACs, SECs, ADIRs, SFCCs and FACs operate normally, d) Flex takeoff is not used, and e) Reverser No. 2 is considered inoperative, f) LGCIU No. 2 is deactivated, g) Alternate procedures are established and used to account for inoperative systems/functions related to the deactivated No. 2 LGCIU, and h) Repairs are made within one flight day. NOTE 1: As a result of a deactivated LGCIU 2 multiple systems are affected. NOTE 2: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.


A

1

0

Applicable to N759AV, N761AV, N764AV, N765AV

SUBJECT

32-31-01 Landing Gear Control And Interface Units No. 2 (LGCIU 2)

(M)(O) LGCIU No. 2 may be inoperative provided: a) Both radio altimeter systems operate normally, b) Both FCU channels operate normally, c) All ELACs, SECs, ADIRs, SFCCs, and FACs operate normally, d) Flex takeoff is not used, e) Reverser No. 2 is considered inoperative, f) LGCIU No. 2 is deactivated, g) Alternate procedures are established and used to account for inoperative systems/functions related to the deactivated No. 2 LGCIU, h) Repairs are made within 1 flight day, and i) The OAT is below ISA+35 degrees C. NOTE 1: As a result of a deactivated LGCIU 2 multiple systems are affected. NOTE 2: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL (Continued) Revision: 36 June 30, 2017

N Registration

Page: 32.5


SUBJECT

CAT

No INS

MIN REQ


32-31-01 Landing Gear Control And Interface Units (LGCIU) (Continued) OPERATIONS (O) 32-31-01 During cockpit preparation: C/B HYDRAULIC/LGCIU/SYS2 (121VU Q35) ……………………………………………..PULL The following table gives the consequences on the systems affected when LGCIU2 is inoperative and above mentioned C/B is pulled

.


N Registration

Page: 32.6


SUBJECT

CAT

No INS

MIN REQ


32-31-01 Landing Gear Control And Interface Units (LGCIU) (Continued)

In case of loss of the second LGCIU, AP and FD are lost, consequently CAT II approaches are not possible. For CAT I approaches, refer to applicable regulations. MIANTENANCE (M) 32-31-01 For the Maintenance procedure to deactivate of the Thrust Reverser System 2; refer to MEL 78-30-01


N Registration

Page: 32.7


CAT

No INS

32-33-01 Landing Gear Gravity Extension System

B

1

ITEM

MIN REQ


0

(M)(O) Except for ER operations, may be inoperative provided the airplane is operated with landing gear down in accordance with the AFM supplement for gear down flight.

OPERATIONS (O) 32-33-01 Notify dispatch. Landing Gear Gravity Extension System Refer to FCOM/PRO-SPO-25-FLIGHT WITH GEAR DOWN. MAINTENANCE (M) 32-33-01 To Deactivation of the Landing Gear Gravity-Extension System refer to AMM 32-31-00-040-802.


N Registration

Page: 32.8


SUBJECT

32-41-01 Wheel Tie Bolts Nose Wheel Tie Bolts Main Wheel Tie Bolts

CAT

No INS

MIN REQ

A A

12 18

11 17


(M) One bolt may be broken or missing provided: a) Affected wheel is removed, checked for broken parts or damage, and replaced if broken parts or damage is found, b) For the main wheel, associated brake is checked for broken parts or damage, and is replaced or deactivated if broken parts or damage is found, c) After each landing, wheel is inspected for additional broken or missing tie bolts, and d) Repairs are made within five flight legs. MAINTENANCE (M) 32-41-01 -

To Check of the Nose Wheel when one tie bolt is missing refer to AMM Task 32-41-00-040-002. To Check of the Main Wheel when one tie bolt is missing refer to AMM Task 32-41-00-040-003.


N Registration

Page: 32.9


SUBJECT

32-42-01 Main Wheel Braking Systems

CAT

No INS

MIN REQ


C

4

3

(M)(O)One brake may be inoperative provided: a) Minimum runway width is 148 feet (45 meters), b) Anti-skid system operates normally, c) Nose wheel steering operates normally, d) Affected brake is removed or deactivated, e) Both reversers operate normally, f) Green and yellow systems on operative brakes operate normally, g) Wheel tachometers are operative, h) AFM performance penalties are applied i) Approach minimums do not require its use, and j) The AUTO/BRK Function is considered inoperative.

OPERATIONS (O) 32-42-01 (Applicable to A318-111, A318-112, A319-112, A319-115, A320-214 aircraft except to A320-200 with Sharklets) Notify dispatch. FLIGHT PREPARATION/LIMITATIONS Maximum landing capability is CAT 3 Single. The following penalties may be used for takeoff and landing performance determination if no takeoff and landing data (predetermined by using OCTOPUS program or other equivalent program with present failure case) is available. Takeoff performance computation: The method explained hereafter allows the determination of the MTOW and associated speeds (V1, VR, V2), by applying decrements on the MTOW and associated speeds computed in normal conditions (i.e. all systems operative). The method is based on the use of RTOW charts established at optimum V2/VS, optimum V1/VR, minimum V1. WARNING ‐ Do not use this method with takeoff charts computed with other conditions. ‐ Do not use this method for takeoff with tailwind. ‐ Do not use this method for takeoff on wet or contaminated runways. How to proceed? ‐ Read, in 0 kt wind column of the takeoff chart computed in normal condition, the MTOW and associated speeds (V1, VR, V2) corresponding to the actual temperature, even in the case of headwind (the method does not take into account the headwind benefit on takeoff performance). ‐ Apply the QNH and/or bleed corrections, if any, to determine the MTOW. ‐ Enter the following table to determine the MTOW and speed decrements. ‐ Applying these decrements, calculate the MTOW and associated speeds corresponding to the actual temperature. CAUTION: Do not extrapolate below the shortest runway length provided by the table. (Continued) Revision: 36 June 30, 2017

N Registration

Page: 32.10

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 32 LANDING GEAR ITEM 32-42-01

SUBJECT

CAT

No INS

MIN REQ


Main Wheel Braking Systems (Continued)




(Continued)


N Registration

Page: 32.11


SUBJECT

CAT

No INS

MIN REQ


32-42-01

Main Wheel Braking Systems (Continued) Applicable to A319-115 except N723AV and N726AV:


If the actual TOW is lower than the MTOW calculated using above method: The speeds determined without failure and associated with the actual TOW may be retained provided that they are all lower than the speeds calculated using above method. Check that the corrected V1 is equal to or above the minimum V1 value shown on the RTOW chart (due to VMCG limitation). If the corrected V1 is lower than the minimum V1: Take this last value as V1. Further decrease the weight by 3 000 kg (6 600 lb) per kt difference between both values. Check that the corrected VR is equal to or above the minimum VR value shown on the RTOW chart (due to VMCA limitation). If the corrected VR is lower than the minimum VR: Takeoff cannot be performed using this method. Check that the corrected V2 is equal to or above the minimum V2 value shown on the RTOW chart (due to VMCA limitation). If the corrected V2 is lower than the minimum V2: Takeoff cannot be performed using this method. (Continued) Revision: 36 June 30, 2017

N Registration

Page: 32.12


SUBJECT

CAT

No INS

MIN REQ



Check that the corrected V2 is equal to or above the minimum V2 due to VMU limitation (see Refer to FCOM/PER-TOF-TOD-25-20 MINIMUM V2 LIMITED BY VMU/VMCA (KT IAS)). If the corrected V2 is lower than the minimum V2: Takeoff cannot be performed using this method. Landing performance computation: Multiply the landing distances by 1.20 (Applicable to A318-111 and A320-214). Multiply the landing distances by 1.25 (Applicable to A318-112, A319-112 and A319-115) FOR TAKEOFF The autobrake function, even if available, must not be used. If the above method was used for takeoff performance computation: Perform the takeoff using full thrust (TOGA). In the case of engine failure at takeoff: Retract the landing gear when positive climb. Vibrations may occur during 1 or 2 min after the retraction of the landing gear. If both engines are operative: Keep the landing gear down for 1 min. FOR LANDING The autobrake function, even if available, must not be used. OPERATIONS (O) 32-42-01 (Applicable to A319-132, A320-233, A321-231, A321-211 and N723AV and N726AV) FLIGHT PREPARATION/LIMITATIONS Maximum landing capability is CAT 3 Single. Takeoff and landing performance computation: The takeoff and landing performance must be determined by using OCTOPUS program or other equivalent program with present failure case taken into accoun. Launch PEP. Landing performance computation: Multiply the landing distances by 1.25 (Applicable to A319-132, A321-211, N723AV and N726AV) Multiply the landing distances by 1.30 (Applicable to A320-233 and A321-231) FOR TAKEOFF The autobrake function, even if available, must not be used. In the case of engine failure at takeoff: Retract the landing gear when positive climb. Vibrations may occur during 1 or 2 min after the retraction of the landing gear. If both engines are operative: Keep the landing gear down for 1 min. FOR LANDING The autobrake function, even if available, must not be used. (Continued) Revision: 36 June 30, 2017

N Registration

Page: 32.13


SUBJECT

CAT

No INS

MIN REQ



OPERATIONS (O) 32-42-01. (Applicable to A320-200 with Sharklets, A320-251N (NEO) and A321253N (NEO)) FLIGHT PREPARATION/LIMITATIONS Maximum landing capability is CAT 3 Single. Takeoff and landing performance computation: The takeoff and landing performance must be determined by using OCTOPUS program or other equivalent program with present failure case taken into account or refer to Dispatch guide. Launch PEP. Landing performance computation: Multiply the landing distances by 1.20 FOR TAKEOFF The autobrake function, even if available, must not be used. In the case of engine failure at takeoff: Retract the landing gear when positive climb. Vibrations may occur during 1 or 2 min after the retraction of the landing gear. If both engines are operative: Keep the landing gear down for 1 min. FOR LANDING The autobrake function, even if available, must not be used. MAINTENANCE (M) 32-42-01 To deactivation of the Main Wheel Brakes refer to Aircraft Maintenance Manual (AMM) 32-42-00-040-003.


N Registration

Page: 32.14


SUBJECT

CAT

No INS

MIN REQ


32-42-02 Green Braking System 1) Without Mod. 25410 2) With Mod. 25410

Not applicable to Avianca. C

1

1

(M)(O) Braking on one wheel may be inoperative provided: a) Minimum runway width is 148 feet (45 meters), b) Green hydraulic supply to affected brake is deactivated, c) Anti-skid system operates normally, d) Nose wheel steering operates normally, e) Both reversers operate normally, f) Wheel tachometers are operative, and g) AFM performance penalties are applied.

OPERATIONS (O) 32-42-02 Notify dispatch. Green brake system Refer to operational procedure of item 32-42-01 MAINTENANCE (M) 32-42-02 To Deactivation of the Normal Braking - With disconnection of the Green Hydraulic Supply refer to Aircraft Maintenance Manual (AMM) 32-42-00-040-002.


N Registration

Page: 32.15


SUBJECT

CAT

No INS

MIN REQ


C

1

0

(M)(O) May be inoperative provided: a) Alternate brake system is verified to operate normally before each departure, b) Brake pressure indicators operate normally. c) The affected channel/system is deactivated, d) Prior to each flight, the CFDS does not indicate a L/G SYS DISAGREE caution, e) Channel 2/System 2 is operative, and f) The AUTO/BRK (LO, MED, MAX) pb-sw DECEL lights and the AUTO/BRK (LO, MED, MAX) pb.sw ON lights are considered inoperative.

32-42-03 Braking/ Steering Control Unit (BSCU) Channels/Systems 1) Channel 1/System 1 a) Aircraft without Mod.36853/ MP P9655 (BSCU STD L4.9) or with Mod. 36853/MP P9655 and Mod. 38973/MP P10891(BSCU STD L4.9B)

NOTE: These provisos apply to all BSCU standards except EM2 L4.9 only. b) Aircraft with Mod. 36853/MP P9655 (BSCU STD L4.9) and Without Mod. 38973/MP P10891(BSCU STD L4.9B)

Not applicable. Applicable to Aircraft With Mod. 36853/MP P9655 and Without Mod. 38973/MP P10891.

2) Channel 2/System 2 a) Aircraft without Mod. 36853/MP P9655 (BSCU STD L4.9) or with Mod. 36853/MP P9655 and Mod. 38973/MP P10891(BSCU STD L4.9B)

C

1

0

(M)(O) May be inoperative provided: a) Alternate brake system is verified to operate normally before each departure, and b) Brake pressure indicators operate normally. c) The affected channel/system is deactivated, d) Prior to each flight, the CFDS does not indicate a L/G SYS DISAGREE caution, and e) Channel 1/System 1 is operative. NOTE: These provisos apply to all BSCU standards except EM2 L4.9.

b) With Mod. 36853/MP P9655 (BSCU STD L4.9) and Without Mod. 38973/MP P10891(BSCU STD L4.9B)

Not applicable. Applicable to Aircraft With Mod. 36853/MP P9655 and Without Mod. 38973/MP P10891.


N Registration

Page: 32.16


SUBJECT

CAT

No INS

MIN REQ


32-42-03 Braking/ Steering Control Unit (BSCU) Channels/Systems (Continued) PLACARD Install 32-42-03 – INOP Placard adjacent to lower ECAM display OPERATIONS (O) 32-42-03 Brake pressure indicators must operate normally. Alternate brake system must be verified to operate normally by performing procedure during preflight: 1) 2) 3) 4) 5) 6) 7)

Ensure aircraft wheels are chocked and green and yellow hydraulic systems pressure is zero. Place parking brake to off. Check brake accumulator pressure indicator is in green band. Depress brake pedals and monitor triple pressure indicator for an increment of the pressure indication on each brake. If brakes pressure increases, check is satisfactory. If pressure on each brake does not increase in proportion to pedal deflection, notify maintenance. Place parking brake on. On taxi out, accomplish normal SOP brake check.

MAINTENANCE (M) 32-42-03 Refer to AMM TASK 32-42-00-040-007 Deactivation of the BSCU Channel/System 1 or 2


N Registration

Page: 32.17


SUBJECT

32-42-04 AUTO/BRK Function

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS (O) May be inoperative provided: a) Approach minimums do not require its use, and b) Normal braking is not affected.

1) AUTO/BRK Panel Mode Lights (LO, MED, MAX) a) ON

b) DECEL

C

3

0

May be inoperative provided Auto Brake indications on ECAM WHEEL page operate normally.

C

3

0

May be inoperative provided associated autobrake mode is not used.

C

3

0

May be inoperative provided Auto Brake indications on ECAM WHEEL page operate normally.

C

3

0

May be inoperative provided associated autobrake mode is not used.

PLACARD Install 32-42-04 – INOP placard adjacent to Autobrake Select panel 402 VU OPERATIONS (O) 32-42-04 If AUTO/BRK Panel Mode Lights (LO, MED, MAX) are inoperative: 1. Verify Auto Brake indications on ECAM Wheel page operate normally before each departure FLIGHT PREPARATION/LIMITATIONS Maximum landing capability is CAT 3 SINGLE. BEFORE TAKEOFF When T.O MEMO is displayed on the EWD, disregard the line: AUTO BRK....................................................................................................................... MAX (blue)


N Registration

Page: 32.18


SUBJECT

32-42-05 Tachometer


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Deleted, Rev 20 MMEL

N Registration

Page: 32.19


SUBJECT

32-42-06 Nose Wheel Brake Pads (Without Mod. 28482)


CAT

No INS

MIN REQ


Not applicable to Avianca. Avianca fleet has incorporated Mod. 28482

N Registration

Page: 32.20


CAT

No INS

32-44-01 Yellow Brake System

C

1

ITEM

MIN REQ

1

REMARKS OR EXCEPTIONS (M) Braking on one wheel may be inoperative provided: a) Yellow hydraulic supply of affected brake is deactivated, and b) Both reversers operate normally.

MAINTENANCE (M) 32-44-01 To Deactivation of the Alternate Braking with disconnection of the Yellow Hydraulic Supply refer to AMM 32-43-00-040-001.


N Registration

Page: 32.21


SUBJECT

CAT

No INS

MIN REQ


32-44-02 ACCU PRESS Indicator 1) Without Mod 31441 2) With Mod 31441

Not Applicable to Avianca Avianca fleet has Mod. 31441. C

1

0

(M) May be inoperative provided: a) Both brake pressure indicators operate normally, and b) Pressure on both brake pressure indicators is verified with parking brake on.

C

1

0

(O) May be inoperative provided: a) ACCU PRESS/ACCU ONLY indication is available on ECAM WHEEL page, and b) Hydraulic pressure of the brake accumulator is checked on ECAM WHEEL page before each flight.

OPERATIONS (O) 32-44-02 DURING COCKPIT PREPARATION ‐ YELLOW ENG 2 PUMP pb-sw...............................................................................................OFF ‐ YELLOW ELEC PUMP pb-sw...................................................................................................Off ‐ Move a side stick in pitch and roll until the yellow system pressure indication on the HYD SD page indicates 0. ‐ PARK BRK handle....................................................................................................................ON ‐ BRAKES pressure............................................................................................................. CHECK On the WHEEL SD page, check that the ACCU PRESS or ACCU ONLY indication is displayed in green. If required, use the electric pump on the yellow hydraulic system to recharge the brake accumulators. WARNING Yellow and green hydraulics systems are pressurized from yellow electric pump. Get ground crew clearance before using the electric pump. ‐ Restore normal settings.

MAINTENANCE (M) 32-44-02 Verify Both brake pressure indicators operate normally, and Pressure on both brake pressure indicators is verified with parking brake on. Install 32-44-02 – INOP placard adjacent to Brake and Accumulator triple indicator on forward instrument panel.


N Registration

Page: 32.22


SUBJECT

32-44-03 BRAKES Pressure Indicators

CAT

No INS

MIN REQ


C

2

1

(O) One may be inoperative provided both BSCU channels/systems operate normally.

PLACARD Install 32-44-03 – INOP placard adjacent to Brake and Accumulator triple indicator on forward instrument panel. OPERATIONS (O) 32-44-03 Check ECAM STS page that BSCU MSG is (are) not present.


N Registration

Page: 32.23


CAT

No INS

32-45-02 Parking Brake External Light

C

1

ITEM


MIN REQ


0

May be inoperative provided parking brake status is verified before moving aircraft.

N Registration

Page: 32.24


SUBJECT

CAT

No INS

MIN REQ

C

2

0

32-47-01 Brake Temperature Monitoring Unit

REMARKS OR EXCEPTIONS (O) May be inoperative provided brake ground cooling time is applied.

OPERATIONS (O) 32-47-01 Notify Dispatch Brake temperature monitoring unit HYDRAULIC/BRK/TEMP/DET/UNIT (121VU M26 or M37) C/B................................................PULL FLIGHT PREPARATION/ LIMITATIONS The brake energy graph and the brake cooling time table given hereafter permit to determine the ground brake cooling time:

OP Proc BRAKE ENERGY GRAPH If MAX reverser thrust was selected for all reversers during the braking phase: Enter the brake energy graph: WITH THRUST REVERSERS USE. If MAX reverser thrust was NOT selected for all reversers during the braking phase: Enter the brake energy graph: WITHOUT THRUST REVERSERS USE. Determination of the brake energy accumulated during a REJECTED TAKEOFF (RTO): ‐ Enter with the aircraft takeoff weight (TOW) and with the rejected takeoff speed in kt IAS). ‐ Apply airport pressure altitude, temperature, wind and runway slope corrections. Determination of the brake energy accumulated during a LANDING: ‐ Enter with the aircraft landing weight, and ‐ Enter with the touch down speed in kt IAS if the autobrake was selected and applied or with the manual braking speed in kt IAS in the other cases. ‐ Apply airport pressure altitude, temperature, wind and runway slope corrections. ‐ Correct for brake setting with a preselected autobrake setting (LO, MED) or with MAX PEDAL braking in the other cases Note: In the case of a dispatch with one brake inoperative (Refer to Item 32-42-01 Main Wheel Brake or Refer to Item 32-42-02 Green System Brake), the brake energy accumulated is increased by 34 %. Determine the Ground Brake Cooling Time (MN) with the energy (MJ) and OAT using the Ground Brake Cooling Time (MN) Table. (Continued)


N Registration

Page: 32.25


SUBJECT

CAT

No INS

MIN REQ


32-47-01 Brake Temperature Monitoring Unit (Continued) For A321 except A321-253N (neo)


N Registration

Page: 32.26


SUBJECT

CAT

No INS

MIN REQ


32-47-01 Brake Temperature Monitoring Unit (Continued) For A321 except A321-253N (neo)


N Registration

Page: 32.27


SUBJECT

CAT

No INS

MIN REQ


32-47-01 Brake Temperature Monitoring Unit (Continued) For A321-253N (neo)


N Registration

Page: 32.28


SUBJECT

CAT

No INS

MIN REQ


32-47-01 Brake Temperature Monitoring Unit (Continued) For A321-253N ( neo )


N Registration

Page: 32.29


SUBJECT

CAT

No INS

MIN REQ


Brake Temperature Monitoring Unit 32-47-01 (Continued) For A320 except A320-251N ( neo)


N Registration

Page: 32.30


SUBJECT

CAT

No INS

MIN REQ


32-47-01 Brake Temperature Monitoring Unit (Continued) For A320 except A320-251N ( neo)


N Registration

Page: 32.31


SUBJECT

CAT

No INS

MIN REQ


32-47-01 Brake Temperature Monitoring Unit (Continued) For A320-251N ( neo)


N Registration

Page: 32.32


SUBJECT

CAT

No INS

MIN REQ




N Registration

Page: 32.33


SUBJECT

CAT

No INS

MIN REQ


32-47-01 Brake Temperature Monitoring Unit (Continued) For A319

(Continued)


N Registration

Page: 32.34


SUBJECT

CAT

No INS

MIN REQ




N Registration

Page: 32.35


SUBJECT

CAT

No INS

MIN REQ




N Registration

Page: 32.36


SUBJECT

CAT

No INS

MIN REQ



(Continued)


N Registration

Page: 32.37


SUBJECT

CAT

No INS

MIN REQ


32-47-01 Brake Temperature Monitoring Unit (Continued) Applicable to all A318/A319/A320/A321 except A320-251N (neo) and A321-253N (neo)


N Registration

Page: 32.38


SUBJECT

CAT

No INS

MIN REQ



( Continued)


N Registration

Page: 32.39


SUBJECT

CAT

No INS

MIN REQ


32-47-01 Brake Temperature Monitoring Unit (Continued) For A320-251N (neo)

( Continued )


N Registration

Page: 32.40


SUBJECT

CAT

No INS

MIN REQ


32-47-01 Brake Temperature Monitoring Unit (Continued) AFTER ENGINE START In the case of a false BRAKES HOT alert displayed on the EWD: EMER CANC pb................................................................................................................. Press Note: In the case of a false BRAKES HOT alert due to a faulty BTMU or a faulty BSCU, the "T.O CONFIG NORMAL” line will not replace the "T.O CONFIG . . TEST" line in the T.O MEMO. Consider normal configuration for takeoff provided that no alert was displayed during the T.O CONFIG TEST.

CAUTION


The T.O CONFIG TEST pb must be maintained pressed to check that there is no alert.

N Registration

Page: 32.41


SUBJECT

32-48-01 Brake Fan System

CAT

No INS

MIN REQ

D

1

0

REMARKS OR EXCEPTIONS Applicable to all A321 and N764AV and N765AV

PLACARD Install 32-48-01 INOP placard adjacent to Brake Cooling Fan switch on forward instrument panel.


N Registration

Page: 32.42


SUBJECT

32-48-02 BRAKE FAN HOT Light

CAT

No INS

MIN REQ


D

1

0

Applicable to all A321 and N764AV and N765AV

PLACARD Install 32-48-02 INOP placard adjacent to Brake Fan Hot Light on forward instrument panel.


N Registration

Page: 32.43


SUBJECT

32-48-03 BRK FAN ON Light

CAT

No INS

MIN REQ


D

1

0

Applicable to all A321 and N764AV and N765AV NOTE: Brake Fan operation may be checked through the brake fan ECAM MEMO.

PLACARD Install 32-48-03 INOP placard adjacent to Brake Fan On Light on forward instrument panel.


N Registration

Page: 32.44


SUBJECT

32-49-01 ECAM Tire Pressure Indications


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not Applicable to Avianca. System not installed on Avianca fleet.

N Registration

Page: 32.45


SUBJECT

32-49-02 Tire Pressure Monitoring System


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not Applicable to Avianca. System not installed on Avianca fleet.

N Registration

Page: 32.46


SUBJECT

CAT

No INS

MIN REQ


32-49-03 Warning and Caution on ECAM EWD 1) WHEEL TYRE LO PR Caution on ECAM EWD


Not applicable. Applicable to Aircraft with WHEEL TYRE LO PR Caution on ECAM EWD installed.

N Registration

Page: 32.47


SUBJECT

32-51-01 Nose Wheel Steering System


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Deleted Rev 20 MMEL

N Registration

Page: 32.48


SUBJECT

32-51-02 PEDALS DISC p.b.

CAT

No INS

MIN REQ

C

2

0

REMARKS OR EXCEPTIONS (O) May be inoperative in the released position (No disconnection possible and NWS still available by rudder pedals).

PLACARD Install 32-51-02 – INOP placard adjacent to associated handwheel OPERATIONS (O) 32-51-02 OPTION 1: When the disconnection is not possible on one side, the rudder flight control check must be performed by the pilot with operative pedal disconnect pb switch. OPTION 2: When the disconnection is not possible on both sides, the rudder flight control check must be performed while aircraft is stopped.


N Registration

Page: 32.49


SUBJECT

32-51-03 Nose Wheel Steering Control System Deactivation Device (for A/C Towing)

CAT

No INS

MIN REQ

C

1

0

(O) May be inoperative (no towing mode when lever in TOWING position)

C

1

0

(M)(O) May be inoperative provided the NWS electrical deactivation box is deactivated.


OPERATIONS (O) 32-51-03 Nose Wheel Steering Control System Deactivation Device (for A/C Towing) Before pushback : A/SKID and N/W STRG selector ………………………………………………………………………OFF In addition, as a result of the NWS Electrical Box deactivation, the parking brake light on that box will not be available. Parking brake setting will need to be verbally confirmed between flight crew and maintenance before pushback. After pushback : A/SKID and N/W STRG selector ………………………………………………………………………….ON OPERATIONS (O) 35-51-03 NWS electrical deactivation box is deactivated DURING COCKPIT PREPARATION After application of the maintenance procedure: Check that the WHEEL N/W STRG FAULT or WHEEL N.W STEER FAULT alert is not displayed anymore on the EWD. If the ECAM alert is still displayed, consider the nosewheel steering inoperative. Refer to FCOM/PRO-NORSUP-LG Operations with Nosewheel Steering Offset-General BEFORE PUSHBACK A/SKID & N/W STRG selector.............................................................................................................. OFF As a result of the NWS electrical box deactivation, the parking brake light on that box will not be available. The parking brake setting must be verbally confirmed between the flight crew and the ground personnel before pushback. AFTER PUSHBACK A/SKID & N/W STRG selector................................................................................................................ ON

MAINTENANCE (M) 32-51-03 To Deactivation of the Nose - Wheel Steering Electrical Deactivation - Box (for Flight) refer to Aircraft Maintenance Manual (AMM) 32-51-00-040-002.


N Registration

Page: 32.50


SUBJECT

32-60-01 LDG Gear Indicator Panel (UNLK and/or Down & Locked Triangle Indications)

CAT

No INS

MIN REQ


B

1

0

(O) May be inoperative provided: a) Both landing gear position indications (on ECAM wheel page) for all three landing gear operate normally, and b) Upper and lower ECAM display units operate normally.

PLACARD Install 32-60-01 – INOP placard adjacent to Landing Gear panel 402 VU OPERATIONS (O) 32-60-01 Use the ECAM wheel page to monitor landing gear position.


N Registration

Page: 32.51


SUBJECT

CAT

No INS

MIN REQ

B

1

0


32-60-02 Gear Not Down Indication 1) Red DOWN Arrow Light

(M) May be inoperative provided GEAR NOT DOWN caution on ECAM operates normally.

PLACARD Install 32-60-02 INOP placard adjacent to Landing Gear lever. MAINTENANCE (M) 32-60-02 To Operational Check of the ECAM Landing Gear NOT DOWN Warning refer to Aircraft Maintenance Manual (AMM) 32-61-00-040-001.


N Registration

Page: 32.52


CAT

No INS

MIN REQ

1) UP LOCK

C

3

0

2) L/G Doors

C

3

0

3) L/G CTL

C

1

0

4) REL

C

4

0

5) ANTI SKID/ ANTI SKID [1,2]

C

1

0

SUBJECT


32-60-03 ECAM Wheel Page Indications

May be inoperative provided MAX SPEED is limited to 250KTS/M.60.

(M) May be inoperative provided antiskid system operates normally. NOTE : For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.

6) AUTO BRK

C

1

0

(O) May by inoperative provided Auto Brake Mode Lights operate normally.

C

1

0

May be inoperative provided AUTO/BRK Function is not used.

7) Brakes Temperatures

C

4

0

(M)(O) May be inoperative provided ground brake cooling time is applied.

8) L/G Position

C

6

3

May be inoperative provided gear position indications are available on landing gear indicator panel.

9) [Y]N/W STEERING (With Mod 31441)

C

2

0

10) [G] NORM BRK (With Mod 31441)

C

2

0

11) [Y] ALTN BRK (With Mod 31441)

C

2

0

12) ACCU PRESS/ ACCU ONLY (With Mod 31441)

C

1

0

OPERATIONS (O) 32-60-03 -6) AUTO BRK Prior to each take-off, select lights test switch to test and verify Auto Brake Mode Lights illuminate. (Continued) Revision: 36 June 30, 2017

N Registration

Page: 32.53


SUBJECT

CAT

No INS

MIN REQ


32-60-03 ECAM Wheel Page Indications (Continued) OPERATIONS (O) 32-60-03 -7) Brakes Temperature In case of false BRAKE HOT caution: After engine start clear the brakes hot caution by depressing the EMER CANC pb. Note: In-case of erroneous triggering of the ECAM caution BRAKES HOT due to a faulty BTMU or a faulty BSCU, after having performed the TO CONFIG TEST, the T.O. MEMO display line will not be replaced by the line "TO CONFIG NORMAL" and will remain displayed. Consider normal configuration for TO provided no warning presented during TO CONFIG TEST. CAUTION: The TO CONFIG TEST pb must be maintained pressed while checking no warning presented. The brake energy graph and the brake cooling time table given hereafter allow to determine the ground brake cooling time. BRAKE ENERGY GRAPH - Enter the brake energy graph : WITH THRUST REVERSERS USE, if MAX REV was selected for all reversers during the braking phase, or WITHOUT THRUST REVERSERS USE , if MAX REV was NOT selected for all reversers during the braking phase. -

Determination of the brake energy accumulated during a REJECTED TAKEOFF (RTO) :  Enter with the aircraft takeoff weight (TOW) and with V1 (Decision speed in kt IAS).  Apply airport pressure altitude, temperature, wind and runway slope corrections. Determination of the brake energy accumulated during a LANDING :  Enter with the aircraft landing weight and with touch down speed in kt IAS.  Apply airport pressure altitude, temperature, wind and runway slope corrections.  Correct for brake setting with a preselected autobrake setting AUTO/BRK (LO, MED) or with MAX PEDAL braking in the other cases.

BRAKE COOLING TIME TABLE - Determination of the ground brake cooling time : Enter the following table with the energy and the OAT to determine the ground brake cooling time. (Continued)


N Registration

Page: 32.54


SUBJECT

CAT

No INS

MIN REQ


32-60-03 ECAM Wheel Page Indications (Continued) For A321

(Continued)


N Registration

Page: 32.55


SUBJECT

CAT

No INS

MIN REQ


ECAM wheel page Indications (Continued)

For A321

(Continued)


N Registration

Page: 32.56


SUBJECT

CAT

No INS

MIN REQ


For A320

(Continued)


N Registration

Page: 32.57


SUBJECT

CAT

No INS

MIN REQ




N Registration

Page: 32.58


SUBJECT

CAT

No INS

MIN REQ




N Registration

Page: 32.59


SUBJECT

CAT

No INS

MIN REQ




N Registration

Page: 32.60


SUBJECT

CAT

No INS

MIN REQ




N Registration

Page: 32.61


SUBJECT

32-60-03

CAT

No INS

MIN REQ


ECAM Wheel Page Indications (Continued)

For A318


N Registration

Page: 32.62


SUBJECT

CAT

No INS

MIN REQ


32-60-03 ECAM Wheel Page Indications (Continued)


N Registration

Page: 32.63


SUBJECT

CAT

No INS

MIN REQ


32-60-03 ECAM Wheel Page Indications (Continued) MAINTENANCE (M) 32-60-03 -5) Refer to Aircraft Maintenance Manual (AMM) Task Number 32-60-00-040-001, Anti Skid Indication on ECAM WHEEL Page

MAINTENANCE (M) 32-60-03 -7) Refer to MEL AMM supplement: AMM task 32-47-00-040-001-A


N Registration

Page: 32.64


SUBJECT

32-60-04 Fault(s)Indicated by BRAKES N/WS MINOR FAULT Caution on ECAM E/WD 1) A318/A319ceo/ A320ceo/A321ceo with Mod 26925/MP P4576 (Alt. Braking) and without Mod. 38973/MP P10891 (BSCU STD L4.9B)

2) A318/A319ceo/ A320ceo/A321ceo with Mod. 26925/MP P4576 (Alt Braking) and with Mod.38973/ MP P10891 (BSCU STCL4.9B) and A319 neo/ A320neo/A321neo Revision: 36 June 30, 2017

CAT

No INS

MIN REQ


B

2

0

B

2

0

B

2

0

Applicable A318 aircraft only. (M)(O) May be displayed provided: a) BSCU system 1 and system 2 operate normally, and b) It is checked prior to each departure that the following CFDS failure messages related to BRAKES N/WS MINOR FAULT are not displayed: - A fault on the Alternate Braking Control Unit (ABCU), - A fault on the Alternate Braking Selector Valve, - A fault on the Alternate Braking Servovalve, or - A degraded pressure on an Alternate Servo-valve. Applicable A318 aircraft only. (M)(O) May be displayed provided: a) BRAKES pressure indicators operate normally, b) Alternate braking system is checked operative before the first flight of each day, and c) It is checked prior to each departure that the following CFDS failure messages related to BRAKES N/WS MINOR FAULT are not displayed: - A fault on the Alternate Braking Control Unit (ABCU), - A fault on the Alternate Braking Selector Valve, - A fault on the Alternate Braking Servovalve, - A fault on the Alternate Pressure Transducer, or - A degraded pressure on an Alternate Servo-valve. Applicable to A319, A320 and A321 aircraft only May be displayed provided BSCU system 1 and system 2 operate normally.

(Continued) N Registration

Page: 32.65


SUBJECT

CAT

No INS

MIN REQ

B

2

0


32-60-04 Fault(s)Indicated by BRAKES N/WS MINOR FAULT Caution on ECAM E/WD (Continued) 2) A318/A319ceo/ A320ceo/A321ceo with Mod. 26925/MP P4576 (Alt Braking) and with Mod.38973/ MP P10891 (BSCU STCL4.9B) and A319 neo/ A320neo/A321neo

Applicable to A319, A320 and A321 aircraft only (M)(O) May be displayed provided: a) BRAKES pressure indicators operate normally, b) Alternate braking system is checked operative before the first flight of each day, and c) It is checked prior to each departure that the following CFDS failure message related to BRAKES N/WS MINOR FAULT is not displayed: - A fault on an Alternate Pressure Transducer or - A Fault on a Normal Pressure Transducer.

OPERATIONS (O) 32-60-04 – All Provisos DURING COCKPIT PREPARATION The ACCU PRESS indication must be in the green band. - If ACCU PRESS indication not in the green band: Y ELEC PUMP pb-sw............................................................................................….……ON then OFF ‐ CHOCKS.........................................................................................................................CHECK IN PLACE ‐ PARKING BRAKE handle...............................................................................................OFF ‐ PARKING PEDALS.........................................................................................................PRESS Apply maximum pressure on both pedals. ‐ BRAKE PRESSURE (on BRAKES pressure indicators)..................................................CHECK Pressure must increase without delay symmetrically on left and right sides for the same application simultaneously applied on left and right pedals. With full pedal deflection, the pressure must be between 900 and 1100 psi. ‐ BRAKES PEDALS........................................................................................................... RELEASE Check that no residual pressure in the brakes remains. ‐ PARKING BRAKE handle.................................................................................................ON MAINTENANCE (M) 32-60-04 First Proviso (Applicable to A318/A319/A320 aircraft) Verify that BSCU Systems 1 and 2 operate normally (Ref to AMM Task 32-46-00-740-001) MAINTENANCE (M) 32-60-04 Second Proviso (Applicable to A318/A319/A320 aircraft) To Check of the BSCU after BRAKES N/WS MINOR FAULT Caution message shown on the Upper Ecam Display Unit refer to Aircraft Maintenance Manual (AMM) 32-46-00-040-001. Revision: 36 June 30, 2017

N Registration

Page: 32.66


SUBJECT

32-60-07 Integral Tire Pressure Indicators


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable to Avianca

N Registration

Page: 32.67


SUBJECT

CAT

No INS

MIN REQ




N Registration

Page: 32.68

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 33 LIGHTS ITEM

SUBJECT

CAT

No INS

MIN REQ

C

3

0


33-10-01 Cockpit and Instrument Panel Lighting System 1) Aircraft with Mod. 27620/MP P5638 (ISIS).

Applicable to A318, A319, A320 and A321 aircraft. Individual lights may be inoperative provided: a) Remaining lights are sufficient to clearly illuminate all required instruments, controls, and other devices for which they are provided, b) Remaining lights are positioned so that direct rays are shielded from flight crewmembers eyes, c) Lighting configuration and intensity is acceptable to the flight crew, and d) RH dome light is operative. NOTE 1: RH dome light is considered operative with a minimum of three bulbs illuminated in each assembly. The bulbs can be checked by selecting the DOME toggle switch from DIM to BRT and ensure both functions operate. NOTE 2: Individual button/switch lights and/or annunciations and indications are excluded from this relief. NOTE 3: Unaided operation (without NVGs) may be permitted with inoperative NVG supplemental lights; cracked or missing filters

2) Aircraft with Mod. 27140/MP P4801 (EEPGS) or with Mod. 37329/MP P10166 or with Mod. 37330/MP P10167 and without Mod 27620/MP P5638 (ISIS).

Not applicable to Avianca fleet

(Continued)


N Registration

Page: 33.1


SUBJECT

CAT

No INS

MIN REQ


33-10-01 Cockpit and Instrument Panel Lighting System (Continued)

3) Aircraft without Mod. 27140/MP P4801 (EEPGS) or without Mod. 27620/MP P5638 (ISIS) or without Mod. 37329/MP P10166 or without Mod. 37330/MP P10167).


Not Applicable to Avianca Fleet. Avianca Fleet has Mod. 27140,

N Registration

Page: 33.2


CAT

No INS

MIN REQ

1) Test Function

B

1

0

2) Dim Function

C

1

0

May be inoperative for day operations.

3) Bright Function

C

1

0

May be inoperative: a) For night operations, and b) Day operations are not conducted.

SUBJECT


33-10-02 Annunciator Lights

PLACARD 33-10-02 Install INOP placard adjacent to Annunciator light switch on OVHD INT LT panel


N Registration

Page: 33.3


CAT

No INS

MIN REQ

1) Passenger Configurations Without Photo- Luminescent Escape Path Marking System

C

1

0

2) Passenger Configurations With Photo- luminescent Escape Path Marking Systems

C

SUBJECT


33-20-01 Cabin Light System Applicable to A318 without Photo- Luminescent Escape Path Marking System (O) Individual lights may be inoperative provided remaining lighting is sufficient for cabin attendants to perform their duties. No more than three non-adjacent cabin lights may be are inoperative 1

0

Applicable to A319, A320 and A321 and A318 with Photo-luminescent Escape Path Marking Systems (O) Individual lights may be inoperative provided: a) Remaining lighting is sufficient for cabin attendants to perform their duties, b) No more than three non-adjacent cabin lights may be are inoperative, c) All floor aisle marker light with arrows must be operative, d) The most forward and farthest aft (floor or sent) marker lights must be operative, e) Every other floor aisle marker light must be operative (no two adjacent marker light may be inoperative), and f) Sidewalk exit indicator must have two of the five lamps operating.

OPERATIONS (O) 33-20-01 1) or 2) For night flights, flight attendants must ensure that illumination is enough to perform their duties safely.


N Registration

Page: 33.4


SUBJECT

33-20-02 Passenger Lighted Information Signs

1) All Cargo, Supernumerary/Courier Area Lighted Information Signs

CAT

No INS

MIN REQ


C C C C

65 52 42 39

59 46 36 33

For A321 Fleet For A320 Fleet For A319 Fleet For A318 Fleet (M) May be inoperative provided: a) Associated passenger seat or lavatory is not occupied from which a passenger lighted information sign is not readily legible, and b) Associated seat or lavatory must be blocked and placarded - DO NOT OCCUPY NOTE: These provisos are not intended to prohibit lavatory use or inspections by crewmembers.

C C C C

65 52 42 39

59 46 36 33

For A321 Fleet For A320 Fleet For A319 Fleet For A318 Fleet (O) May be inoperative and associated passenger seat or lavatory may be occupied provided: a) PA system operates normally, and b) PA system is used to notify passengers and cabin crew when associated sign(s) are placed on or off.

0

0


OPERATIONS (O) 33-20-02 Notify cabin crew of the restricted seating: 1- Confirm the PA system operates normally. 2- Notify cabin crew to use PA system to alert passengers when seat belts should be fastened and when passengers should return to cabin from lavatories and portable electronic devices must be turned off. MAINTENANCE (M)33-20-02 1 2 3

Do the operational test of the Cabin Signs (Ref. TASK AMM 23-73-00-710-017) and find the defective NS/FSB/RTS sign(s). Find the passenger seats from which you cannot see the serviceable NS/FSB/RTS sign. Put warning notices in position on these seats to tell the passengers not to use them. Note: It must be possible to see a serviceable NS/FSB/RTS sign from every passenger seat that is in use.


N Registration

Page: 33.5


SUBJECT

33-20-04 Passenger Lighted Information Signs AUTO Function

CAT

No INS

MIN REQ


C

1

0

(O) May be inoperative provided Manual function operates normally.

OPERATIONS (O) 33-20-04) AUTO Function: Prior to each departure: 1. Place “NO PORTABLE ELECTRICAL DEVICES” sign switch to ON and verify the “NO PORTABLE ELECTRICAL DEVICES” lights in the passenger cabin illuminate. 2. Cycle the FASTEN SEAT BELT sign switch to OFF then ON and verify “FASTEN SEAT BELT” signs illuminate and chime sounds in passenger cabin.


N Registration

Page: 33.6

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 33 LIGHTS SUBJECT

CAT

No INS

33-30-01 Cargo and Service Compartment Lighting System

D

1

ITEM


MIN REQ

0

N Registration


Page: 33.7


SUBJECT

CAT

No INS

MIN REQ


33-40-01 Navigation Lights Systems 1) Aircraft Equipped With One Navigation Lights System 2) Aircraft Equipped With Two Navigation Lights Systems 3) Navigation Light System


Not applicable to Avianca. Avianca fleet has installed two Navigation lights System. C

2

1

NAV 1 or NAV 2 system may be inoperative.

C

2

0

May be inoperative for day operations. Not Applicable to Avianca

N Registration

Page: 33.8


SUBJECT

CAT

No INS

MIN REQ


C

2

1

One may be inoperative provided taxi and takeoff lights operate normally.

C

2

0


C

2

0

(O) May be inoperative in the extended position provided a 1% fuel penalty is applied for each extended light.

C

2

0

May be inoperative in the retracted position provided that the associated light is considered inoperative.

33-40-02 Landing Lighting System 1) Landing Lights

2) Extension / Retraction Systems

PLACARD 33-40-02 Install INOP placard adjacent to appropriate LAND LT switch on overhead EXT LT panel OPERATIONS (O) 33-40-02 The fuel consumption is increased by 1 % per landing light extended


N Registration

Page: 33.9


CAT

No INS

33-40-03 Runway Turn-Off Light Systems

C

2

ITEM

MIN REQ

0


PLACARD 33-40-03 Install INOP placard adjacent to appropriate Turn off switch on overhead EXT LT panel


N Registration

Page: 33.10


CAT

No INS

33-40-04 Taxi and Takeoff Light Systems

C

2

ITEM

MIN REQ

0


PLACARD 33-40-04 Install INOP placard adjacent to applicable switch on overhead EXT LT pane


N Registration

Page: 33.11


SUBJECT

33-40-05 Logo Lights

CAT

No INS

MIN REQ

D

2

0


PLACARD 33-40-05 Install INOP placard adjacent to appropriate Logo light switch on overhead EXT LT panel


N Registration

Page: 33.12


SUBJECT

33-40-06 Anti-Collision Light System

CAT

No INS

MIN REQ

C

2

0


C

2

0

May be inoperative for night operation provided wing/tail strobe lights operate normally.


PLACARD 33-40-06 Install INOP placard adjacent to Anti-Collision light switch on overhead EXT LT panel


N Registration

Page: 33.13


SUBJECT

33-40-07 Wing Scan Lights

CAT

No INS

MIN REQ

C

2

0

REMARKS OR EXCEPTIONS (O) May be inoperative provided ground deicing procedures do not require their use.

PLACARD 33-40-07 Install INOP placard adjacent to Wing Scan Light switch on overhead EXT LT panel OPERATIONS (O) 33-40-07 On ground wings must be inspected by maintenance and the Flight Crew, with appropriate flash light or better device.


N Registration

Page: 33.14


CAT

No INS

33-40-08 Wing/Tail Strobe Light System

D

1

ITEM

MIN REQ

0


PLACARD 33-40-08 Install INOP placard adjacent to Wing/Tail Strobe light switch on overhead EXT LT panel


N Registration

Page: 33.15


CAT

No INS

MIN REQ

C

14

0

(O) May be inoperative or missing provided: a) No passengers are carried, b) A maximum of 19 persons authorized in accordance with Equipment relief without passengers definition (refer to definitions section of this MEL) for non-passenger carrying operations are carried, and c) Alternate procedures are established and used.

1)Wall Mounted Exit (Marking) Signs

C

14

14

Up to three non-adjacent Bulbs or LEDs may be inoperative in individual signs.

2)Main Aisle Overhead Exit (Location) Sign

C C C

8 4 2

8 4 2

For A321 Fleet For A319 and A320 Fleet For A318 Up to three non-adjacent LEDs may be inoperative in individual signs.

SUBJECT

33-50-01 Exit Signs


NOTE: For main aisle overhead Exit (Location) Signs with Bulbs, all Bulbs must be operative. OPERATIONS (O) 33-50-01 1. No passengers may be carried. 2. A maximum of 19 persons authorized in accordance with Equipment relief without passengers definition (refer to definitions section of this MEL) may be carried. 3. Captain will brief the first attendant as follow: Before takeoff, the first attendant shall ensure direct voice communication with the persons on board to provide a safety briefing about: a) No smoking during entire flight. b) The use of seat belts c) The location and operation of emergency exits, and d) For extended overwater operations, the location and operation of life preservers including a demonstration of the method of donning and inflating a life preserver.


N Registration

Page: 33.16


SUBJECT

CAT

No INS

MIN REQ

C

11

9


33-50-02 Overhead Emergency Lights 1) A318/A319

A maximum of two non-adjacent overhead emergency lights may be inoperative.

2) A320 a) Without Mod. 24399/MP K3756 b) With Mod. 24399/MP K3756 3) A321


Not applicable to Avianca Avianca fleet has included Mod. 24399 C

12

9

A maximum of three non-adjacent overhead emergency lights may be inoperative.

C

19

15

A maximum of three non-adjacent overhead emergency lights may be inoperative.

N Registration

Page: 33.17

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 33 LIGHTS CAT

No INS

MIN REQ

33-50-03 Floor Proximity Emergency Escape Path Marking System

C

1

0

a) Aircraft equipped with Individual Incandescent Bulbs or LED’s, Components

C

1

1

Individual light may be inoperative or missing provided no two adjacent individual lights and not directly opposite each other.

b) Aircraft equipped with Photoluminescent Components

C

1

1

Each of the photoluminescent strips of an aisle may be inoperative or missing up to a length of 0,25 meter (10 inches) provided the inoperative or missing parts are not directly opposite each other and are not closer than 2,0 meter (78.74 inches), and no more than four such inoperative or missing parts are allowed.

ITEM

SUBJECT

REMARKS OR EXCEPTIONS (O) May be inoperative or missing provided: a) No passengers are carried, b) A maximum of 19 persons authorized in accordance with Equipment relief without passengers definition (refer to definitions section of this MEL) for non-passenger carrying operations are carried, and c) Alternate procedures are established and used.

OPERATIONAL (O) 1. No passengers may be carried. 2. A maximum of 19 persons authorized in accordance with Equipment relief without passengers definition (refer to definitions section of this MEL) may be carried. 3. Captain will brief the first attendant as follow: Before takeoff, the first attendant shall ensure direct voice communication with the persons on board to provide a safety briefing about: a) No smoking during entire flight. b) The use of seat belts c) The location and operation of emergency exits, and d) For extended overwater operations, the location and operation of life preservers including a demonstration of the method of donning and inflating a life preserver.


N Registration

Page: 33.18


CAT

No INS

MIN REQ

1) Overwing Emergency Light

C

4

0

2) Overwing Exit handle light

B

2

0

SUBJECT


33-50-04 Overwing Escape Route Lighting (A318/A319/A320)



N Registration

Page: 33.19


CAT

No INS

33-50-05 Escape Slide Lighting

B B

8 6

ITEM

MIN REQ

0 0

REMARKS OR EXCEPTIONS For A321 Fleet For A318, A319 and A320 Fleet May be inoperative for day operations.


N Registration

Page: 33.20


SUBJECT

33-50-06 Lavatory Auxiliary Lights


CAT

No INS

MIN REQ

C

3

0

N Registration


Page: 33.21


SUBJECT

CAT

No INS

MIN REQ


33-50-07 EMER LIGHT TEST 1) SYS TEST


Moved to item 23-73-07 1).

N Registration

Page: 33.22


SUBJECT

33-50-08 EMER EXIT LT OFF Light on SIGNS Overhead Panel


CAT

No INS

MIN REQ

C

1

0

N Registration


Page: 33.23


SUBJECT

33-50-09 Interior and Exterior Emergency Lighting Systems

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS (O) May be inoperative or missing provided: a) No passengers are carried, b) A maximum of 19 persons authorized in accordance with Equipment relief without passengers definition (refer to definitions section of this MEL) for non-passenger carrying operations are carried, and c) Alternate procedures are established and used.

OPERATIONAL (O) 1. No passengers may be carried. 2. A maximum of 19 persons authorized in accordance with Equipment relief without passengers definition (refer to definitions section of this MEL) may be carried. 3. Captain will brief the first attendant as follow: Before takeoff, the first attendant shall ensure direct voice communication with the persons on board to provide a safety briefing about: a) No smoking during entire flight. b) The use of seat belts c) The location and operation of emergency exits, and d) For extended overwater operations, the location and operation of life preservers including a demonstration of the method of donning and inflating a life preserver.


N Registration

Page: 33.24


SUBJECT

33-51-12 BAT TEST p.b on the PTP


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not Applicable to Avianca Fleet. Avianca fleet has not BAT TEST p.b on the PTP installed.

N Registration

Page: 33.25


SUBJECT

33-81-01 Visual Ice Detector Lighting


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS MMEL deleted Rev 18. (See item 30-81-03).

N Registration

Page: 33.26

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 34 NAVIGATION ITEM 34-00

SUBJECT

CAT

No INS

MIN REQ


CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) Fault(s) Indicated by ADR

C

2) Fault(s) Indicated by IR

C

3) Fault(s) Indicated by RA 1(2)

C

NOTE 1: Dispatch with either of the above MAINT STS messages displayed on ECAM is permitted without CFDS interrogation. NOTE 2: The systems are designed to be fault tolerant for a period of time given on the category column in accordance with MEL preamble information. Quantities are not required for this item while the idea is to allow these fault indication.


N Registration

Page: 34.1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 34 NAVIGATION ITEM

SUBJECT

34-00-01 Autotune Systems

CAT

No INS

MIN REQ

C

2

1


PLACARD 34-00-01 Install INOP placard adjacent to applicable panel on the center pedestal


N Registration

Page: 34.2


SUBJECT

CAT

No INS

MIN REQ


34-10-01 ADIRS 1) IR 1 Not applicable to Avianca fleet Avianca fleet has installed the P/N related.

a) Aircraft without Honeywell FMS2 (P1A or Release 1A standard) or without any of the following Mod’s: • 35526/MP P9126 (FMGC Standard P1I10), or • 37311/MP P9823 (FMGC Standard P1I11), or • 37934/MP P10439 (FMGC Standard P1C12), or • 150370/MP P11613 (FMGC Standard P1C12A), or • 38779/MP P10763 (FMGC Standard H2I11), or • 38778/MP P10762 (FMGC Standard H2C12)

b) Aircraft with Honeywell FMS2 (P1A or Release 1A standard) and with any of the following Mod’s: • 35526/MP P9126 (FMGC Standard P1I10), or • 37311/MP P9823 (FMGC Standard P1I11), or • 37934/MP P10439 (FMGC Standard P1C12), or • 150370/MP P11613 (FMGC Standard P1C12A), or • 38779/MP P10763 (FMGC Standard H2I11), or • 38778/MP P10762 (FMGC Standard H2C12))

A

1

0

Applicable to A318/A319/A320/A321 aircraft (O) NAV Mode of IR 1 may be inoperative provided: a) NAV Mode of IR 2 and NAV Mode of IR 3 are operative, b) Approach minimums do not require its use, c) The FMGC 1 is considered inoperative, and d) Repairs are made within three flight legs.

NOTE1 The terrain function of TAWS is inoperative. NOTE 2: Refer to item 22-83-01 to FMCG inoperative.

(Continued)


N Registration

Page: 34.3


SUBJECT

CAT

No INS

MIN REQ


34-10-01 ADIRS (Continued) 2) IR 2 Not applicable to Avianca fleet Avianca fleet has installed the P/N related.

a) Aircraft without Honeywell FMS2 (P1A or Release 1A standard) or without any of the following Mod’s: • 35526/MP P9126 (FMGC Standard P1I10), or • 37311/MP P9823 (FMGC Standard P1I11), or • 37934/MP P10439 (FMGC Standard P1C12), or • 150370/MP P11613 (FMGC Standard P1C12A), or • 38779/MP P10763 (FMGC Standard H2I11), or • 38778/MP P10762 (FMGC Standard H2C12)

.

(Continued)


N Registration

Page: 34.4


SUBJECT

CAT

No INS

MIN REQ

A

1

0


34-10-01 ADIRS 2) IR 2 (Continued) b) Aircraft with Honeywell FMS2 (P1A or Release 1A standard) and with any of the following Mod’s:

(O) NAV Mode of IR2 may be inoperative provided: a) NAV Mode of IR 1 and NAV Mode of IR 3 are operative, b) Approach minimums do not require its use, c) The FMGC 2 is considered inoperative, and d) Repairs are made within three flight legs.

•35526/MP P9126(FMGC Standard P1I10), or • 37311/MP P9823 (FMGC Standard P1I11), or • 37934/MP P10439 (FMGC Standard P1C12), or • 150370/MP P11613 (FMGC Standard P1C12A), or • 38779/P10763 (FMGC Standard H2I11), or • 38778/MP P10762 (FMGC Standard H2C12) b) Aircraft with Honeywell FMS2 (P1A or Release 1A standard) and with any of the following Mod’s:

Applicable to A318/A319/A320/A321 aircraft.

A

1

0

Applicable to A318/A319/A320/A321 aircraft (M)(O) May be inoperative provided: a) IR 1 and 3 are operative, b) Both FCU channels operate normally, c) All ELACs, SECs, SFCCs, FACs, LGCIUs, and RAs operate normally, d) All flight control accelerometers are verified operative, e) Takeoff in CONF 1+F is prohibited, f) Approach minimums do not require its use, g) The FMGC 2 is considered inoperative, and h) Repairs are made within three flight legs.

• 35526/MP P9126(FMGC Standard P1I10), or • 37311/MP P9823 (FMGC Standard P1I11), or • 37934/MP P10439 (FMGC Standard P1C12), or • 150370/MP P11613 (FMGC Standard P1C12A), or • 38779/P10763 (FMGC Standard H2I11), or • 38778/MP P10762 (FMGC Standard H2C12) 3) IR 3

C

1

0

(O) NAV Mode of IR 3 may be inoperative provided: a) NAV Mode of IR 1 and NAV Mode of IR 2 are operative, and b) Approach minimums do not require its use.


N Registration

Page: 34.5


SUBJECT

CAT

No INS

MIN REQ

C

1

0


34-10-01 ADIRS 3) IR 3 (Continued)

Not applicable to Avianca fleet. Avianca fleet does not have installed the P/N related.

a) Aircraft with any of the following (Honeywell) ADIRU P/N’s: • HG1150AC05 (Mod 21206/MP P1488/SB A320-34-1010), or • HG1150AC06 (Mod 24349/MP P3510/SB A320/34-1084), or • HG1150AC07 (Mod 30652/MP P6739/SB A320-34-1231 4) ADR 2 or 3 (IAE Engines, CFM Engines or PW 6000 Engines)

(M)(O) May be inoperative provided: a) IR 1 and 2 are operative, b) Both FCU channels operate normally, c) All ELACs, SECs, SFCCs, FACs, LGCIUs, and RAs operate normally, d) All flight control accelerometers are verified operative, and e) Approach minimums do not require its use.

C

2

1

(M)(O) Except where enroute operations require its use, one may be inoperative provided: a) Both FCU channels operate normally, b) All ELACs, SECs,SECs,SFCCs, FACs, LGCIUs, and RAs, operative normally, c) All flight control accelerometers are verified operative, d) Takeoff in CONF 1+F is prohibited with ADR 2 inoperative, and e) Approach minimums do not require its use. NOTE: Without Mod. 30416/MP P6635 or 31528/MP P7268, ADR 2 must be operative for RVSM operations (Not applicable to Avianca fleet).

(PW 1100G Engines)

Not Applicable to Avianca fleet Avianca fleet has not PW1100G Engines NOTE 1: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL. NOTE 2: For PBN operations refer to Appendix PBN (RNAV- RNP) operations of this MEL. (Continued)


N Registration

Page: 34.6


SUBJECT

CAT

No INS

MIN REQ


34-10-01 ADIRS (Continued) PLACARD 34-10-01 Install INOP placard adjacent to overhead ADIRU panel OPERATIONS (O) 34-10-01 Subitem -1) IR 1 ATT HDG selector ………………………………………………………..CAPT 3 IR 1 mode selector ………………………………………………………...ATT The heading must be entered through the CDU keyboard for the affected IR and has to be reset frequently (refer to FCOM/PRO-ABN-34 IR ALIGNMENT IN ATT MODE). The FMGC 1 is considered inoperative refer to (O) procedure 22-83-01. NOTE: See FCOM PRO-ABN-34 page 15 and QRH pag 2.21 (IR ALIGMENT IN ATT MODE) for TCAS operation Subitem -2) IR 2 (NAV Mode of IR2 Inoperative) DURING COCKPIT PREPARATION ‐ ATT HDG SWITCHING selector.............................................................................................F/O 3 ‐ IR 2 mode selector..................................................................................................................ATT ‐ The heading must be entered through the CDU keyboard for the IR 2 and has to be frequently reset (Refer to FCOM/PRO-ABN-34 IR ALIGNMENT IN ATT MODE). The FMGC 2 is considered inoperative refer to (O) procedure 22-83-01. Subitem -2) IR 2 Second Proviso (IR 2 totally inoperative) ‐ IR 2 pb-sw..............................................................................................................................OFF The F/CTL MAINTENANCE message is displayed on the STATUS SD page. ‐ ATT HDG SWITCHING selector...........................................................................................F/O 3 ‐ AIR DATA SWITCHING selector..........................................................................................F/O 3 The FMGC 2 is considered inoperative refer to (O) procedure 22-83-01 Note: When the ADR 2 is set to OFF, and if the aircraft is in CONF 1+F, the SFCS n°2 Flap channel is unable to crosscheck the airspeed coming from the ADR 1 with the ADR 2 airspeed coming from the SFCS n°2 Slat channel. This may lead to an uncommanded flap retraction during the takeoff. As a consequence, takeoff in CONF 1+F is not permitted when the ADR 2 is set to OFF. Subitem -3) IR 3 (First Proviso - NAV Mode of IR 3 inoperative) DURING COCKPIT PREPARATION

‐ IR 3 mode selector..................................................................................................................ATT ‐ The heading must be entered through the CDU keyboard for the IR 3 and has to be frequently reset (Refer to FCOM/PRO-ABN-34 IR ALIGNMENT IN ATT MODE) (Applicable to A318 and A319-112 aircraft only). ‐ The heading must be entered through the MCDU for the IR 3 and has to be frequently reset (Refer to FCOM/PRO-ABN-34 IR ALIGNMENT IN ATT MODE) (Applicable to A319-115, A319-132 and A320 aircraft).(Continued) Revision: 29 October 23, 2014

N Registration

Page: 34.7


SUBJECT

CAT

No INS

MIN REQ


34-10-01 ADIRS (Continued) Subitem -3) IR 3 (Second Proviso - IR 3 totally inoperative) FLIGHT PREPARATION/LIMITATIONS Maximum landing capability is CAT 3 SINGLE. DURING COCKPIT PREPARATION IR 3 pb-sw................................................................................................................................... OFF The F/CTL MAINTENANCE is displayed on the STATUS SD page. Subitem -4) ADR 2 or 3 ADR 2 DURING COCKPIT PREPARATION ‐ ADR 2 pb-sw...........................................................................................................................OFF The F/CTL MAINTENANCE message is displayed on the STATUS SD page. ‐ AIR DATA SWITCHING selector..........................................................................................F/O 3 ‐ ADIRS/ADIRU/2/26VAC AND AOA (location 121VU N08 or N09) C/B................................... Pull AFTER ENGINE START ‐ Use the RCL pb-sw on the ECAM control panel, in order to recall the NAV ADR 2 FAULT alert. ‐ On the EWD, check that the ADR 2...OFF procedure is not displayed. FOR TAKEOFF Takeoff in CONF 1+F is not permitted. Note: When the ADR 2 pb-sw is set to OFF, and if the aircraft is in CONF 1+F, the SFCS n°2 Flap channel is unable to crosscheck the airspeed coming from the ADR 1 with the ADR 2 airspeed coming from the SFCS n°2 Slat channel. This may lead to an uncommanded flap retraction during the takeoff. As a consequence, takeoff in CONF 1+F is not permitted when the ADR 2 pb-sw is set to OFF. ADR 3 DURING COCKPIT PREPARATION ‐ ADR 3 pb-sw...........................................................................................................................OFF The F/CTL MAINTENANCE message is displayed on the STATUS SD page. ‐ ADIRS/ADIRU/3/26VAC AND AOA (location 121VU N07 or N08) C/B................................... Pull AFTER ENGINE START ‐ Use the RCL pb-sw on the ECAM control panel, in order to recall the NAV ADR 3 FAULT alert. ‐ On the EWD, check that the ADR 3...OFF procedure is not displayed. MAINTENANCE (M) 34-10-01 Refer to Aircraft Maintenance Manual (AMM) Task Number 34-10-00-040-002. ADIRS - Check of all Flight Control Accelerometers for Correct Operation.


N Registration

Page: 34.8


SUBJECT

CAT

No INS

MIN REQ

34-10-02 ADIRS CDU (Aircraft Pre. Mod. 36743)

REMARKS OR EXCEPTIONS Applicable to A318 aircraft only.

1.

Mode Rotary Selectors

C

3

2

ADIRS 2 or 3 selector may be inoperative provided the associated ADIRS is considered inoperative.

2.

Data Selector

C

1

0

May be inoperative provided MCDU 1 and MCDU 2 operate normally.

3.

System Selector

C

1

0

May be inoperative provided: a) MCDU 1 and MCDU 2 operate normally, and b) IRS initialization is available through FMGS.

4.

Display

C

1

0


5.

ADR Fault Lights

C

3

0

May be inoperative provided ECAM display operates normally.

6.

ADR OFF Lights

C

3

0


7.

IR FAULT Lights

C

3

0


8.

IR ALIGN Lights

C

3

0


9.

ON BAT Light

C

1

0

10. Keyboard

C

1

0


11. ADR 2 p.b Switch

C

1

0

(O) May be inoperative provided: a) Mode Rotary Selector 2 is operative, and b) ADR 1, ADR 3, IR1 and IR3 are operative.

12. ADR 3 p.b Switch

C

1

0

(O) May be inoperative provided: a) Mode Rotary Selector 3 is operative, and b) ADR 1, ADR 2, IR1 and IR2 are operative.

OPERATIONS (O) 34-10-02 11) and 12) Affected ADR can be set to OFF through the associated mode rotary selector. In this case associated IR is also set to OFF.


N Registration

Page: 34.9


SUBJECT

CAT

No INS

MIN REQ

34-10-03 ADIRS MSU (Aircraft Post Mod. 36743)

REMARKS OR EXCEPTIONS Applicable to A319, A320 and A321 aircraft.

1. Mode Rotary Selectors

C

3

2

ADIRS 2 or 3 selector may be inoperative provided the associated ADIRS is considered inoperative.

2. IR 2 p.b Switch

C

1

0

(O)May be inoperative provided: a) Mode Rotary Selector 2 is operative, and b) ADR 1, ADR 3, IR1 and IR3 are operative.

3. IR 3 p.b. Switch

C

1

0


4. IR FAULT Lights

C

3

0


5. IR OFF Lights

C

3

0


6. ADR 2 p.b. Switch

C

1

0


7. ADR 3 p.b. Switch

C

1

0


8. ADR FAULT Lights

C

3

0


9. ADR OFF Lights

C

3

0


10. ON BAT Light

C

1

0

(Continued)


N Registration

Page: 34.10

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 34 NAVIGATION ITEM 34-10-03

SUBJECT

CAT

No INS

MIN REQ


ADIRS MSU (Aircraft Post Mod. 36743) (Continued)

OPERATIONS (O) 34-10-03 2) AND 3) IR pb-sw Affected IR can be set to OFF through the associated mode rotary selector. In this case associated ADR is also set to OFF. OPERATIONS (O) 34-10-03 6) AND 7) ADR Pb-sw Affected ADR can be set to OFF through the associated mode rotary selector. In this case associated IR is also set to OFF.


N Registration

Page: 34.11


SUBJECT

34-13-02 Mach numbers on PFD

(Aircraft with Mod. 27620)

CAT

No INS

MIN REQ

C

2

1

C

2

0

(O) May be inoperative provided: a) MMO black and red strips operate normally on both PFDs, and b) Airplane remains at or below FL 250.

C

2

0

May be inoperative provided ISIS Mach Number function is operative.


PLACARD 34-13-02 Install INOP placard adjacent to applicable PFD on lower left side OPERATIONS (O) 34-13-02 Remain at or below FL 250 and adjust the flight plan and the dispatch release.


N Registration

Page: 34.12


SUBJECT

CAT

No INS

MIN REQ

C

2

0


34-13-05 Vertical Speed indications on PFD 1) Inertial Mode PLACARD 34-13-05 Install INOP placard adjacent to applicable PFD on right side


N Registration

Page: 34.13


SUBJECT

34-13-06 Other Air Data Related Indicators (Except Airspeed and Altitude)


CAT

No INS

MIN REQ


DELETED, MMEL Revision 13.

N Registration

Page: 34.14


SUBJECT

34-13-07 Ground Speed Indications on ND

CAT

No INS

MIN REQ

C

2

0


PLACARD 34-13-07 Install INOP placard adjacent to applicable ND on upper left side


N Registration

Page: 34.15


SUBJECT

34-13-08 True Airspeed Speed Indications on ND (IAE, CFM, PW6000 Engines)

CAT

No INS

MIN REQ

C

2

0




N Registration

Page: 34.16


SUBJECT

34-13-09 Wind Speed Indications on ND

CAT

No INS

MIN REQ

C

2

0




N Registration

Page: 34.17


SUBJECT

34-14-02 EIS Heading

CAT

No INS

MIN REQ

C

4

3


PLACARD 34-14-02 Install INOP placard adjacent to applicable Display Unit (DU)


N Registration

Page: 34.18


SUBJECT

34-14-03 Position


CAT

No INS

MIN REQ


DELETED, MMEL Revision 3.

N Registration

Page: 34.19


SUBJECT

34-14-04 Navigation Station Information

CAT

No INS

MIN REQ

C

2

0


NOTE : For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.

PLACARD 34-14-04 Install INOP placard adjacent to applicable Display Unit (DU)


N Registration

Page: 34.20


SUBJECT

34-14-05 Chrono

CAT

No INS

MIN REQ

C

2

0


PLACARD 34-14-05 Install INOP placard adjacent to associated Chrono switch(es) on glareshield


N Registration

Page: 34.21


SUBJECT

34-15-01 Angle of Attack Indicator


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable to Avianca Avianca fleet does not have installed this equipment.

N Registration

Page: 34.22


SUBJECT

CAT

No INS

MIN REQ


34-21-01 Standby Airspeed Indicator

1) Airspeed Bugs


Not Applicable to Avianca fleet. Avianca fleet does not have installed this component

N Registration

Page: 34.23


SUBJECT

CAT

No INS

MIN REQ


34-21-02 Standby Altimeter 1) Airspeed Bugs


Not Applicable to Avianca fleet. Avianca fleet does not have installed this component.

N Registration

Page: 34.24


SUBJECT

34-21-03 Standby Metric Altimeter


CAT

No INS

MIN REQ


N Registration

Page: 34.25


SUBJECT

34-22-01 Standby Horizon (Attitude) (Aircraft with Honeywell ADIRUs or Aircraft with Litton ADIRUs P/N 465020-0303-0316 and Mod. 30650 or 30872)


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not Applicable to Avianca fleet. Avianca fleet does not have installed this component

N Registration

Page: 34.26


SUBJECT

34-22-02 Non-Stabilized Magnetic Compass (Standby) (Aircraft equipped with Honeywell ADIRU's or aircraft equipped with Litton ADIRUs P/N 465020-0303-316 and Mod. 30650 or 30872)

CAT

No INS

MIN REQ

B

1

0

(O) May be inoperative provided: a. Three IR's operate normally,and b. ATT/HDG, EIS DMC and PFD/ND switching capabilities operate normally.

B

1

0

(O)May be inoperative provided: a. Three IR's operate normally, b. Honeywell ADIRU's (PN HG2030AD09) must have MOD 3 or 6 (numeral b) Not Applicable to Avianca see more details on the above note), and c. DDRMI operates normally.

B

1

0

(O)May be inoperative provided: a. Any combination of two IRs are operative, b. Honeywell ADIRU's (PN HG2030AD09) must have MOD 3 or 6 (numeral b) Not Applicable to Avianca see more details on the above note), and c. Airplane is operated with dual independent navigation capability and under positive radar control by ATC on enroute portion of flight.


Note: Avianca fleet has equipped with Honeywell ADIRU.

1) Lighting (Aircraft equipped with Honeywell or Litton ADIRU's)

C

1

0

PLACARD 34-22-02 Install INOP placard adjacent to Standby Magnetic Compass door OPERATIONS (O) 34-22-02 During cockpit preparation : ATT HDG sel ……………………………………………….CAPT 3 Check normal display on CAPT PFD, ND and RMI VOR (Continued) Revision: 34 May 26, 2016

N Registration

Page: 34.27


SUBJECT

CAT

No INS

MIN REQ


34-22-02 Non-Stabilized Magnetic Compass (Standby) (Aircraft equipped with Honeywell ADIRU's only) (Continued) ATT HDG sel ……………………………………………………………………..F/O 3 Check normal display on F/O PFD, ND ATT HDG sel ……………………………………………………………………NORM EIS DMC …………………………………………………………………..CAPT 3 Check normal display on CAPT PFD, ND EIS DMC ……………………………………………………………….........F/O 3 Check normal display on F/O PFD, ND EIS DMC ……………………………………………………………………NORM CAPT PFD/ND ………………………………………………………………………XFR Check that CAPT PFD and ND images are interchanged CAPT PFD/ND ………………………………………………………………………XFR F/O PFD/ND ………………………………………………………………...........XFR Check that F/O PFD and ND images are interchanged F/O PFD/ND ………………………………………………………………...........XFR


N Registration

Page: 34.28


SUBJECT

CAT

No INS

MIN REQ

34-22-03 Integrated Standby Instrument System

REMARKS OR EXCEPTIONS Applicable to aircraft A318, A319, A320 and A321.

1) Horizon (Attitude) Function

1

1

2) ILS Function

D

1

0

3) Mach Number Function

D

1

0

4) Bugs Function

D

1

0

All must be operative, in accordance with Colombian Civil Aviation Regulation (RAC 4.5.6.3)

PLACARD 34-22-03 Install INOP placard adjacent to ISIS Indicator


N Registration

Page: 34.29


SUBJECT

34-30-01 Head Up Display (HUD)


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable. Applicable to Aircraft with HUD installed.

N Registration

Page: 34.30


SUBJECT

34-36-01 ILS Navigation Systems

CAT

No INS

MIN REQ


C

2

1

FAR and RAC requirements are included herein. NOTE 1: GPWS Glideslope Deviation Light(s) will be inoperative with the loss of the ILS.1 NOTE 2: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.


N Registration

Page: 34.31

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 34 NAVIGATION CAT

No INS

MIN REQ


34-40-07 GPWS – G/S pb-sw For aircraft with Mod 21391/MP P1631 (PULL UP – GPWS), or Mod 20522/MP P0811 (PULL UP –G/S pb-sw)

C

2

1

(O) One may be inoperative provided GPWS and TAWS aural and visual warnings are checked operative.

For aircraft with Mod 21391/MP P1631 (PULL UP – GPWS), or Mod 20522/MP P0811 (PULL UP –G/S pb-sw)

A

2

0

Both may be inoperative provided: a) The GPWS and TAWS are considered inoperative, and b) Repairs are made within two flight days.

ITEM

SUBJECT

PLACARD Install 34-40-07 INOP placard adjacent to G/S pb-sw or PULL UP –G/S pb-sw affected. OPERATIONAL (O) 34-40-07 Check of the GPWS (or TAWS) aural and visual warnings: Applicable to A318: ‐ GPWS – G/S pb-sw (operative)............................................................................................Press Applicable to A319 and A320 aircraft: ‐ PULL UP – GPWS pb-sw (operative)...................................................................................Press ‐ Check that the GPWS (or the TAWS) aural and visual warnings are operative. Refer to FCOM/DSC-3470 GPWS.


N Registration

Page: 34.32

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 34 NAVIGATION SUBJECT

CAT

No INS

34-40-09 Runway End Overrun Warning / Runway End Overrun Protection (ROW/ROP) (Mod. 155269/MP P12511)

D

1

ITEM


MIN REQ

0

REMARKS OR EXCEPTIONS Applicable to N519AV, N557AV, N567AV, N599AV, N723AV, N724AV, N725AV, N726AV, N728AV, N729AV, N730AV, N740AV, N741AV, N742AV, N743AV, N744AV, N745AV, N746AV, N748AV, N750AV, N751AV, N753AV, N755AV N759AV, N761AV, N763AV, N764AV, N765AV, N789AV, N821AV, N862AV, N939AV.

N Registration

Page: 34.33


SUBJECT

34-41-01 Weather Radar Systems

CAT

No INS

MIN REQ

D

2

1

Applicable to A319, A320 and A321 aircraft.

1

1

Applicable to A318 only,


Must be operative. 1) Transceiver (Aircraft with dual transceivers)

D

2

1

Applicable to A319, A320 and A321 aircraft May be inoperative

2) Map Mode

C

2

0

3) Automatic Gain Control (CAL)

C

2

0

4) Turbulence Detection Mode

C

1

0

5) Ground Clutter Suppression

C

1

0

6) AUTO TILT Control

C

1

0

7) Predictive Windshear Detection and Avoidance System

B

2

0

Applicable to A319, A320 and A321 aircraft.

B

1

0

Applicable to A318 only (O) May be inoperative provided alternate procedures are established and used. NOTE: Operator’s alternate procedures should include reviewing windshear avoidance and windshear recovery procedures.

C

2

0

Applicable to A319, A320 and A321 aircraft

C

1

0

Applicable to A318 only (O) May be inoperative provided: a) Alternate procedures are established and used, and b) Windshear Warning and Guidance System (Reactive) operates normally.

(Continued)


N Registration

Page: 34.34


SUBJECT

CAT

No INS

MIN REQ


34-41-01 Weather Radar Systems (Continued) PLACARD Install 34-41-01 INOP placard on Captain Weather radar control panel. OPERATIONAL (O) 34-41-01 7) 1. Flight may be conducted if there are no windshear conditions for takeoff and none are forecast for landing 2. If current weather reports for route(s) to be flown indicate thunderstorms or other potentially hazardous condition may be present, verify normal operation of Weather Radar System when clear of ramp area. 3. Refer to FCOM PRO-ABN-80 Miscellaneous Abnormal & Emergency Procedures Windshear and FCOM PRO-SUP-91-20 Operations in Windshear or Downburst Conditions.


N Registration

Page: 34.35


SUBJECT

34-42-01 Radio Altimeter (RA) Systems

CAT

No INS

MIN REQ


A

2

1

(O) One may be inoperative provided: a) Approach minimums do not require its use, b) Both FCU channels operate normally, c) All ELACs, SECs, ADIRS, SFCC, LGCIU, and FACs operate normally, and d) Repairs are made within two flight days for RA 1 and within three flight days for RA 2. NOTE 1: For aircraft equipped with TCAS or T2CAS, inoperative RA 1 renders GPWS inoperative. NOTE 2: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.


If R/A1 inoperative. C/B COM NAV/RAD ALTM/1 (121VU K11) If R/A2 inoperative. C/B COM NAV/RAD ALTM/2 (121VU K12)

…………………………………………………PULL …………………………………………………PULL

Note: 1) Status message F/CTL is displayed 2) Maximum landing capability is CAT 2.


N Registration

Page: 34.36


SUBJECT

34-42-02 Automatic Call Out System


CAT

No INS

MIN REQ


C

1

0

May be inoperative provided approach minimums do not require its use. NOTE: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.

N Registration

Page: 34.37


SUBJECT

34-42-04 Altitude Alerting System


CAT

No INS

MIN REQ

1

1

REMARKS OR EXCEPTIONS All must be operative, in accordance with Colombian Civil Aviation Regulation (RAC 4.2.2.10)

N Registration

Page: 34.38


SUBJECT

34-43-01 Traffic Alert Collision Avoidance System (TCAS II) 1) Combined Traffic Alert (TA) and Resolution Advisory (RA) Dual Display System(s)

CAT

No INS

MIN REQ

B

1

0

(M) May be inoperative provided: a) System is deactivated and secured, and b) Enroute or approach procedures do not require its use.

C

2

1

May be inoperative on the non-flying pilot side provided: a) TA and RA visual display is operative on the flying pilot side, and


b) TA and RA audio function is operative on flying pilot side. 2) Resolution Advisory (RA) Display System(s)

Not applicable to Avianca. Avianca fleet has dual display system installed

3) Traffic Alert Display System(s)

Not applicable to Avianca. Avianca fleet has dual display system installed

4)Audio Functions 5) Airspace Selection Function

B

1

0

May be inoperative provided enroute or approach procedures do not require use of TCAS. Not applicable to Avianca NOTE: For aircraft equipped with Mod. 34637/MP P8454 (T2CAS), when the TCAS is deactivated, the TAWS is also inoperative (Not applicable. Applicable to Aircraft with Mod. 34637 incorporated).

MAINTENANCE (M) 34-43-01 To deactivate TCAS refer to Aircraft Maintenance Manual (AMM) Task Number 34-43-00-040-001.


N Registration

Page: 34.39


SUBJECT

34-48-01 Ground Proximity Warning System (GPWS)

CAT

No INS

MIN REQ

A

1

0

REMARKS OR EXCEPTIONS (O) May be inoperative provided: a) Alternate procedures are established and used, and b) Repairs are made within two flight days.

1) Modes 1-4

A

4

0

(O) May be inoperative provided: a) Alternate procedures are established and used, and b) Repairs are made within two flight days.

2) Test Mode

A

1

0

May be inoperative provided: a) GPWS is considered inoperative, and b) Repairs are made within two flight days.

3) Glideslope Deviation (Mode 5)

C

2

1

B

2

0

B

1

0

4) Advisory Callouts 5) Windshear Mode 6) Terrain Awareness and Warning System (TERR) a) Terrain System – Forward Looking Terrain Avoidance (FLTA) and Premature Descent Alert (PDA Functions) b) Terrain Displays (TERR ON ND) 7) Runway Awareness & Advisory System (RAAS)

(O) May be inoperative provided alternate procedures are established and used. Deleted, MMEL revision 18 (See item 22-66-03).

B

1

0

C

2

1

B

2

0

C

1

0


NOTE: For PBN operations refer to Appendix PBN (RNAV- RNP) operations of this MEL. (Continued) Revision: 29 October 23, 2014

N Registration

Page: 34.40


SUBJECT

CAT

No INS

MIN REQ


34-48-01 Ground Proximity Warning System (GPWS) (Continued) PLACARD If GPWS SYSTEM or TEST MODE IS INOPERATIVE 1. Pull and collar circuit breakers P6 GPWS 28 VDC and P7 GPWS 115 VAC on panel 121VU 2. 34-48-01 Install INOP placard adjacent to SYS push button switch on GPWS control panel If MODES 1 THRU 4 INOPERATIVE 1. 34-48-01 Install INOP placard adjacent to SYS push button switch on GPWS control panel If GLIDESLOPE DEVIATION (mode 5) INOPERATIVE 1. 34-48-01 Install INOP placard adjacent to G/S mode push button switch on GPWS control panel If TAWS IS INOPERATIVE 34-48-01 Install INOP placard adjacent to TERR push button switch on GPWS control panel OPERATIONS (O) 34-48-01 and -1) 1- During departure briefing and descent / approach briefing, emphasize the necessity of being more aware of terrain avoidance due to lack of GPWS. 2- Use all airplane systems available (e.g, autopilot, autoland, ILS) to assist in the awareness of airplane configuration, altitude, and flight path. 3- If visual contact with terrain cannot be continuously maintained, set radio altimeter (if operative) to the highest selectable altitude. When terrain closure is recognized (visually or on radio altimeter) the radio altimeter may be reset at pilot’s discretion. OPERATIONS (O) 34-48-01 -4) Advisory Callouts The pilot is responsible to make the callouts loud and clear during all flight phases in accordance with the information displayed on PFD, ND, master warning and master caution signs. OPERATIONS (O) 34-48-01 -6) Be aware of Airplane configuration (Landing Gear and Flaps) vs. Terrain Closure and be familiar with the Airway’s MEA’s and MORA’s. Make emphasis on the approach DA/MDA.


N Registration

Page: 34.41


SUBJECT

34-48-02 GPWS FAULT Light

CAT

No INS

MIN REQ


C

1

0

May be inoperative provided GPWS is verified to operate normally before each flight.

A

1

0

May be inoperative provided: a) GPWS is considered inoperative, and b) Repairs are made within two flight days.

PLACARD 34-48-02 Install INOP placard adjacent to GPWS FAULT light on overhead panel 21 VU


N Registration

Page: 34.42


SUBJECT

34-51-01 DME

CAT

No INS

MIN REQ

C

2

1

REMARKS OR EXCEPTIONS One may be inoperative NOTE: For PBN operations refer to Appendix PBN (RNAV- RNP) operations of this MEL.

PLACARD 34-51-01 Install INOP placard adjacent to DDRMI on center pedestal instrument panel


N Registration

Page: 34.43

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 34 NAVIGATION CAT

No INS

MIN REQ

34-52-01 ATC Transponders and Automatic Altitude Reporting Systems

C

2

1

1) Elementary and Enhanced Downlink Aircraft Reportable Parameters not Required by FAR

A

ITEM

SUBJECT

2) ADS-B Squitter Transmissions


REMARKS OR EXCEPTIONS One may be inoperative. Note: FAR (91.215 & 91.219) and RAC requirements are already included herein.

12

0

May be inoperative provided: a) Operations do not require its use, and b) Repairs are made prior to completion of the next heavy maintenance visit. Not applicable. Applicable to Aircraft with ADS-B Squitter Transmissions.

N Registration

Page: 34.44


SUBJECT

34-52-03 Windshear Detection and Guidance System


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Moved to 22-66-03 in MMEL Rev. 13.

N Registration

Page: 34.45


SUBJECT

34-53-01 ADF System

CAT

No INS

MIN REQ

D

2

0

Applicable to N281AV, N284AV, N345AV, N398AV, N401AV, N411AV, N416AV, N422AV, N426AV, N446AV, N448AV, N451AV, N481AV, N647AV, N664AV, N691AV, N961AV, N980AV and N992AV only.

D

1

0

Applicable to N195AV, N519AV, N557AV, N567AV, N589AV, N590EL, N591EL, N592EL, N593EL, N594EL, N595EL, N596EL, N597EL, N598EL, N599AV, N763AV, N789AV, N821AV, N862AV and N939AV only.




N Registration

Page: 34.46


SUBJECT

34-55-01 VOR Navigation

CAT

No INS

MIN REQ

C

2

1

REMARKS OR EXCEPTIONS One maybe inoperative. FAR (129.17) and RAC requirements are included herein. NOTE: For PBN operations refer to Appendix PBN (RNAV- RNP) operations of this MEL.


N Registration

Page: 34.47


SUBJECT

34-55-02 Marker Beacon

CAT

No INS

MIN REQ


D

1

0

May be inoperative provided approach minimums do not require its use. NOTE: For CAT II/III dispatch refer to Appendix CAT II/III of this MEL.


N Registration

Page: 34.48


SUBJECT

34-55-03 Long Range Navigation Systems


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable to Avianca. Avianca fleet does not have this system installed.

N Registration

Page: 34.49


SUBJECT

34-55-04 MLS


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable to Avianca. Avianca fleet does not have this system installed.

N Registration

Page: 34.50


SUBJECT

CAT

No INS

MIN REQ

34-57-01 DDRMI (Without Mod. 33503)

REMARKS OR EXCEPTIONS Except to N195AV, N454AV, N477AV, N519AV, N536AV, N538AV, N557AV, N562AV, N603AV, N632AV, N690AV, N694AV, N695AV, N696AV, N723AV, N724AV, N725AV, N726AV, N728AV, N729AV, N730AV, N740AV, N741AV, N742AV, N743AV, N744AV, N745AV, N746AV, N748AV, N750AV, N751AV, N753AV, N755AV, N789AV, N821AV, N862AV and N939AV

1) Compass Card

C

1

0

2) VOR Pointers

C

2

1

(O) May be inoperative provided VOR navigation system operates normally.

3) DME Counters

C

2

0

(O) May be inoperative provided ADF navigation system operates normally.

4) ADF Pointers

D

2

1

(O) May be inoperative provided DME navigation system operates normally.

NOTE: FAR and RAC requirements are included herein. PLACARD 34-57-01 Install INOP placard adjacent to lower ECAM display. OPERATIONS (O) 34-57-01 2) 3) 4) When the DDRMI indication (VOR, ADF and DME) is not available or the DDRMI is not installed on the aircraft (Post Mod 33503), the VOR, ADF, DME and Magnetic Heading indications are also available on the NDs and PFDs.


N Registration

Page: 34.51


SUBJECT

34-57-02 Automatic Dependent Surveillance-Broadcast (ADS-B) System


CAT

No INS

MIN REQ

0

0

REMARKS OR EXCEPTIONS Not Applicable to Avianca Fleet

N Registration

Page: 34.52


SUBJECT

34-58-01 Global Positioning System

CAT

No INS

MIN REQ

C

2

0

REMARKS OR EXCEPTIONS (O) May be inoperative provided alternate procedures are established and used. NOTE: For PBN operations refer to Appendix PBN (RNAV-RNP) operations of this MEL.

OPERATIONS (O) 34-58-01 If one GPS is operative in operations RNAV-RNP and CLASS II NAV, there is no time limitation to conduct such operations. In case of both GPS are inoperative CLASS II navigation RNP time limitations is limited to 6.2 hours since IRS ground alignment or 5.7 hours since last FM radio update. Crew awareness. Refer to FCOM/PRO/ABN-34 PG 19. Class II navigation is prohibited and aircraft must remain within operational service volume of VOR or ADF. When GPS Primary is not available and FMS navigation accuracy check prevents the crew from using the NAV in a phase of flight, the TERR pushbutton must be switched OFF (FCOM/PRO/SUP-34 PG 13)


N Registration

Page: 34.53

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 34 NAVIGATION SUBJECT

CAT

No INS

34-61-01 Navigation Databases

C

2

ITEM

MIN REQ


2

(O) May be out of currency provided: a) Current Aeronautical Charts are used to verify Navigation Fixes prior to dispatch, b) Procedures are established and used to verify status and suitability of Navigation Facilities used to define route of flight, and c) Approach Navigation Radios are manually tuned and identified. NOTE 1:

For PBN operations refer to Appendix PBN (RNAV-RNP) operations of this MEL.

NOTE 2: If FMGC is inoperative the related Navigation Database is not accessible. Refer to MEL 22-83-01. OPERATIONS (O) 34-61-01 Current Aeronautical Charts are used to verify Navigation fixes prior to dispatch, verify status and suitability of navigation facilities used to define route of flight, and approach Navigation Radios are manually tuned and identified.


N Registration

Page: 34.54

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 35 OXYGEN ITEM

SUBJECT

35-10-01 Quick Donning Cockpit Oxygen Mask and Mic


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Deleted, Rev. 4. Item now covered under 25-1106, First Observer's Sliding Seat.

N Registration

Page: 35.1


SUBJECT

35-10-02 Indications On DOOR/OXY ECAM Page


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Moved to 35-13-01, REV 20 MMEL.

N Registration

Page: 35.2

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 35 OXYGEN SUBJECT

CAT

No INS

35-10-04 Exterior Oxygen Overpressure Indicator Disc (Green Disc)

C

1

ITEM

MIN REQ

0

REMARKS OR EXCEPTIONS (O) May be damaged or missing.

PLACARD: Install placard adjacent to lower ECAM display. OPERATIONS (O) 35-10-04 During cockpit preparation before the first flight of each day verify as follows that oxygen pressure is not decreasing: check OXY pressure indication on ECAM DOOR/OXY page twice with a 15 minutes interval between each check.


N Registration

Page: 35.3


SUBJECT

35-10-05 CREW SUPPLY p.b. Switch


CAT

No INS

MIN REQ


N Registration

Page: 35.4


SUBJECT

CAT

No INS

MIN REQ


35-13-01 Indications On DOOR/OXY ECAM Page 1) OXY High Pressure Indication A318/A319/A320/A321 without Mod. 161337/MP K17059

A318/A319/A320/A321 with Mod. 161337/MP K17059

Applicable to all A318/A319/A320/A321 except N759AV, N761AV, N764AV and N765AV C

1

0

(M)(O) May be inoperative provided: a) The oxygen pressure is verified by direct reading before each departure, b) The oxygen pressure is sufficient for the intended flight, and c) The REGUL LO PR indication is operative.

C

2

0

Applicable to N759AV, N761AV, N764AV and N765AV only. (M)(O) May be inoperative provided: a) The oxygen pressure is verified by direct reading before each departure, b) The oxygen pressure is sufficient for the intended flight, and c) The REGUL 1(2) (1+2) LO PR indication is operative.

2) REGUL LO PR Indication A318/A319/A320/A321 without Mod. 161337/MP K17059

Applicable to all A318/A319/A320/A321 except N759AV, N761AV, N764AV and N765AV C

1

0

(M)(O) May be inoperative provided the oxygen pressure is verified before the first flight of each day.

3) REGUL 1(2)(1+2) LO PR Indication Applicable to N759AV, N761AV, N764AV and N765AV only.

A318/A319/A320/A321 with Mod. 161337/MP K17059 C

3

0

(M)(O) One or more may be inoperative provided the oxygen pressure is verified each departure

Continued


N Registration

Page: 35.5


SUBJECT

CAT

No INS

MIN REQ


35-13-01 Indications On DOOR/OXY ECAM Page ( continued ) PLACARD: Install INOP Placard adjacent to lower ECAM display a) OXY High Pressure Indication OPERATIONAL (O) 35-13-01 Applicable to all airplanes DURING COCKPIT PREPARATION After application of the maintenance procedure: Check that the oxygen pressure is sufficient for the intended flight. Refer to FCOM/LIM-OXY Minimum Flight Crew Oxygen Pressure.

MAINTENANCE (M) 35-13-01 01) Refer to Aircraft Maintenance Manual (AMM) TASK 35-10-00-040-001 OXY High Pressure IndicationDirect Reading. b) REGUL LO PR Indication OPERATIONAL (O) 35-13-01 01. Applicable to All airplanes except N759AV, N761AV, N764AV and N765AV, GENERAL INFORMATION On the DOOR/OXY SD page, disregard the REGUL LO PR indication and the associated OXY indication. OPERATIONAL (O) 35-13-01 01. Applicable to N759AV, N761AV, N764AV and N765AV only., GENERAL INFORMATION On the DOOR/OXY SD page, disregard the REGUL 1(2) (1+2) LO PR indication and the associated OXY indication.

MAINTENANCE (M) 35-13-01 02) Refer to Aircraft Maintenance Manual (AMM) TASK 35-10-00-040-002 Loss of REGUL LO PR Indication


N Registration

Page: 35.6


SUBJECT

CAT

No INS

MIN REQ

C

1

0


35-13-02 Crew Supply p.b. Switch OFF Light PLACARD: Install INOP placard adjacent to switch.


N Registration

Page: 35.7


SUBJECT

CAT

No INS

MIN REQ


PASSENGER OXYGEN SYSTEM 35-20-01 Automatic Control System


Moved to 35-23-02, REV 20 MMEL

N Registration

Page: 35.8


SUBJECT

35-20-02 Manual Control System


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Moved to 35-23-01, REV 20 MMEL

N Registration

Page: 35.9


SUBJECT

35-20-03 Passenger Oxygen Storage


CAT

No INS

MIN REQ


N Registration

Page: 35.10


SUBJECT

35-20-04 Lavatory Module


CAT

No INS

MIN REQ


N Registration

Page: 35.11


SUBJECT

35-20-05 PASSENGER SYS ON Light


CAT

No INS

MIN REQ


N Registration

Page: 35.12


SUBJECT

35-20-06 Portable Oxygen Units (Bottle and Mask)


CAT

No INS

MIN REQ


N Registration

Page: 35.13


SUBJECT

35-20-07 Protective Breathing Equipment (PBE)


CAT

No INS

MIN REQ


N Registration

Page: 35.14


SUBJECT

CAT

No INS

MIN REQ

B B B B

68 52 45 36

0 0 0 0

For A321 aircraft For A320 aircraft For A319 aircraft For A318 aircraft May be inoperative provided associated seats are placard "DO NOT OCCUPY".

B B B B

68 52 45 36

0 0 0 0

For A321 aircraft For A320 aircraft For A319 aircraft For A318 aircraft (O) Modules may be inoperative provided airplane remains at or below FL 250.

B B

4 3

0 0

For A319, A320 and A321 aircraft For A318 aircraft May be inoperative provided associated flight attendant seat(s) are considered inoperative

B B

4 3

0 0

For A319, A320 and A321 aircraft For A318 aircraft (O) Modules may be inoperative provided airplane remains at or below FL 250.

B

5

0

(O) May be inoperative and associated galley occupied provided airplane remains at or below FL 250.

B

5

0

May be inoperative and associated galley occupied provided a portable oxygen bottle and mask are available for the associated galley occupant.


35-21-01 Passenger Oxygen Storage 1) Passenger Oxygen Modules

2) Flight Attendant Oxygen Modules

3) Galley Modules

PLACARD: 1. Install INOP placard on affected module and adjacent to Oxygen switch on overhead panel. 2. Install “DO NOT OCCUPY” placard on affected seats. Note: Dispatch Concurrence required due passenger load and/or operating altitude may be affected. OPERATIONAL (O) 35-21-01 Passenger Oxygen Unit Before the flight, the flight crew shall brief cabin crew on the alternate emergency procedures that will be used. Affected occupants are briefed appropriately. Cabin Attendant Oxygen Unit Before the flight, the flight crew shall brief cabin crew on the alternate emergency procedures that will be used. Galley Oxygen Unit Before the flight, the flight crew shall brief cabin crew that unit is inoperative and to use the other oxygen unit. Revision: 36 June 30, 2017

N Registration

Page: 35.15


SUBJECT

35-21-02 Lavatory Oxygen Module

CAT

No INS

MIN REQ

B

3

1

REMARKS OR EXCEPTIONS Applicable to A318, A319, A320 and 321 aircraft with unregulated decentralized gaseous oxygen type II container embodied. (M) May be inoperative provided lavatory is placarded "INOPERATIVE-DO NOT OCCUPY".

PLACARD: 1. Install INOP placard on lavatory module. 2. Install “INOPERATIVE – DO NOT OCCUPY” placard on affected lavatory (ies). MAINTENANCE (M) 35-21-02 1. Refer to Maintenance Procedure of MEL item 38-30-01 for Inoperative Lavatories


N Registration

Page: 35.16


SUBJECT

35-23-01 Passenger Oxygen Manual Control System

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS (O) May be inoperative provided airplane remains at or below FL 250.

PLACARD: Install – INOP placard adjacent to guarded oxygen switch on overhead panel. Note: Dispatch Concurrence required due operating altitude may be affected. OPERATIONS (O) 35-23-01 Notify dispatch. Operate aircraft at FL 250 or below. Passenger oxygen system automatic control must operate normally.


N Registration

Page: 35.17


SUBJECT

35-23-02 Passenger Oxygen AUTO Control System

CAT

No INS

MIN REQ

C

1

0

(M)(O) May be inoperative provided: a) Airplane remains at or below FL300,and b) Passenger oxygen manual control system to operate normally.

C

1

0

(O)May be inoperative provided airplane remains at or below FL 250.


PLACARD Install – INOP placard adjacent to passenger oxygen switch on overhead panel. Note: Dispatch Concurrence required due operating altitude may be affected. MAINTENANCE (M) 35-23-05 To Check of the MAN MASK pushbutton when the HI ALT system does not operate refer to Aircraft Maintenance Manual (AMM) 35-23-00-040-001. OPERATIONS (O) 35-23-02 Notify dispatch. Operate aircraft at FL 300 or below. Be prepared to deploy passenger masks manually (Using MASK MANUAL ON switch).


N Registration

Page: 35.18


SUBJECT

35-23-03 PASSENGER SYS ON Light

CAT

No INS

MIN REQ

C

1

0


PLACARD Install INOP placard adjacent to passenger SYS ON light on overhead panel


N Registration

Page: 35.19


SUBJECT

35-23-04 HI ALT LANDING pb-sw ON light

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS Applicable to A319, A320 and A321 aircraft.

PLACARD Install 35-23-04 INOP placard adjacent to HI ALT LANDING pb-sw.


N Registration

Page: 35.20


SUBJECT

35-23-05 HI ALT LANDING pb-sw

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS Applicable to A319, A320 and A321 aircraft. (M)(O) May be inoperative provided that the passenger oxygen AUTO control is verified operative.

C

1

0

May be inoperative provided that the passenger oxygen AUTO control is considered inoperative

PLACARD Install 35-23-05 INOP placard on HI ALT LANDING pb-sw. OPERATIONAL (O) 35-23-05 ON GROUND Inform the cabin crew that if the cabin altitude exceeds 12 500 ft, the oxygen masks may drop down. MAINTENANCE (M) 35-23-05 To Check of the MAN MASK pushbutton when the HI ALT system does not operate refer to Aircraft Maintenance Manual (AMM) 35-23-00-040-001.


N Registration

Page: 35.21

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 35 OXYGEN SUBJECT

CAT

No INS

35-31-01 Portable Oxygen Units (Bottle and Mask)

D

4

3

For A318 and A319-112 Only

D

5

3

Applicable to A319-132 and N723AV, N726AV N741AV, N751AV and N753AV.

D

5

4

Applicable to N195AV, N454AV, N477AV, N536AV, N538AV, N562AV, N603AV, N632AV, N724AV, N728AV, N740AV, N742AV, N743AV, N745AV, N748AV, N750AV, N755AV, N764AV and N765AV

D

6

3

Applicable to A319-115 except to N723AV, N726AV and N741AV, N751AV and N753AV.

D

6

4

Applicable to A321 and A320-214 except to N195AV, N454AV, N477AV, N536AV, N538AV, N562AV, N632AV, N724AV, N728AV, N740AV, N742AV, N743AV, N745AV, N748AV, N750AV and N755AV.

ITEM

MIN REQ


(M) Any in excess of those required by FAR and RAC may be unserviceable or missing provided: a) Required distribution of serviceable bottles is maintained throughout the aircraft, and b) Bottles not properly serviced are replaced, serviced, or removed at the next available maintenance facility. Note: FAR and RAC requirements are already included herein. PLACARD: Install placard adjacent to applicable Oxygen Bottle mounting bracket and at forward Attendant’s Panel. MAINTENANCE (M) 35-31-01 1. Evenly distribute the remaining oxygen bottles as applicable. 2. Replace or service used Oxygen bottles as applicable at next available maintenance facility.


N Registration

Page: 35.22


SUBJECT

35-32-01 Protective Breathing Equipment (PBE)

CAT

No INS

MIN REQ

C

5

4

Applicable to A318 and A319-112 aircraft only.

C

6

4

Applicable to A319-115, A319-132 and N195AV, N454AV, N477AV, N536AV, N538AV, N562AV, N603AV, N632AV, N724AV, N728AV, N740AV, N742AV, N743AV, N745AV, N748AV, N750AV and N755AV.

C

7

5

Applicable to A321 and A320 aircraft except to N195AV, N454AV, N477AV, N536AV, N538AV, N562AV, N603AV, N632AV, N724AV, N728AV, N740AV, N742AV, N743AV, N745AV, N748AV, N750AV , N755AV, N759AV and N761AV.

C

8

6

Applicable to N759AV and N761AV


May be inoperative or removed provided location placarding is removed or obscured NOTE 1: The cockpit PBE must be operative at all times. PLACARD: Install INOP placard adjacent to affected PBE and install INOP placard on location placarding (see Figure 1) of related PBE affected. Figure 1 Example of PBE location placarding


N Registration

Page: 35.23


SUBJECT

CAT

No INS

MIN REQ




N Registration

Page: 35.24

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 36 PNEUMATIC ITEM 36-00

SUBJECT

CAT

No INS

MIN REQ


CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) Fault(s) indicated by AIR BLEED a) A318/A319ceo/ A320ceo/A321ceo aircraft with Mod. 36595/MP P9594

Applicable to A319, A320 and A321 aircraft except to N647AV, N691AV, N664AV. C

(M) May be displayed provided it is verified that the CFDS does not report a fault on APU Leak detection loop.

C

May be displayed provided APU Leak detection loop is considered inoperative. NOTE: Dispatch with this maintenance status message displayed on ECAM is permitted without CFDS interrogation.

b) A318/A319ceo/ A320ceo/A321 ceo without Mod. 36595/MP P9594

Applicable to A318and N647AV, N691AV, N664AV. C

(M) May be displayed provided it is verified that the CFDS does not report a fault on APU Leak detection loop.

C

(M) May be displayed provided: a) Verify CFDS does not report faults on BMC 1, LH pylon leak detection loop or the APU Leak detection loop, b) If CFDS reports a fault on BMC 2, BMC 2 is considered inoperative, and c) If CFDS reports a fault on RH pylon leak detection loop, RH pylon leak detection loop is considered inoperative.

C


(M) May be displayed provided: a) Verify CFDS does not report faults on BMC 2 or RH pylon leak detection loop, b) If CFDS reports a fault on BMC 1, BMC 1 is considered inoperative, c) If CFDS reports a fault on LH pylon leak detection loop, LH pylon leak detection loop is considered inoperative, and d) If CFDS reports a fault on APU leak detection loop, APU leak detection loop is considered inoperative. (Continued)

N Registration

Page: 36.1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 36 PNEUMATIC ITEM

SUBJECT

CAT

No INS

MIN REQ


(Continued) 36-00

Fault(s) indicated by AIR BLEED (Continued) c) A319neo/A320neo C /A321neo NOTE: Dispatch with this maintenance status message dis-played on ECAM is permitted without CFDS interrogation.

MAINTENANCE (M) 36-00 a) Refer to AMM TASK 36-11-00-040-004 Check of the CFDS to Make Sure that the Pylon Leak Detection Operates Correctly MAINTENANCE (M) 36-00 b) Refer to AMM TASK 36-11-00-040-807 check of the Only RH side affected. Refer to AMM TASK 36-11-00-040-808 check of the Only LH side and/or APU leak detection loop affected


N Registration

Page: 36.2


SUBJECT

CAT

No INS

MIN REQ


36-11-01 Bleed Air Supply Systems . 1) A318/A319ceo/A320ceo /A321ceo Aircraft Without Mod. 31283/ MP P7125 or A319neo/A320neo /A321neo

C

2) A318/ A320ceo/ A321ceo with Mod. 31283/ MP P7125 or A320neo/A321neo

C

3) A319ceo with Mod. 31283 /MP P7125 or A319neo

C

2

1

Applicable to N759AV, N761AV, N764AV and N765AV only. (O) Except for ER operations beyond 120 minutes, one may be inoperative provided: a) The associated ENG BLEED p.b sw is selected OFF, b) The aircraft is not operated in known or forecast icing conditions, c) Airplane remains at or below FL 310,and d) The X-BLEED valve selector switch is selected OPEN.

2

1

Applicable to all A318, A320ceo, A321ceo, A320neo and A321neo (O) Except for ER operations beyond 120 minutes, one may be inoperative provided: a) The associated ENG BLEED p.b. sw is selected OFF, b) The aircraft is not operated in known or forecast icing conditions, c) The speed brakes are operative, and d) The X-BLEED valve selector switch is selected OPEN.

2

1

(O) Except for ER operations beyond 120 minutes, one may be inoperative provided: a) The associated ENG BLEED p.b. sw is selected OFF, b) The aircraft is not operated in known or forecast icing conditions, c) Airplane remains at or below FL 370, d) The speedbrakes are operative, and e) The X-BLEED valve selector switch is selected OPEN.

( Continued )


N Registration

Page: 36.3


SUBJECT

CAT

No INS

MIN REQ

C

2

1


36-11-01 Bleed Air Supply System ( Continued) 4) A318 with Mod. 31283/ MP P7125

(O) Except for ER operations beyond 120 minutes, one may be inoperative provided: a) The associated ENG BLEED p.b sw. is selected OFF, b) The aircraft is not operated in known or forecast icing conditions, c) Airplane remains at or below FL 350, d) The speedbrakes are operative, and e) The X-BLEED valve selector switch is selected OPEN.

PLACARD Install placard 36-11-01, INOP adjacent to affected bleed switch. OPERATIONS ( O ) 36-11-01 for 1) and 2) Applicable to N759AV, N761AV, N764AV and N765AV only FLIGHT PREPARATION/LIMITATIONS The flight crew should take into account the severity of forecast icing conditions. The wing anti-ice will be lost if the remaining engine bleed air supply system becomes inoperative. If the cargo heating is switched off: For live animal transportation, use the Live Animal Transportation Calculation Tool. If forecast icing conditions during cruise, use of wing anti-ice may request to switch off the FWD cargo ventilation. For live animal transportation, use the Live Animal Transportation Calculation Tool. AFTER ENGINE START ENG BLEED (AFFECTED) pb-sw...............................................................................................OFF AFT CARGO HOT AIR pb-sw................................................................................................. OFF If both PACKs are operative: PACK (AFFECTED) pb-sw........................................................................................................ OFF X BLEED rotary selector.......................................................................................................... OPEN AFTER TAKEOFF If the APU has been used to supply the air conditioning during the takeoff: APU BLEED pb-sw.......................................................................................................................OFF IN FLIGHT In the case of failure of the remaining engine bleed air supply system, or in the case of failure of the associated engine: Apply the AIR ENG 1+2 BLEED FAULT ECAM procedure. ( Continued )


N Registration

Page: 36.4


SUBJECT

CAT

No INS

MIN REQ


36-11-01 Bleed Air Supply System ( Continued) CAUTION

Reset ENG BLEED pb-sw as requested by ECAM procedure even if the ENG BLEED pb-sw is placarded inoperative as per MMEL 36-11-01.

In the case of failure of the opposite PACK: PACK (AFFECTED) pb-sw..................................................................................................... ON

OPERATIONS (O) 36-11-01 for 2) and 3) except for A318, A321, A320neo and A321neo FLIGHT PREPARATION/LIMITATIONS The flight crew should take into account the severity of forecast icing conditions. The wing anti-ice will be lost if the remaining engine bleed air supply system becomes inoperative. AFTER ENGINE START ENG BLEED (AFFECTED) pb-sw.......................................................................................... OFF X BLEED rotary selector......................................................................................................OPEN  If both PACKs are operative:  If Wing Anti-Ice is not required: PACK FLOW selector....................................................................................................... LO The PACK FLOW selector must be set to LO due to precooler performance.  If Wing Anti-Ice is required: PACK (AFFECTED) pb-sw.............................................................................................OFF  If one PACK is inoperative: PACK FLOW selector...............................................................................................................HI FOR TAKEOFF Set at least one air conditioning pack to off, or use the APU bleed air supply system. AFTER TAKEOFF  If the APU has been used to supply the air conditioning during the takeoff: APU BLEED pb-sw..................................................................................................................Off IN FLIGHT  If Wing Anti-Ice is required and both PACKs are operative: PACK (affected side) pb-sw..................................................................................................OFF  In the case of failure of the remaining engine bleed air supply system, or in the case of failure of the associated engine: ‐ Apply the associated ECAM procedure, then ‐ Refer to QRH/ABN-11 AIR ENG 1+2 BLEED FAULT. ( Continued )


N Registration

Page: 36.5


SUBJECT

CAT

No INS

MIN REQ


36-11-01 Bleed Air Supply System ( Continued) OPERATIONS (O) 36-11-01 2) for A321 except A321-253N (neo) FLIGHT PREPARATION/LIMITATIONS The flight crew should take into account the severity of forecast icing conditions. The wing anti-ice will be lost if the remaining engine bleed air supply system becomes inoperative. If the cargo heating is switched off: For live animal transportation, use the Live Animal Transportation Calculation Tool.

AFTER ENGINE START ‐ ENG BLEED (AFFECTED) pb-sw.......................................................................................... OFF ‐ X BLEED rotary selector......................................................................................................OPEN  If both PACKs are operative:  If Wing Anti-Ice is not required: ECON FLOW pb-sw.................................................................................................................ON The ECON FLOW pb-sw must be set to ON due to precooler performance. AFT CARGO HOT AIR pb-sw………………………………………………………………………OFF  If Wing Anti-Ice is required: PACK (AFFECTED) pb-sw.....................................................................................................OFF  If one PACK is inoperative: ECON FLOW pb-sw................................................................................................................ Off FOR TAKEOFF Set at least one air conditioning pack to off, or use the APU bleed air supply system. AFTER TAKEOFF  If the APU has been used to supply the air conditioning during the takeoff: APU BLEED pb-sw..................................................................................................................Off IN FLIGHT  If Wing Anti-Ice is required and both PACKs are operative: PACK (affected side) pb-sw..................................................................................................OFF In the case of failure of the remaining engine bleed air supply system, or in the case of failure of the associated engine: ‐ Apply the associated ECAM procedure, then ‐ Refer to QRH/ABN-11 AIR ENG 1+2 BLEED FAULT.

(Continued)


N Registration

Page: 36.6


SUBJECT

CAT

No INS

MIN REQ


36-11-01 Bleed Air Supply Systems Continued OPERATIONS (O) 36-11-01 4) Applicable to A318 only FLIGHT PREPARATION/LIMITATIONS The flight crew should take into account the severity of forecast icing conditions. The wing anti-ice will be lost if the remaining engine bleed air supply system becomes inoperative. AFTER ENGINE START ENG BLEED (AFFECTED) pb-sw.......................................................................................... OFF X BLEED rotary selector......................................................................................................OPEN  If both PACKs are operative and Wing Anti-Ice is required: PACK (AFFECTED) pb-sw................................................................................................... OFF  If one PACK is inoperative: HI FLOW pb-sw...................................................................................................................... ON FOR TAKEOFF Set at least one air conditioning pack to off, or use the APU bleed air supply system. AFTER TAKEOFF  If the APU has been used to supply the air conditioning during the takeoff: APU BLEED pb-sw..................................................................................................................Off IN FLIGHT  If Wing Anti-Ice is required and both PACKs are operative: PACK (affected side) pb-sw..................................................................................................OFF In the case of failure of the remaining engine bleed air supply system, or in the case of failure of the associated engine: ‐ Apply the associated ECAM procedure, then ‐ Refer to QRH/ABN-11 AIR ENG 1+2 BLEED FAULT.


N Registration

Page: 36.7


SUBJECT

36-11-02 Bleed Valves(PRV)

CAT

No INS

MIN REQ


C

2

1

(M)(O)Except for ER operations beyond 120 minutes, one may be inoperative secured closed provided associated bleed air supply system is considered inoperative.

PLACARD Install placard, INOP adjacent to affected bleed switch. OPERATIONIS ( O ) 36-11-02 Applicable to N759AV, N761AV, N764AV and N765AV only FLIGHT PREPARATION/LIMITATIONS The flight crew should take into account the severity of forecast icing conditions. The wing anti-ice will be lost if the remaining engine bleed air supply system becomes inoperative. If the cargo heating is switched off: For live animal transportation, use the Live Animal Transportation Calculation Tool. If forecast icing conditions during cruise, use of wing anti-ice may request to switch off the FWD cargo ventilation. For live animal transportation, use the Live Animal Transportation Calculation Tool. AFTER ENGINE START ENG BLEED (AFFECTED) pb-sw...............................................................................................OFF AFT CARGO HOT AIR pb-sw................................................................................................. OFF If both PACKs are operative: PACK (AFFECTED) pb-sw........................................................................................................ OFF X BLEED rotary selector.......................................................................................................... OPEN AFTER TAKEOFF If the APU has been used to supply the air conditioning during the takeoff: APU BLEED pb-sw.......................................................................................................................OFF IN FLIGHT In the case of failure of the remaining engine bleed air supply system, or in the case of failure of the associated engine: Apply the AIR ENG 1+2 BLEED FAULT ECAM procedure

CAUTION




N Registration

Page: 36.8


SUBJECT

CAT

No INS

MIN REQ


36-11-02 Bleed Valves(PRV) ( Continued ) OPERATIONS (O) 36-11-02 Applicable to A319 and A320 except A318, A320neo and A321neo. FLIGHT PREPARATION/LIMITATIONS The flight crew should take into account the severity of forecast icing conditions. The wing anti-ice will be lost if the remaining engine bleed air supply system becomes inoperative. AFTER ENGINE START ENG BLEED (AFFECTED) pb-sw.......................................................................................... OFF X BLEED rotary selector......................................................................................................OPEN  If both PACKs are operative:  If Wing Anti-Ice is not required: PACK FLOW selector....................................................................................................... LO The PACK FLOW selector must be set to LO due to precooler performance.  If Wing Anti-Ice is required: PACK (AFFECTED) pb-sw.............................................................................................OFF  If one PACK is inoperative: PACK FLOW selector...............................................................................................................HI FOR TAKEOFF Set at least one air conditioning pack to off, or use the APU bleed air supply system. AFTER TAKEOFF  If the APU has been used to supply the air conditioning during the takeoff: APU BLEED pb-sw..................................................................................................................Off IN FLIGHT  If Wing Anti-Ice is required and both PACKs are operative: PACK (affected side) pb-sw..................................................................................................OFF  In the case of failure of the remaining engine bleed air supply system, or in the case of failure of the associated engine: ‐ Apply the associated ECAM procedure, then ‐ Refer to QRH/ABN-11 AIR ENG 1+2 BLEED FAULT.

OPERATIONS (O) 36-11-02 Applicable to A321 except A321-253N (neo) FLIGHT PREPARATION/LIMITATIONS The flight crew should take into account the severity of forecast icing conditions. The wing anti-ice will be lost if the remaining engine bleed air supply system becomes inoperative. If the cargo heating is switched off: For live animal transportation, use the Live Animal Transportation Calculation Tool.

( Continued )


N Registration

Page: 36.9


SUBJECT

CAT

No INS

MIN REQ


36-11-02 Bleed Valves(PRV) ( Continued) AFTER ENGINE START ‐ ENG BLEED (AFFECTED) pb-sw.......................................................................................... OFF ‐ X BLEED rotary selector......................................................................................................OPEN  If both PACKs are operative:  If Wing Anti-Ice is not required: ECON FLOW pb-sw.................................................................................................................ON The ECON FLOW pb-sw must be set to ON due to precooler performance. AFT CARGO HOT AIR pb-sw………………………………………………………………………OFF  If Wing Anti-Ice is required: PACK (AFFECTED) pb-sw.....................................................................................................OFF  If one PACK is inoperative: ECON FLOW pb-sw................................................................................................................ Off FOR TAKEOFF Set at least one air conditioning pack to off, or use the APU bleed air supply system. AFTER TAKEOFF  If the APU has been used to supply the air conditioning during the takeoff: APU BLEED pb-sw..................................................................................................................Off IN FLIGHT  If Wing Anti-Ice is required and both PACKs are operative: PACK (affected side) pb-sw..................................................................................................OFF In the case of failure of the remaining engine bleed air supply system, or in the case of failure of the associated engine: ‐ Apply the associated ECAM procedure, then ‐ Refer to QRH/ABN-11 AIR ENG 1+2 BLEED FAULT. OPERATIONS (O) 36-11-02 Applicable to A318 only. FLIGHT PREPARATION/LIMITATIONS The flight crew should take into account the severity of forecast icing conditions. The wing anti-ice will be lost if the remaining engine bleed air supply system becomes inoperative. AFTER ENGINE START ENG BLEED (AFFECTED) pb-sw.......................................................................................... OFF X BLEED rotary selector......................................................................................................OPEN ( Continued )


N Registration

Page: 36.10


SUBJECT

CAT

No INS

MIN REQ


36-11-02 Bleed Valves(PRV) ( Continued)  

If both PACKs are operative and Wing Anti-Ice is required: PACK (AFFECTED) pb-sw........................................................................................ OFF If one PACK is inoperative: HI FLOW pb-sw.......................................................................................................... ON

FOR TAKEOFF Set at least one air conditioning pack to off, or use the APU bleed air supply system. AFTER TAKEOFF  If the APU has been used to supply the air conditioning during the takeoff: APU BLEED pb-sw..................................................................................................................Off IN FLIGHT  If Wing Anti-Ice is required and both PACKs are operative: PACK (affected side) pb-sw..................................................................................................OFF In the case of failure of the remaining engine bleed air supply system, or in the case of failure of the associated engine: ‐ Apply the associated ECAM procedure, then ‐ Refer to QRH/ABN-11 AIR ENG 1+2 BLEED FAULT.

MAINTENANCE (M) 36-11-02 Refer to Aircraft Maintenance Manual (AMM) task number 36-11-00-040-001


N Registration

Page: 36.11


SUBJECT

CAT

No INS

MIN REQ


C

2

1

(O) One may be inoperative closed provided associated bleed air supply system is considered inoperative.

C

2

0

May be inoperative in open provided ENG BLEED FAULT or ENG BLEED ABNORM PR cautions were not triggered during previous flight.

0

0

Not Applicable to Avianca Fleet

Applicable to N759AV, N761AV, N764AV and N765AV (O) One may be inoperative in open position provided associated bleed air supply system is considered inoperative.

36-11-03 Overpressure Valves 1) A318/A319ceo/A3 20ceo/A321ceo

2) A319neo/A320neo /A321neo with PW1100G engines

3) A319neo/A320neo /A321neo with CFM LEAP-1A engines

C

2

1

C

2

0

May be inoperative in open position provided ENG BLEED FAULT or ENG BLEED ABNORM PR cautions were not triggered during previous flight.

C

2

1

(M) One may be inoperative provided: a) Affected valve is deactivated in open position, and b) Associated bleed air supply system is considered inoperative.

PLACARD Install placard, INOP adjacent to applicable engine bleed switch OPERATIONS (O) 36-11-03 for 1) Applicable to A318 only FLIGHT PREPARATION/LIMITATIONS The flight crew should take into account the severity of forecast icing conditions. The wing anti-ice will be lost if the remaining engine bleed air supply system becomes inoperative. AFTER ENGINE START ENG BLEED (AFFECTED) pb-sw.......................................................................................... OFF X BLEED rotary selector......................................................................................................OPEN ( Continued )


N Registration

Page: 36.12


SUBJECT

CAT

No INS

MIN REQ


36-11-03 Overpressure Valves ( Continued )  

If both PACKs are operative and Wing Anti-Ice is required: PACK (AFFECTED) pb-sw........................................................................................ OFF If one PACK is inoperative: HI FLOW pb-sw.......................................................................................................... ON

FOR TAKEOFF Set at least one air conditioning pack to off, or use the APU bleed air supply system. AFTER TAKEOFF  If the APU has been used to supply the air conditioning during the takeoff: APU BLEED pb-sw..................................................................................................................Off IN FLIGHT  If Wing Anti-Ice is required and both PACKs are operative: PACK (affected side) pb-sw..................................................................................................OFF In the case of failure of the remaining engine bleed air supply system, or in the case of failure of the associated engine: ‐ Apply the associated ECAM procedure, then ‐ Refer to QRH/ABN-11 AIR ENG 1+2 BLEED FAULT. OPERATIONS (O) 36-11-03 for 1) Applicable to A319 and A320 except A318,A320 neo and A321neo FLIGHT PREPARATION/LIMITATIONS The flight crew should take into account the severity of forecast icing conditions. The wing anti-ice will be lost if the remaining engine bleed air supply system becomes inoperative. AFTER ENGINE START ENG BLEED (AFFECTED) pb-sw.......................................................................................... OFF X BLEED rotary selector......................................................................................................OPEN  If both PACKs are operative:  If Wing Anti-Ice is not required: PACK FLOW selector....................................................................................................... LO The PACK FLOW selector must be set to LO due to precooler performance.  If Wing Anti-Ice is required: PACK (AFFECTED) pb-sw.............................................................................................OFF  If one PACK is inoperative: PACK FLOW selector...............................................................................................................HI FOR TAKEOFF Set at least one air conditioning pack to off, or use the APU bleed air supply system. AFTER TAKEOFF  If the APU has been used to supply the air conditioning during the takeoff: APU BLEED pb-sw..................................................................................................................Off ( Continued ) Revision: 36 June 30, 2017

N Registration

Page: 36.13


SUBJECT

CAT

No INS

MIN REQ


36-11-03 Overpressure Valves ( Continued IN FLIGHT  If Wing Anti-Ice is required and both PACKs are operative: PACK (affected side) pb-sw..................................................................................................OFF  In the case of failure of the remaining engine bleed air supply system, or in the case of failure of the associated engine: ‐ Apply the associated ECAM procedure, then ‐ Refer to QRH/ABN-11 AIR ENG 1+2 BLEED FAULT. OPERATIONS (O) 36-11-02 Applicable to A321 except A321-253N (neo) FLIGHT PREPARATION/LIMITATIONS The flight crew should take into account the severity of forecast icing conditions. The wing anti-ice will be lost if the remaining engine bleed air supply system becomes inoperative. If the cargo heating is switched off: For live animal transportation, use the Live Animal Transportation Calculation Tool.

AFTER ENGINE START ‐ ENG BLEED (AFFECTED) pb-sw.......................................................................................... OFF ‐ X BLEED rotary selector......................................................................................................OPEN  If both PACKs are operative:  If Wing Anti-Ice is not required: ECON FLOW pb-sw.................................................................................................................ON The ECON FLOW pb-sw must be set to ON due to precooler performance. AFT CARGO HOT AIR pb-sw………………………………………………………………………OFF  If Wing Anti-Ice is required: PACK (AFFECTED) pb-sw.....................................................................................................OFF  If one PACK is inoperative: ECON FLOW pb-sw................................................................................................................ Off FOR TAKEOFF Set at least one air conditioning pack to off, or use the APU bleed air supply system. AFTER TAKEOFF  If the APU has been used to supply the air conditioning during the takeoff: APU BLEED pb-sw..................................................................................................................Off IN FLIGHT  If Wing Anti-Ice is required and both PACKs are operative: PACK (affected side) pb-sw..................................................................................................OFF ( Continued ) Revision: 36 June 30, 2017

N Registration

Page: 36.14


SUBJECT

CAT

No INS

MIN REQ


36-11-03 Overpressure Valves ( Continued In the case of failure of the remaining engine bleed air supply system, or in the case of failure of the associated engine: ‐ Apply the associated ECAM procedure, then ‐ Refer to QRH/ABN-11 AIR ENG 1+2 BLEED FAULT. OPERATIONIS ( O ) 36-11-02 Applicable to N759AV, N761AV, N764AV and N765AV only FLIGHT PREPARATION/LIMITATIONS The flight crew should take into account the severity of forecast icing conditions. The wing anti-ice will be lost if the remaining engine bleed air supply system becomes inoperative. If the cargo heating is switched off: For live animal transportation, use the Live Animal Transportation Calculation Tool. If forecast icing conditions during cruise, use of wing anti-ice may request to switch off the FWD cargo ventilation. For live animal transportation, use the Live Animal Transportation Calculation Tool. AFTER ENGINE START ENG BLEED (AFFECTED) pb-sw...............................................................................................OFF AFT CARGO HOT AIR pb-sw................................................................................................. OFF If both PACKs are operative: PACK (AFFECTED) pb-sw........................................................................................................ OFF X BLEED rotary selector.......................................................................................................... OPEN AFTER TAKEOFF If the APU has been used to supply the air conditioning during the takeoff: APU BLEED pb-sw.......................................................................................................................OFF IN FLIGHT In the case of failure of the remaining engine bleed air supply system, or in the case of failure of the associated engine: Apply the AIR ENG 1+2 BLEED FAULT ECAM procedure

CAUTION




N Registration

Page: 36.15

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 36 PNEUMATIC SUBJECT

CAT

No INS

36-11-04 Fan Air Valves (FAV)

C

2

ITEM

MIN REQ

1

REMARKS OR EXCEPTIONS (O) Except for ER operations beyond 120 minutes, one may be inoperative provided associated bleed air supply system is not used.

PLACARD Install placard, INOP adjacent to applicable engine bleed switch OPERATIONS (O) 36-11-04 Notify dispatch. -

Associated bleed valve is set to OFF Cross bleed valve is open Airplane is not flown in known or forecast icing conditions, and Airplane remains at or below FL 310.


N Registration

Page: 36.16


SUBJECT

36-11-05 Bleed Air Precooler Exchangers

CAT

No INS

MIN REQ

C

2

1

REMARKS OR EXCEPTIONS (O) Except for ER operations beyond 120 minutes, one may be inoperative provided associated bleed air supply system is not used.

OPERATIONS (O) 36-11-05 Notify dispatch. -

Associated bleed valve is set to OFF Cross bleed valve is open Airplane is not flown in known or forecast icing conditions, and Airplane remains at or below FL 310.


N Registration

Page: 36.17


CAT

No INS

36-11-06 Intermediate Pressure Check Valves (IP)

C

2

1

(O) One may be inoperative provided associated bleed air supply system is considered inoperative.

C

2

1

(M)(O) One may be inoperative in open position provided: a) Associated HP valve is secured closed, and b) Opposite bleed air supply system is operative.

ITEM

MIN REQ


PLACARD Install placard, INOP adjacent to Pneumatic Panel. OPERATIONS (O) 36-11-06 FLIGHT PREPARATION/LIMITATIONS The flight crew should take into account the severity of forecast icing conditions. At low power settings, the wing anti-ice will be lost if the opposite engine bleed air supply system becomes inoperative. DURING TAXI When the engines operate in idle thrust: ENG (affected side) BLEED pb-sw.........................................................................................OFF X BLEED selector................................................................................................................ OPEN 

If wing anti-ice is required: One PACK pb-sw..................................................................................................................OFF

BEFORE TAKEOFF AND UNTIL DESCENT Just before applying takeoff thrust ENG (affected side) BLEED pb-sw...........................................................................................On X BLEED selector................................................................................................................ AUTO 

If one PACK has been selected OFF during TAXI: PACK pb-sw............................................................................................................................ON

BEFORE DESCENT AND UNTIL LANDING When the engines operate in idle thrust: ENG (affected side) BLEED pb-sw.........................................................................................OFF X BLEED selector................................................................................................................ OPEN 

If wing anti-ice is required: One PACK pb-sw..................................................................................................................OFF

MAINTENANCE (M) 36-11-06 Refer to Aircraft Maintenance Manual AMM Task card number 36-11-00-040-002


N Registration

Page: 36.18


CAT

No INS

36-11-07 High Pressure Valves (HPV)

C

2

1

(O) One may be inoperative in the closed position provided associated bleed air supply system is considered inoperative.

C

2

1

(M)(O)One may be inoperative provided a) Affected HP valve is secured closed, and b) Opposite bleed air supply system is operative.

ITEM

MIN REQ


PLACARD Install placard, INOP adjacent to applicable Engine Bleed switch. OPERATIONS (O) 36-11-07 Notify dispatch. Refer to AVA A318/A319/A320 MEL Operational Procedure on item 36-11-06 MAINTENANCE (M) 36-11-07 Refer to Aircraft Maintenance Manual (AMM) task number 36-11-00-040-003


N Registration

Page: 36.19


CAT

No INS

MIN REQ

1) A318/A319ceo/ A320ceo/A321ceo aircraft fitted with Mod. 33844, or Mod. 33847, or Mod 33687 or A319neo/A320neo /A321neo

C

2

1

2) A318/A319ceo/ A320ceo/A321ceo aircraft fitted without Mod. 33844, or Mod. 33847, or Mod 33687

C

SUBJECT


36-11-08 Bleed Monitoring Computers (BMC)

3) A320ceo/A321ceo aircraft fitted with Mod. 31283/MP P7125 and without Mod. 33844, or Mod. 33847. 4) A319ceo aircraft fitted with Mod. 31283/MP P7125 and without Mod. 33844 or 33847

Applicable to A319/A320/A321, A319neo/A320neo/a321neo aircraft only, One may be inoperative provided: a) Associated Bleed air supply system is considered inoperative, and b) If BMC 1 is inoperative, APU leak detection loop is considered inoperative.

2

1

Applicable to A318 only. (O) Except for ER operations beyond 120 minutes, one may be inoperative provided: a) The associated BLEED p.b-sw is set to OFF, b) The associated PACK p.b-sw is set to OFF, c) The X-BLEED selector is set to SHUT, d) If BMC 1 is inoperative, APU bleed leak detection loop is considered inoperative, e) The aircraft is not operated in known or forecast icing conditions, and f) Airplane remains at or below FL 310.

0

0

Not Applicable to Avianca

Not Applicable to Avianca A319 Avianca fleet has incorporated Mod.33844, and 33847


N Registration

Page: 36.20


SUBJECT

CAT

No INS

MIN REQ


C

2

1

(O) Except for ER operations, one may be inoperative provided: a) The associated BLEED p.b-sw is set to OFF, b) The associated PACK p.b-sw is set to OFF, c) The X-BLEED selector is set to SHUT, d) If BMC 1 is inoperative, APU bleed leak detection loop is considered inoperative, e) The aircraft is not operated in known or forecast icing conditions, f) Airplane remains at or below FL 350, and g) The speedbrakes are operative.

36-11-08 Bleed Monitoring Computers (BMC) (Continued) 5) A318 aircraft fitted with Mod. 31283/MP P7125 and without Mod. 33844, or Mod. 33687

OPERATIONS (O) 36-11-08 2) and 5)

DURING COCKPIT PREPARATION -ENG (affected side) BLEED pb-sw.........................................................................................OFF -PACK (affected side) pb-sw....................................................................................................OFF -X BLEED selector.................................................................................................................SHUT  If the BMC 1 is affected: -APU BLEED pb-sw............................................................................................................... OFF Note: The use of the APU bleed air supply system for Main Engine Start is permitted. IN FLIGHT In the case of failure of the remaining engine bleed air supply system, or in the case of failure of the associated engine: -Apply the associated ECAM procedure, then -Refer to QRH/ABN-36 AIR ENG 1+2 BLEED FAULT.


N Registration

Page: 36.21


CAT

No INS

36-12-01 APU Bleed Air Supply System

C

1

ITEM

MIN REQ

0

REMARKS OR EXCEPTIONS (O) May be inoperative provided APU BLEED switch remains OFF. NOTE: APU can be used for electrical power.

PLACARD Install placard, INOP adjacent to APU Bleed switch. OPERATIONS (O) 36-12-01 Note 1: Notify dispatch, APU Bleed Air System operations are not operative and require an air power source for engine start. Note 2: APU may be used for electrical generation purposes 1 2

APU BLEED switch must remain “OFF” (Verify on ECAM Bleed Page) Use alternate air power source for engine start.


N Registration

Page: 36.22


SUBJECT

36-12-02 APU Bleed Valve

CAT

No INS

MIN REQ


C

1

0

(M) May be inoperative deactivated in the closed position provided APU bleed switch is selected OFF. NOTE: APU can be used for electrical power.

C

1

0

(O) May be inoperative in the open position provided APU is not used in flight.

PLACARD Install placard, INOP adjacent to APU Bleed switch. OPERATIONAL (O) 36-12-02 ON GROUND OR IN FLIGHT  When the APU runs: APU BLEED pb-sw.....................................................................................................................ON  After APU shutdown: APU BLEED pb-sw.....................................................................................................................OFF MAINTENANCE (M) 36-12-02 1. Check the APU model installed and accomplishes the follow step as applicable: - To Deactivation of the APU Bleed Load Control-Valve (GTCP 36-300) refer to AMM 49-51-00-040-001. - To Deactivation of the Bleed Control Valve (APS 3200) refer to AMM 49-51-00-040-002. - To Deactivation of the APU Load Control-Valve (131-9(A)) refer to AMM TASK 49-51-00-040-004.


N Registration

Page: 36.23


SUBJECT

36-12-03 APU Bleed Check Valve

CAT

No INS

MIN REQ

C

1

0

(O) May be inoperative closed provided APU bleed switch is selected OFF.

C

1

0

(O) May be inoperative open and APU used provided: a) Airplane remains at or below FL 200, and b) X BLEED selector is selected SHUT and ENG 1 bleed is selected OFF if engine bleed is used.

C

1

0

(O) May be inoperative open provided APU is not used.


PLACARD Install placard, INOP adjacent to APU switch. OPERATIONS (O) 36-12-03 Notify Dispatch First Proviso: If inoperative CLOSED, APU BLEED pb switch must remain “OFF” Second Proviso: If inoperative OPEN: Aircraft must remain at or below FL 200 X BLEED selector is selected SHUT and ENG 1 bleed is selected OFF Third Proviso: APU is considered inoperative and not used.


N Registration

Page: 36.24


CAT

No INS

MIN REQ


1) Automatic Control

C

1

0

(O) May be inoperative provided manual control operates normally.

2) Manual Control

C

1

0

(O) Except for ER operations beyond 120 minutes, may be inoperative provided: a) Automatic control is verified to operate normally before each flight, b) APU bleed is operative for engine start, c) Aircraft is not operated in known or forecast icing conditions, d) Both bleed air supply systems operate normally, and e) Both air conditioning packs operate normally.

SUBJECT

36-12-04 Cross Bleed Valve

PLACARD Install placard, INOP adjacent to X- Bleed Selector. OPERATIONS (O) 36-12-04 1) GENERAL INFORMATION When the APU BLEED pb-sw is ON, or for engine start: - X BLEED selector................................................................................................................ OPEN - Select SHUT in all other cases. DURING COCKPIT PREPARATION Check of the manual control of the X BLEED valve: - X BLEED selector …………………………….………………………………………………… . OPEN - On the BLEED SD page, check that the cross bleed valve is indicated open. - X BLEED selector ……………………………………………………………………………….. SHUT - On the BLEED SD page, check that the cross bleed valve is indicated closed. - X BLEED selector ………………………………………………………………………………... AUTO OPERATIONS (O) 36-12-04 2) DURING COCKPIT PREPARATION - X BLEED selector.....................................................................................................................AUTO Check of the automatic control of the X BLEED valve: Check that the APU is started. - APU BLEED pb-sw....................................................................................................................Off - On the BLEED SD page, check that the cross bleed valve is indicated closed. - APU BLEED pb-sw...................................................................................................................ON - On the BLEED SD page, check that the cross bleed valve is indicated open.


N Registration

Page: 36.25


CAT

No INS

MIN REQ

1) FAULT Lights

C

2

0

2) OFF Lights

C

2

0

SUBJECT


36-20-01 ENG BLEED p.b. Switch May be inoperative provided alternate procedures are established and used.

PLACARD Install placard, INOP adjacent to associated Fault Light.


N Registration

Page: 36.26


CAT

No INS

MIN REQ

1) FAULT Light

C

1

0

2) ON Light

C

1

0

SUBJECT


36-20-02 APU BLEED p.b. Switch

PLACARD Install placard, INOP adjacent to APU bleed Fault Light.


N Registration

Page: 36.27


CAT

No INS

MIN REQ

1) ENG BLEED Pressure

C

2

0

2) ENG BLEED Temperature

C

2

0

3) ENG BLEED Valve

C

2

0

4) ENG HP Valve

C

2

0

5) APU BLEED Valve

C

1

0

6) X BLEED Valve

C

1

0

SUBJECT


36-20-03 ECAM BLEED Page Indications

May be inoperative provided the Cross bleed valve automatic control is considered inoperative.

PLACARD Install placard, INOP adjacent to lower ECAM display.


N Registration

Page: 36.28


CAT

No INS

MIN REQ


1) A318/A319ceo/ A320ceo/A321ceo aircraft fitted with Mod. 33844/MP P8341, or Mod. 33847/MP P8340, or Mod. 33687/MP P8297.

C

2

1

Applicable to A319, A320 and A321 aircraft only.

2) A318/A319ceo/ A320ceo/A321ceo aircraft without Mod. 33844/MP P8341, or Mod. 33847/MP P8340, or Mod. 33687/MP P8297

C

SUBJECT

36-22-15 Pylon Leak Detection Loops

3) A318/A320ceo/ A321ceo aircraft fitted with Mod. 31283/MP P7125 and without Mod. 33844/MP P8341 or Mod. 33847/MP P8340.

(M) One may be inoperative provided: a) The associated pylon leak detection loop is deactivated, b) The caution AIR ENG 1(2) BLEED LEAK is confirmed to be false by troubleshooting, and c) The affected bleed air supply system is considered inoperative. 2

1

Applicable to A318 only. (M)(O) Except for ER operations beyond 120 minutes, one may be inoperative provided: a) The associated pylon leak detection loop is deactivated, b) The associated BLEED p.b-sw is set to OFF, c) The associated PACK p.b-sw is set to OFF, d) The X-BLEED selector is set to SHUT, e) The APU BLEED p.b-sw is set to OFF if LH side is affected, f) The aircraft is not operated in known or forecast icing conditions, and g) Airplane remains at or below FL 310.

0

0


(Continued)


N Registration

Page: 36.29


SUBJECT

CAT

No INS

MIN REQ


36-22-15 Pylon Leak Detection Loops (Continued) 4) A319ceo aircraft fitted with Mod. 31283/MP P7125 and without Mod. 33844/MP P8341 or Mod. 33847/MP P¨8340

Not Applicable to Avianca A319 Avianca fleet has incorporated Mod.33844, and 33847. .

5) A318 aircraft fitted with Mod. 31283/MP P7125 and 33844/MP P8341 or Mod. 33847/MP P8340, or Mod. 33687/MP P8297.

0

6) A319neo/A320neo /A321neo

0

Not Applicable to Avianca 318 Avianca fleet has not incorporated Mod.33844, 33847 and 33687

Incorporated into item 36-36-00.

PLACARD Install placard, INOP adjacent to the upper ECAM display. OPERATIONS (O) 36-22-15 (Applicable to A319 A320 and A321 aircraft only): Notify dispatch airplane remains at or below FL 310 OPERATIONS (O) 36-22-15 (Applicable to A318 aircraft only): During cockpit preparation: ENG (affected side) BLEED pb-sw ......................................................................................................... OFF PACK (affected side) pb-sw ................................................................................................................... OFF X-BLEED pb-sw ................................................................................................................................... SHUT -

If LH side is affected: APU BLEED pb-sw ............................................................................................................................... OFF Note: The use of the APU bleed air supply system for Main Engine Start is allowed. (Continued)

36-22-15

Pylon Leak Detection Loops (Continued)

In flight: Revision: 36 June 30, 2017

N Registration

Page: 36.30


SUBJECT

CAT

No INS

MIN REQ


In the case of failure of the remaining engine bleed air supply system, or in the case of failure of the associated engine: - Apply associated ECAM procedure, then - Refer to Refer to QRH/ABN-36 AIR ENG 1+2 BLEED FAULT. MAINTENANCE (M) 36-22-15 (Applicable to A318/A319/A320/A321 aircraft): Refer to AMM TASK 36-22-00-040-001 Deactivation of the Pylon Overheat Sensing-Element (1HF1, 1HF2)


N Registration

Page: 36.31


SUBJECT

36-22-16 Wing Leak Detection Loops


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Deleted, REV 20 MMEL. Incorporated into 36-00.

N Registration

Page: 36.32

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 36 PNEUMATIC CAT

No INS

MIN REQ

36-22-17 APU Leak Detection Loop

C

1

0

(M) May be inoperative provided: a) APU check valve is removed and replaced by a cover plate, and b) APU air supply system is considered inoperative.

1) A320ceo/A321ceo with Mod. 31283 / MP P7125

C

1

0

(O) Except for ER operations beyond 120 minutes, may be inoperative provided: a) AIR APU BLEED LEAK was not displayed during the previous flight, b) ENG 1 BLEED p.b-sw is set to OFF, c) PACK 1 p.b-sw is set to OFF, d) X-BLEED selector is set to SHUT, e) APU BLEED p.b-sw is set to OFF, f) Aircraft is not operated in known or forecast icing conditions, and g) Speedbrakes are operative.

2) A319ceo with Mod. 31283 / MP P7125

C

1

0

(O) Except for ER operations beyond 120 minutes, may be inoperative provided: a) AIR APU BLEED LEAK was not displayed during the previous flight, b) ENG 1 BLEED p.b-sw is set to OFF, c) PACK 1 p.b-sw is set to OFF, d) The X-BLEED selector is set to SHUT, e) The APU BLEED p.b-sw is set to OFF, f) The aircraft is not operated in known or forecast icing conditions, g) The speedbrakes are operative, and h) Airplane remains at or below FL 370.

3) A318 with Mod. 31283 / MP P7125

C

1

0

(O) Except for ER operations beyond 120 minutes, may be inoperative provided: a) The AIR APU BLEED LEAK was not displayed during the previous flight, b) The ENG 1 BLEED p.b-sw is set to OFF, c) The PACK 1 p.b-sw is set to OFF, d) The X-BLEED selector is set to SHUT, e) The APU BLEED p.b-sw is set to OFF, f) The aircraft is not operated in known or forecast icing conditions, g) The speedbrakes are operative, and h) Airplane remains at or below FL 350.

ITEM

SUBJECT


(Continued)


N Registration

Page: 36.33


SUBJECT

CAT

No INS

MIN REQ


C

1

0

(O) Except for ER operations beyond 120 minutes, may be inoperative provided: a) The AIR APU BLEED LEAK was not displayed during the previous flight, b) The ENG 1 BLEED p.b-sw is set to OFF, c) The PACK 1 p.b-sw is set to OFF, d) The X-BLEED selector is set to SHUT, e) The APU BLEED p.b-sw is set to OFF, f) The aircraft is not operated in known or forecast icing conditions, and g) Airplane remains at or below FL 310.

36-22-17 APU Leak Detection Loop (Continued) 4) A318/A319ceo/A3 20ceo/A321ceo

5) A320neo/A321neo

Applicable to N759AV, N761AV, N764AV and N765AV only. C

0

(O) Except for ER operations beyond 120 minutes, may be inoperative provided: a) AIR APU BLEED LEAK and the APU LEAK FED BY ENG subtitle were not displayed during the previous flight, b) ENG 1 BLEED p.b-sw is set to OFF, c) PACK 1 p.b-sw is set to OFF, d) X-BLEED selector is set to SHUT, e) APU BLEED p.b-sw is set to OFF, f) Aircraft is not operated in known or forecast icing conditions, and g) Speedbrakes are operative.

6) A319neo


7) A319neo/A320neo /A321neo

Applicable to N759AV, N761AV, N764AV and N765AV only C


1

0

0

(O) Except for ER operations beyond 120 minutes, may be inoperative provided: a) The AIR APU BLEED LEAK and the APU LEAK FED BY ENG were not displayed during the previous flight, b) The ENG 1 BLEED p.b-sw is set to OFF, c) The PACK 1 p.b-sw is set to OFF, d) The X-BLEED selector is set to SHUT, e) The APU BLEED p.b-sw is set to OFF, f) The aircraft is not operated in known or forecast icing conditions, and g) Airplane remains at or below FL 310.

N Registration

Page: 36.34


SUBJECT

CAT

No INS

MIN REQ


PLACARD Install placard, INOP adjacent to the upper ECAM display. OPERATIONS (O) 36-22-17: DURING COCKPIT PREPARATION - ENG (affected side) BLEED pb-sw.........................................................................................OFF - PACK (affected side) pb-sw....................................................................................................OFF - X BLEED selector.................................................................................................................SHUT - If the LH side is affected: APU BLEED pb-sw............................................................................................................... OFF Note: The use of the APU bleed air supply system for Main Engine Start is permitted. IN FLIGHT In the case of failure of the remaining engine bleed air supply system, or in the case of failure of the associated engine: - Apply the associated ECAM procedure, then - Refer to QRH/ABN-36 AIR ENG 1+2 BLEED FAULT.

OPERATIONS (O) 36-22-17 Applicable to N759AV, N761AV, N764AV and N765AV only DURING COCKPIT PREPARATION ENG 1 BLEED pb-sw.................................................................................................................. OFF PACK 1 pb-sw............................................................................................................................. OFF X BLEED selector..................................................................................................................... SHUT APU BLEED pb-sw......................................................................................................................OFF BEFORE ENGINE START X BLEED selector.....................................................................................................................OPEN APU BLEED pb-sw............................................................................................................ AS RQRD Note: The use of the APU bleed air supply system is permitted for Main Engine Start. AFTER ENGINE START X BLEED selector..................................................................................................................... SHUT APU BLEED pb-sw......................................................................................................................OFF IN FLIGHT In the case of failure of the remaining engine bleed air supply system, or in the case of failure of the associated engine: Apply the AIR ENG 1+2 BLEED FAULT ECAM procedure.

MAINTENANCE (M) 36-22-17: Refer to AMM TASK 36-22-00-040-001A for Deactivation. Refer to AMM TASK 36-22-00-440-001A for Reactivation.


N Registration

Page: 36.35


SUBJECT

CAT

No INS

MIN REQ




N Registration

Page: 36.36

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 38 WATER/WASTE ITEM

SUBJECT

38-10-01 Potable Water Systems

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS (M) Individual components may be inoperative provided: a) Associated components are deactivated or isolated, and b) Associated system components are verified not to have leaks. NOTE: Any portion of system which operates normally may be used.

C

1

0

(M) May be inoperative provided: a) System is drained, and b) Procedures are established to ensure that system is not serviced.

MAINTENANCE (M) 38-10-01 Access Zone: GSE: Fin 1MA 1MB 2MB 9MB

Access Item: Associated Circuit Breakers Designation WATER SYS LAV FWD-HOT WATER LAV AFT-HOT WATER-D LAV AFT-HOT WATER-E

Location 2001 VU 2000 VU 2001 VU 2001 VU

NOTE: Dispatch Concurrence required due to galley and/or potable water to FULL water. If water quantity is inoperative: -

Advise System Operations to have stations service potable water to FULL, as required.

If only Galley Potable Water system is affected perform the following: -

Close the applicable galley(ies) water shut-off valve(s) or cap lines as required to isolate leak(s). Leak check to verify leak(s) has (have) contained AMM 38-11-41 page 601. Ensure there are no accumulation of water or ice in affected areas (if leak has been reported).

If only Lavatory(ies) Potable water system is affected perform the following: -

Close the applicable lavatory(ies) potable water shut-off valve(s) located at the front of toilet shroud. Shut-off valve heater switch located near the top of the top of the heater, under the wash basin. Ensure there are no accumulation of water or ice in affected areas (if leak has been reported). Apply MEL item 38-30-01 Lavatory inoperative procedures. (Continued)


N Registration

Page: 38.1


SUBJECT

CAT

No INS

MIN REQ


38-10-01 Potable Water Systems (Continued) The following procedure deactivates all three lavatories and all water service on the aircraft -

Dispatch Concurrence required due passengers must be informed that there will be no lavatories or water available during flight. Drain potable system. AMM 12-24-38 page 201. Ensure there are not accumulation of water or ice in the affected area if a leak has been noticed Install “Do not fill potable water” placard near the water servicing port located in water service panel on aft LH fuselage. Open and collar circuit breakers 1MB located on panel 2000VU and circuit breakers 1MA, 2MB AND 9MB on panel 2001VU for deactivating the lavatory water heaters.. Apply MEL item 38-30-01 lavatory Inoperative procedures.


N Registration

Page: 38.2


SUBJECT

38-30-01 Lavatory Waste Systems (Including Wheelchair Accessible Lavatories)

CAT

No INS

MIN REQ

C

3

0

REMARKS OR EXCEPTIONS (M) Individual components may be inoperative provided: a) Associated components are deactivated or isolated, and b) Associated system components are verified not to have leaks. NOTE: Any portion of system which operates normally may be used.

C

3

0

(M) Associated lavatory system(s) may be inoperative provided: a) Associated components are deactivated or isolated to prevent leaks, b) The Pilot-in-Command will determine if flight duration is acceptable with a FWD lavatory unusable, and c) Associated lavatory door(s) is secured closed and placarded, "INOPERATIVE – DO NOT ENTER". NOTE: These provisions are not intended to prohibit inspections by crewmembers.

1) Vacuum Generator Systems (Toilet)

C

2

0

(M)(O)May be inoperative provided: a) Vacuum generator is deactivated, and b) Procedures are established and used to only allow use of the associated lavatory at or above 16000 FT MSL.

PLACARD Install 38-30-01 INOP-DO NOT ENTER placard on applicable lavatory door at eye level and adjacent to forward Flight. OPERATIONS (O) 38-30-01 Due to the vacuum generator having been deactivated as per maintenance procedure, the lavatory must be used at or above 16000 FT MSL, the captain must inform the first flight attendant when the airplane has reached this level and the use of the lavatory is permitted. (Continued)


N Registration

Page: 38.3


SUBJECT

CAT

No INS

MIN REQ


38-30-01 Lavatory Waste Systems (Including Wheelchair Accessible Lavatories) (Continued) MAINTENANCE (M) 38-30-01 Access Zone: GSE:

Access Item:

Fin 33 MG

Associated Circuit Breakers Designation TOILET SYSTEM/ VACUUM GEN

Location 2001 VU

35 MG

TOILET SYSTEM/ VACUUM SYS

2001 VU

Applicable to first/second provisos Deactivate a lavatory as follows: 1. Ensure the lavatory(ies) does (do) not require servicing and not leaks are present. 2. Empty lavatory waste receptacle. 3. Associated lavatory door(s) is secure closed and placarded “INOPERATIVE- DO NOT ENTER” NOTE: Dispatch Concurrence required due lavatories may be inoperative. MAINTENANCE (M) 38-30-01 -1) Vacuum Generator Systems (Toilet) Deactivate the vacuum generator as follows: 1. Open and safety the C/B 33MG located in the panel 2001 VU (Vacuum toilet system/vacuum gen). 2. Install placard “Lav INOP below 16,000 ft”.


N Registration

Page: 38.4

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 46 INFORMATION SYSTEMS ITEM

SUBJECT

CAT

No INS

MIN REQ


46-20-01 Electronic Flight Bag

Systems (EFBs)


1. Class 3 EFBs


2. Data Connectivity (Class 2)


3. Power Connection (Class 1 & 2)


4. Mounting Device (Class 2)


N Registration

Page: 46.1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 46 INFORMATION SYSTEMS SUBJECT

CAT

No INS

46-21-01 Air Traffic Service Unit System (ATSU)

C

1

0


D

1

0


ITEM

MIN REQ


NOTE 1: Any ATSU function or mode that operates normally may be used. NOTE 2: In case of total ATSU failure, the Airman system for aircraft monitoring is considered inoperative. PLACARD Install 46-21-01 INOP placard adjacent to the ECAM display. OPERATIONS (O) 46-21-01 Notify to MCC, CCD and CCV. Use available VHF voice communication system to send and/or receive data/reports. If any aircraft fault condition is presented, MCC should be notified when time permits.


N Registration

Page: 46.2


SUBJECT

46-21-02 Data-Link Control Display Units (DCDU)


CAT

No INS

MIN REQ


N Registration

Page: 46.3


SUBJECT

46-21-03 ATC Msg. p.b.


CAT

No INS

MIN REQ


N Registration

Page: 46.4

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 47 INERT GAS SYSTEM ITEM 47-00

SUBJECT

CAT

No INS

MIN REQ


CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) Faults indicated by FUEL INERT (A318/A319/A320/ A321 aircraft fitted with Mod. 38062 /MP J2879)

A

Applicable to A318, A319, A320 and 321 aircraft with FTIS embodied. May be displayed provided repairs are made within twenty flight days. NOTE: Dispatch with associated MAINT STS message displayed on ECAM is permitted without CFDS interrogation.


N Registration

Page: 47.1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 47 INERT GAS SYSTEM ITEM

SUBJECT

47-10-01 Fuel Tank Inerting System (A318/A319/A320/A321 aircraft fitted with Mod. 38062/MP J2879 and Mod 151269/MP P11819)


CAT

No INS

MIN REQ

A

1

0

REMARKS OR EXCEPTIONS Applicable to A318, A319, A320 and 321 aircraft with FTIS embodied. May be inoperative provided repairs are made within twenty flight-days.

N Registration

Page: 47.2

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 49 AIRBORNE AUXILIARY POWER ITEM 49-00

SUBJECT

CAT

No INS

MIN REQ


CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) Fault(s) indicated by APU

C NOTE 1: Dispatch with this maintenance status message displayed on ECAM is permitted without CFDS interrogation. NOTE 2: The systems are designed to be fault tolerant for a period of time given on the category column in accordance with MEL preamble information. Quantities are not required for this item while the idea is to allow these fault indication.


N Registration

Page: 49.1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 49 AIRBORNE AUXILIARY POWER ITEM

SUBJECT

49-10-01 APU System 1) A318/A319/A321 (A320 with Mod. 27189 or Mod. 33972)

CAT

No INS

MIN REQ

C

1

0

(O) Except for ER operations, may be inoperative.

A

1

0

(O) Except for ER operations beyond 120 minutes, may be inoperative for four flights.


OPERATION (O) 49-10-01 DURING PRELIMINARY COCKPIT PREPARATION Do not use the APU. APU MASTER SW pbsw..............................................................................................................Off No APU bleed air will be available for Main Engine Start (MES) or air conditioning. No electrical power will be available from the APU generator. BEFORE PUSHBACK OR ENGINE START For engine start without APU, Refer to FCOM/PRO-NOR-SUP-ENG Engine Start with External Pneumatic Power. AFTER LANDING, AT THE GATE In absence of suitable ground support equipment at destination, an engine opposite to the refueling point will need to be operated during refueling to ensure the continued availability of bleed air and electrical power for engine starting. Refer to FCOM/PRO-NOR-SUP-FUEL Refueling with One Engine Running.


N Registration

Page: 49.2


SUBJECT

49-10-02 APU Air Intake Flap

CAT

No INS

MIN REQ

A

1

0

(M) May be inoperative secured open and APU used provided repairs are made within 10 flight days.

C

1

0

May be inoperative closed or partially closed provided APU is not used.


MAINTENANCE (M) 49-10-02 Applicable only to aircraft with APU 131-9A installed: Refer to Aircraft Maintenance Manual (AMM) Task Card number 49-16-00-040-003 Applicable only to aircraft with APU APS 3200 installed: Refer to Aircraft Maintenance Manual (AMM) Task Card number 49-16-00-040-002


N Registration

Page: 49.3


SUBJECT

49-30-01 APU Fuel Pump

1) A318/A319/A321 (A320 with Mod. 27189 or Mod. 33972)

CAT

No INS

MIN REQ

C

1

0

Except for ER operations, may be inoperative provided both engine driven generators are operative.

A

1

0

(O) Except for ER operations beyond 120 minutes, may be inoperative for four flights.


NOTE: APU may be started using A.C. boost pump feeding the left fuel manifold. OPERATION (O) 49-30-01 APU may be started using A.C. boost pump feeding the left fuel manifold.


N Registration

Page: 49.4


SUBJECT

49-30-02 APU LP Valve

CAT

No INS

MIN REQ


C

1

0

(M) May be inoperative secured closed provided APU is not used.

C

1

0

(O) May be inoperative in closed position provided: a) Valve is indicated closed on ECAM, and b) APU is not used.

OPERATIONS (O) 49-30-02 Install 49-30-02 INOP placard adjacent to APU master p.b. switch on APU panel 25 VU. Engine start with external pneumatic power FCOM/PRO/SUP-70 PG 5. MAINTENANCE (M) 49-30-02 1. Low Pressure Valve secured in close Position. 2. Do the Deactivation procedure referred in AMM Task 28-29-00-040-002.


N Registration

Page: 49.5


SUBJECT

49-70-01 MASTER Switch ON Light


CAT

No INS

MIN REQ

C

1

0

N Registration


Page: 49.6


SUBJECT

49-70-02 MASTER Switch FAULT Light


CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS May be inoperative provided N and EGT indications are available on ECAM APU page.

N Registration

Page: 49.7


SUBJECT

49-70-03 START ON Light


CAT

No INS

MIN REQ

C

1

0

N Registration


Page: 49.8


SUBJECT

49-70-04 START/AVAIL Light


CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS May be inoperative provided N indication is available on ECAM APU page.

N Registration

Page: 49.9


CAT

No INS

MIN REQ

1. APU Indications

C

10

0

May be inoperative provided procedures do not require their use.

2. APU GEN Parameters

C

3

0

Except for ER operations, may be inoperative provided both Engine Driven Generators are operative.

3. ECAM APU Page LOW OIL LEVEL

B

1

0

(M) May be inoperative provided:

SUBJECT


49-70-05 ECAM APU Page Indications

a) Oil level is verified before each refueling, and b) There is no evidence of abnormal consumption or leakage. MAINTENANCE (M) 49-70-05 1. Install Placard Inop. ECAM APU Page LOW OIL LEVEL Adjacent to lower ECAM display. NO START APU 2. Energize the ground service network 3. On the panel 25VU, make sure that the APU MASTER SW pushbutton is OFF. 4. Oil Level is verified before each refueling, and there is no evidence of abnormal consumption or leakage. 5. Remove the placard


N Registration

Page: 49.10

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 52 DOORS ITEM

SUBJECT

52-10-03 Passenger Exit Stop Fitting

CAT

No INS

MIN REQ

C

56

54

C

108 106 For A321 fleet

REMARKS OR EXCEPTIONS For A318/A319 and A320 fleet

(O)One per exit may be inoperative provided the airplane is flown in an unpressurized configuration. PLACARD Install 52-10-03 INOP placard, adjacent to lower ECAM Display. OPERATIONS (O) 52-10-03 Aircraft is to be operated unpressurized. Aircraft altitude is limited to 10000 ft, and climb and descent rates should not exceed 500 ft per minute. Refer to FCOM/PRO/SPO-20 FLIGHT WITHOUT CABIN PRESSURIZATION


N Registration

Page: 52.1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 52 DOORS SUBJECT

CAT

No INS

52-10-04 Emergency Operation Cylinder Damper Functions

C C

4 8

ITEM

MIN REQ

0 0

REMARKS OR EXCEPTIONS For A318/A319/A320 Fleet For A321 Fleet (M) May be inoperative Damper Function if the Emergency Opening Function operates normally. NOTE 1: If the Emergency Opening Function is inoperative or bottle pressure indicator is out limits, the aircraft can not be release to fly. NOTE 2: Notify to crewmembers about operation door precaution.

PLACARD 1. 2.

Install 52-10-04 INOP placard, adjacent to lower ECAM Display. Install a placard on affected door “OPERATE WITH PRECAUTION - DAMPER INOP”.

MAINTENANCE (M) 52-10-04 Check the Door Opening/Closing operates normally: 1.

Make sure the affected door (s) opening normally in accordance with Aircraft Maintenance Manual TASK 52-10-00-010-001.

2.

Make sure the affected door (s) closing normally in accordance with Aircraft Maintenance Manual TASK 52-10-00-410-001.

Emergency Opening Function

Damper Function

Door- Damper and Emergency-Operation Cylinder


N Registration

Page: 52.2


SUBJECT

52-10-05 Door Bottle Pressure Indication (On PTP/FAP)

CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Moved to items 23-73-07 3) for aircraft without mod. 30354 and 23-73-08 7) for aircraft with mod. 30354. NOTE: For Avianca fleet refer to 23-73-08 7).


N Registration

Page: 52.3


SUBJECT

CAT

No INS

MIN REQ


52-30-01 Cargo Door Actuators Without Mod 25044 With Mod 25044

Not applicable to Avianca. Avianca fleet has included Mod. 25044 A

4

2

(M) One per door may be inoperative provided: a) Integrity of Yellow hydraulic system is not affected, b) Wind velocity does not exceed 30 knots, and c) Operation of the door with a single actuator is limited to 75 flight cycles.

C

4

0

(M) May be inoperative provided: a) Integrity of Yellow hydraulic system is not affected, and b) Door(s) is manually closed and locked.

PLACARD Install 52-30-01 INOP Placard adjacent to applicable door operation selector. MAINTENANCE (M) 52-30-01 CAUTION: The door can be opened using a crane provided the actuators have been deactivated as indicated below: Deactivate the cargo Door Actuator in accordance with Aircraft Maintenance Manual TASK 52-36-00-040001.


N Registration

Page: 52.4


SUBJECT

52-30-02 Cargo Door Locking Hooks And Spools System

CAT

No INS

MIN REQ


C

12

10

(M)(O)One locking hook or one spool per door may be inoperative provided: a) The remainder are normal, and b) The airplane is flown in an unpressurized configuration.

PLACARD Install 52-30-02 INOP Placard adjacent to applicable cargo door operation selector. OPERATIONS (O) 52-30-02 1. 2. 3. 4.

Aircraft is to be operated unpressurized. Aircraft altitude is limited to 10000 ft. Climb and descent rates should not exceed 500 ft per minute. Refer to FCOM/PRO/SPO-20 FLIGHT WITHOUT CABIN PRESSURIZATION

MAINTENANCE (M) 52-30-02 FWD Cargo Compartment Deactivate the Locking Hooks and Spools in the FWD Cargo compartment door in accordance with Aircraft Maintenance Manual TASK 52-31-00-040-003. AFT Cargo compartment Deactivate the Locking Hooks and Spools in the AFT Cargo compartment door in accordance with Aircraft Maintenance Manual TASK 52-32-00-040-003.


N Registration

Page: 52.5


SUBJECT

52-30-03 Hand Pump

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS (M) May be inoperative provided the integrity of the Yellow hydraulic system is not affected.

PLACARD Install 52-30-03 INOP Placard adjacent to hand pump in service panel and adjacent to lower ECAM display. MAINTENANCE (M) 52-30-03 Deactivate the Hand Pump and in accordance with Aircraft Maintenance Manual TASK 52-36-00-040-002.


N Registration

Page: 52.6


SUBJECT

52-30-04 Cargo Door(s) Opening Electrical Control System

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS (O) May be inoperative provided the affected cargo door(s) is verified closed on ECAM door page prior to each departure. NOTE: Any cargo door control function that operates normally may be used.

C

1

0

May be inoperative provided: a) Hand pump operates normally, and b) Cargo doors are fully open during loading and unloading. NOTE: Any cargo door control function that operates normally may be used.

1) Open and Locked (Green) Lights

D

2

0

(O) May be inoperative and associated cargo compartment used, provided cargo door is fully open during loading and unloading.

PLACARD Install 52-30-04 INOP Placard adjacent to applicable selector in service panel and adjacent to lower ECAM display. OPERATIONS (O) 52-30-04 Notify Dispatch Prior to each departure, verify with the maintenance personnel that the affected cargo door is properly closed and corroborate that the same door is closed on ECAM door page. OPERATIONS (O) 52-30-04 1) ON GROUND When the Cargo Door Open/Locked Indicator light is inoperative, it is necessary to inform the ground personnel: ‐ To visually check that the affected cargo door is in the fully open position, with no downward movement after releasing the lever of the manual selector valve. ‐ To visually check that the lever of the manual selector valve stays in the neutral position.


N Registration

Page: 52.7


SUBJECT

52-33-01 Bulk Cargo Door Balance mechanism

CAT

No INS

MIN REQ

C

1

0

REMARKS OR EXCEPTIONS (M) May be inoperative or damaged provided: a) A safety hold device is used to maintain the door in the open position, and b) A visual check is made to confirm that the door is correctly closed and locked after each use. NOTE: Applicable to A320 and A321 aircraft only.

PLACARD Install 52-33-01 INOP Placard adjacent to lower ECAM display. MAINTENANCE (M) 52-33-01 I. II.

III.

Install a placard on the bulk cargo door to warn ground personnel that bulk cargo door balance mechanism is inoperative. When opening the bulk cargo door 1 Push door upwards until hook engages 2 Use strap or rope holder for additional device to safely maintain the door in open position. When closing the bulk cargo door 1 Remove the strap or rope holder 2 Support the door before handle is turned in "OPEN" position to release hook. 3 Lower the door slowly to the closed position. 4 After the handle is turned to the "LOCKED" position, check that door is correctly locked, door skin faired with fuselage and outer door handle faired with door.


N Registration

Page: 52.8


SUBJECT

52-50-01 Flight Deck Door Lock Solenoid


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable to Avianca fleet. Refer to Item 52-50-02

N Registration

Page: 52.9


CAT

No INS

MIN REQ


A

1

0

(M)(O) May be inoperative provided: a) Automatic locking system is deactivated, b) Door dead bolt operates normally and is used to lock the door, c) Alternate procedures are established and used for locking and unlocking the door using the deadbolt, and d) Repairs are made within two flight days.

a) UNLOCK Function

C

1

0


b) LOCK Function

C

1

0

(M)(O)May be inoperative provided: a) The cockpit door locking system keypad is deactivated, and b) Alternate procedures are established and used.

2) OPEN Light

C

1

0

3) FAULT Light

C

1

0

(O) May be inoperative provided all LEDs on CKPT DOOR CONT Panel are operative.

4) Buzzer

C

1

0

(M)(O)May be inoperative provided: a) Keypad is deactivated, and b) Alternate procedures are established and used.

5) Keypad

C

1

0

(M)(O)May be inoperative provided: a) Keypad is deactivated, and b) Alternate procedures are established and used.

C

2

0

(O) May be inoperative provided Alternate procedures are established and used.

C

2

1

A

2

0

SUBJECT

52-50-02 Cockpit Door Locking System (Automatic System) (Mod. 32088 and 32090) FAR 25.795 compliant

1) Cockpit Door Toggle Switch

a) Green and Red LEDs 6) Pressure Rate Sensors

May be inoperative provided repairs are made within two flight days.

(Continued)


N Registration

Page: 52.10


SUBJECT

CAT

No INS

MIN REQ

C

3

2

One may be inoperative provided that the associated door release strike is failed in the open/unlocked position.

C

3

2

(M) One may be inoperative provided associated door release strike is deactivated or removed.

C

5

0

(O) May be inoperative provided associated FAULT light is verified to operate normally.


52-50-02 Cockpit Door Locking System (Automatic System) (Mod. 32088 and 32090) FAR 25.795 compliant (Continued) 7) Door Release Strikes(Catch Spring, Solenoid, Bolt)

8) Control Unit LED's

PLACARD Install 52-50-02 INOP Placard on/or adjacent to inoperative component or panel. OPERATIONS (O) 52-50-02 The Captain will brief the Flight Crew and the Flight Attendants of the inoperative Cockpit Door Locking System. Normal/Emergency flight deck entry procedures will be followed as referenced in the Flight Operations Manual or MOV (Manual de Operaciones de Vuelo). OPERATIONS (O) 52-50-02 -1) a) UNLOCK function: Before flight: Alternate normal procedures will be established before departure in order to remind the cabin crew to use the cabin interphone or the passenger address system to communicate with cockpit crew to request access to the cockpit.

(Continued)


N Registration

Page: 52.11


SUBJECT

CAT

No INS

MIN REQ


52-50-02 Cockpit Door Locking System (Automatic System) (Mod. 32088 and 32090) FAR 25.795 compliant (Continued) Before the first flight under this item: NORM and LOCK functions are verified to operate normally: Close the cockpit door and verify by manual inspection that it is locked when the toggle switch of the COCKPIT DOOR panel is in the NORM position, Ask a flight crew member to perform the emergency access procedure (FCOM/PRO/SUP-25 PG 1/4) Set the toggle switch of the COCKPIT DOOR panel to the LOCK position Verify that the door remains closed and locked and the Keypad and buzzer are inhibited. OPERATIONS (O) 52-50-02 -1)b): LOCK function: Before flight: Cockpit Crew will brief crew that the Keypad is inoperative. Alternate normal procedures will be established before departure in order to remind the cabin crew to use the cabin interphone or the passenger address system to communicate with cockpit crew to request access to the cockpit. Before the first flight under this item: NORM and UNLOCK function are verified to operate normally: Close the cockpit door and verify by manual inspection that it is locked when the toggle switch of the COCKPIT DOOR panel is in the NORM position, Set the toggle switch of the COCKPIT DOOR panel to the UNLOCK position, Verify that the door is unlocked. OPERATIONS (O) 52-50-02 -3) Fault Light Before the first flight under this item: NORM and LOCK functions are verified to operate normally: Close the cockpit door and verify by manual inspection that it is locked when the toggle switch of the COCKPIT DOOR panel is in the NORM position, Ask a flight crew member to perform the emergency access procedure (FCOM/PRO/SUP-25 PG 1/4). Set the toggle switch of the COCKPIT DOOR panel to the LOCK position Verify that the door remains closed and locked and the Keypad and buzzer are inhibited. OPERATIONS (O) 52-50-02 -4): Buzzer. A minimum of two people have to remain in the cockpit for the duration of the flight. Before flight: Flight Crew will brief Flight Attendants that the interphone system will be used to request access to the cockpit.

(Continued)


N Registration

Page: 52.12


SUBJECT

CAT

No INS

MIN REQ


52-50-02 Cockpit Door Locking System (Automatic System) (Mod. 32088 and 32090) FAR 25.795 compliant (Continued) OPERATIONS (O) 52-50-02 --5) Keypad: At least two people must be always present in the cockpit throughout the entire flight Before flight: Flight crew will brief cabin crew that the interphone system will be used to request access to the cockpit. OPERATIONS (O) 52-50-02 -5)a) Green and Red Leds: Before flight: Brief cabin crew that the green and/or red LED(s) on the Keypad are inoperative. OPERATIONS (O) 52-50-02 -8): Control Unit LED’s: Before the first flight under this item: Check that the FAULT light comes on when lamp test is performed by setting the ANN LT switch on the TEST position. MAINTENANCE (M) 52-50-02 This procedure applies to comply with the general note at the beginning of the MMEL Item 01-52-50-02 (Cockpit Door Locking System (CDLS)). 1 2 3 4

Make sure that access to the flight compartment is available. Make sure that the aircraft electrical circuits are energized. Open, safety and tag C/B 1MQ. Put the aircraft back to the serviceable condition.

MAINTENANCE (M) 52-50-02 –1) b) Deactivate the Fixed Interior Cockpit Door Locking System (CDLS) Cockpit Door Toggle Switch Lock Function in accordance with Aircraft Maintenance Manual TASK 52-51-00-040-002. MAINTENANCE (M) 52-50-02 -4) Deactivate the Fixed Interior Cockpit Door Locking System (CDLS) Buzzer in accordance with Aircraft Maintenance Manual TASK 52-51-00-040-003. (Continued) Revision: 27 May 20, 2014

N Registration

Page: 52.13


SUBJECT

CAT

No INS

MIN REQ


52-50-02 Cockpit Door Locking System (Automatic System) (Mod. 32088 and 32090) FAR 25.795 compliant (Continued) MAINTENANCE (M) 52-50-02 -5) Refer to Aircraft Maintenance Manual (AMM) task card number 52-51-00-040-007 MAINTENANCE (M) 52-50-02 -7) Refer to Aircraft Maintenance Manual (AMM) task card number 52-51-00-040-010


N Registration

Page: 52.14


SUBJECT

52-50-03 Cockpit Door Secondary Locking System (Deadbolt) (Mod. 33777) FAR 25.795 Compliant


CAT

No INS

MIN REQ


C

1

0

Applicable to A319, A320 and A321 aircraft only, except to N266CT aircraft. May be inoperative provided automatic lock controls operate normally.

N Registration

Page: 52.15


SUBJECT

52-60-01 Entrance Stairs (With Mod 23308)


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable to Avianca fleet. Avianca fleet does not have Airstairs installed.

N Registration

Page: 52.16


SUBJECT

CAT

No INS

MIN REQ

C C

8 4

0 0

For A321 Fleet For A318/A319/A320 fleet (O) May be inoperative provided: a) A visual check is made before each departure to ensure that the affected door(s) is closed and locked, and b) White SLIDE ARMED light on the affected door does not illuminate when the door is closed and locked and slide armed.

C C

8 4

0 0

For A321 Fleet For A318/A319/A320 fleet (O) May be inoperative for day operations provided a visual check is made before each departure to ensure that the affected door(s) is closed and locked.

B B

8 4

0 0

For A321 Fleet For A318/A319/A320 fleet (O) May be inoperative provided: a) A visual check is made before each departure to ensure that the affected door(s) is closed and locked, and b) White SLIDE ARMED light on the affected door remains illuminated when the door is closed and locked and slide armed.

C C

8 4

0 0

For A321 Fleet For A318/A319/A320 fleet (M)(O) May be inoperative provided: a) A visual check is made before each departure to ensure that the affected door(s) is closed and locked, and b) Control circuit of affected door slide lighting system is verified to operate normally.

C C

8 4

0 0

For A321 Fleet For A318/A319/A320 fleet (O) May be inoperative for day operations provided a visual check is made before each departure to ensure that the affected door(s) is closed and locked.


52-70-01 ECAM DOOR Page Indications 1) Passenger Doors a) Open Indication

b) Closed Indication

(Continued)


N Registration

Page: 52.17


CAT

No INS

MIN REQ

C C

4 2

0 0

Applicable to A320 aircraft. Applicable to A318 and A319 aircraft. (M)(O) May be inoperative provided: a) A visual check is made before each departure to ensure that the affected exit(s) is closed and locked, and b) SLIDE Indication on ECAM DOOR page illuminates white when the exits are closed and locked.

C C

4 2

0 0

Applicable to A320 aircraft. Applicable to A318 and A319 aircraft. (M)(O) May be inoperative for day operations provided a visual check is made before each departure to ensure that the affected exit(s) is closed and locked.

C C

4 2

0 0

Applicable to A320 aircraft. Applicable to A318 and A319 aircraft. (M)(O) May be inoperative for day operations provided a visual check is made before each departure to ensure that the affected exit(s) is closed and locked.

3) Cargo Door

C C

3 2

0 0

Applicable to A320 and A321 aircraft. Applicable to A318 and A319 aircraft. (M)(O) Indications may be inoperative provided a visual check is made before each departure to confirm that doors are closed and locked.

4) Avionics Compartment Access Door

C

4

0

(M)(O) Indications may be inoperative provided a visual check is made before each departure to confirm that doors are closed and locked.

SUBJECT


52-70-01 ECAM DOOR Page Indications (Continued) 2) Overwing Emergency Exits (A318/A319/A320) a) Open Indication

b) Closed Indication

5) Airstairs Door

Not applicable to Avianca. Avianca fleet does not have installed this system.

PLACARD Install 52-33-01 INOP Placard adjacent to lower ECAM display.

(Continued) Revision: 29 October 23, 2014

N Registration

Page: 52.18


SUBJECT

CAT

No INS

MIN REQ


52-70-01 ECAM DOOR Page Indications (Continued) OPERATIONS (O) 52-70-01 1) a)Open Indication All sets of provisos. General Information If passenger doors /emergency exits (for A321) are affected, indications on the PTP or the FAP may be affected. If passenger doors are affected, the time recorded in the ACARS movement report may be wrong. The SLIDE ARMED light on passenger doors may be permanently illuminated. Note: this line is applicable to second and third set of provisos. After Engine Start -In the case of false door alert: EMER CANC pb.............................................................PRESS Note: the limitation MAX FL: 100/MEA remains displayed on the STATUS SD page. Before Takeoff

T.O CONFIG pb.......................................................................PRESS In the T.O MEMO, the “T.O CONFIG NORMAL” line will not replace the “T.O CONFIG……….TEST” line. Consider normal configuration for takeoff provided that no alert was displayed during the T.O CONFIG TEST. OPERATIONS (O) 52-70-01 1) b) Closed Indication All sets of provisos. General Information If passenger doors /emergency exits (for A321) are affected, indications on the PTP or the FAP may be affected. If passenger doors are affected, the time recorded in the ACARS movement report may be wrong. OPERATIONS (O) 52-70-01 2) All sets of provisos. GENERAL INFORMATION Indications on the PTP or the FAP may be affected (Continued)


N Registration

Page: 52.19


SUBJECT

CAT

No INS

MIN REQ


52-70-01 ECAM DOOR Page Indications (Continued) AFTER ENGINE START In the case of false door alert: EMER CANC pb................................................................................................................. Press Note: the limitation MAX FL : 100/MEA remains displayed on the STATUS SD page. BEFORE TAKEOFF

‐ T.O CONFIG pb....................................................................................................................Press In the T.O MEMO, the "T.O CONFIG NORMAL" line will not replace the "T.O CONFIG . . TEST" line. ‐ Consider normal configuration for takeoff provided that no alert was displayed during the T.O CONFIG TEST. OPERATIONS (O) 52-70-01 3) GENERAL INFORMATION If the cargo doors are affected, the time recorded in the ACARS movement report may be wrong. If cargo indication is inoperative due to a proximity switch failure: The relevant cargo heating is inhibited. For live animal transportation, use the Live Animal Transportation Calculation Tool. AFTER ENGINE START In the case of false door alert: EMER CANC pb................................................................................................................. Press Note: the limitation MAX FL : 100/MEA remains displayed on the STATUS SD page. BEFORE TAKEOFF

‐ T.O CONFIG pb....................................................................................................................Press In the T.O MEMO, the "T.O CONFIG NORMAL" line will not replace the "T.O CONFIG . . TEST" line. ‐ Consider normal configuration for takeoff provided that no alert was displayed during the T.O CONFIG TEST. (Continued)


N Registration

Page: 52.20


SUBJECT

CAT

No INS

MIN REQ


52-70-01 ECAM DOOR Page Indications (Continued) OPERATIONS (O) 52-70-01 4) AFTER ENGINE START In the case of false door alert: EMER CANC pb................................................................................................................. Press Note: the limitation MAX FL : 100/MEA remains displayed on the STATUS SD page. BEFORE TAKEOFF

‐ T.O CONFIG pb....................................................................................................................Press In the T.O MEMO, the "T.O CONFIG NORMAL" line will not replace the "T.O CONFIG . . TEST" line. ‐ Consider normal configuration for takeoff provided that no alert was displayed during the T.O CONFIG TEST. MAINTENANCE (M) 52-70-01 –1)b) ECAM DOOR Page indications, for closed indication, refer to Aircraft Maintenance Manual (AMM) 52-7300-710-001A MAINTENANCE (M) 52-70-01 –2)a) ECAM DOOR Page indications, for open indication, refer to Aircraft Maintenance Manual (AMM) 52-7000-040-010 MAINTENANCE (M) 52-70-01 –2)b) ECAM DOOR Page indications, for closed indication, refer to Aircraft Maintenance Manual (AMM) 52-7000-040-010 MAINTENANCE (M) 52-70-01 -3) ECAM DOOR Page indications, for Cargo Door, refer to Aircraft Maintenance Manual (AMM) 52-70-00040-001 MAINTENANCE (M) 52-70-01 -4) ECAM DOOR Page indications, for Avionics Compartment Access Door, refer to Aircraft Maintenance Manual (AMM) 52-70-00-040-004


N Registration

Page: 52.21

Avianca AIRBUS A318/A319/A320 MINIMUM EQUIPMENT LIST ATA 52 DOORS 52-70-02 CABIN PRESSURE Light (On Doors)

C

8

0

For A321 Fleet

C

4

0

For A18/A319/A320 fleet (O)May be inoperative provided alternate procedures are established and used.

OPERATIONS (O) 52-70-02 Install a warning notice on affected door View ECAM press page to ensure cabin is at the same level as airfield prior to opening doors. PIC must inform cabin crew members when aircraft is not pressurized before doors are open.


N Registration

Page: 52.22

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 56 WINDOWS ITEM 56-11-01

SUBJECT Front Windshields

CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Deleted, MMEL REV 21. NOTE: Refer to Aircraft Maintenance (AMM), Structural Repair Manual (SRM), or Aircraft Flight Manual.


N Registration

Page: 56.1


SUBJECT Fixed Lateral Windows

CAT

No INS

MIN REQ



N Registration

Page: 56.2


SUBJECT Sliding Windows

CAT

No INS

MIN REQ



N Registration

Page: 56.3

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 56 WINDOWS ITEM

SUBJECT

56-21-01 Cabin Windows

CAT

No INS

MIN REQ



N Registration

Page: 56.4

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 71 POWER PLANT ITEM 71-00

SUBJECT

No CAT INS

MIN REQ


CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) Fault (s) Indicated by ENG (1and/or 2) FADEC a) Except for CFM565B affected by CFM VSB 73-0241

A

2

Applicable to A318. May be inoperative for 10 consecutive calendar days.

b) For CFM 56- 5B affected by CFM VSB 73-0241 only)

A

2

Applicable to A319, A320Ceo and A321Ceo. (M) May be inoperative for 10 consecutive calendar days provided it is verified before the first flight of each day that the CFDS does not report any fault on a T12 sensor.

A

2

Applicable to A319, A320Ceo and A321Ceo. May be inoperative for 25 flight hours or 3 flight days whichever occurs first.

2) Fault(s) Indicated by ENG (1 and/ or 2) EIU

C

2

3) Fault(s) Indicated by EVMU

C

2 NOTE 1: Dispatch with any of the above maintenance status messages displayed on ECAM is permitted without CFDS interrogation. NOTE 2: The systems are designed to be fault tolerant for a period of time given on the category column in accordance with MEL preamble information. Quantities are not required for this item while the idea is to allow these fault indication.

4) Fault(s) Indicated by ENG (1 AND 2) EIU (Aircraft Without Mod 22327)

Deleted, MMEL REV 21.

(Continued)


N Registration

Page: 71.1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 71 POWER PLANT ITEM 71-00

SUBJECT

No CAT INS

MIN REQ


CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY (Continued)

MAINTENANCE NOTE (M) 71-00 1. Before each departure, please make sure that the Pre-pressurization fault signal is NOT displayed on LOWER ECAM display. If this fault signal is displayed the aircraft can not be dispatched. MAINTENANCE (M) 71-00 1) To check of the ENG FADEC Maintenance Messages displayed on ECAM page refer to Aircraft Maintenance Manual (AMM) 73-29-00-040-001.


N Registration

Page: 71.2

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 71 POWER PLANT ITEM

SUBJECT

71-10-01 ENG 1(2) FAN COWL NOT CLSD Alert (A319neo/A320neo/ A321neo)

No CAT INS

C

MIN REQ

2

0

REMARKS OR EXCEPTIONS Applicable to N759AV, N761AV, N764AV and N765AV (O) May be inoperative provided associated fan cowl door latches are checked closed before each flight.

PLACARD 71-10-01 Install INOP placard adjacent to the EWD OPERATIONS (O) 71-10-01 EXTERIOR WALKAROUND During the exterior walkaround, the flight crew must check carefully on both sides of each engine that all the fan cowl door latches are correctly closed. If necessary, the flight crew should use a torch and crouch to perform the check.

Revision: 36 June 30. 2017

N Registration

Page: 71.3

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 71 POWER PLANT ITEM

SUBJECT

No CAT INS

MIN REQ




N Registration

Page: 71.4

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 73 ENGINE FUEL & CONTROL ITEM

SUBJECT

73-10-01 Fuel Switches (V2500 Engines Only)


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Incorporated into 71-00.

N Registration

Page: 73.1


SUBJECT

73-10-02 Fuel Return-to- Tank Valves (V2500 Engines Only)


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Incorporated into 71-00.

N Registration

Page: 73.2


SUBJECT

CAT

No INS

MIN REQ


C

2

1

One may be inoperative in the closed position on one engine provided that the APU generator is operative.

C

2

0

One or both may be inoperative in the open position provided that the four wing tank pumps are operative.

73-11-01 Fuel Recirculation System (CFM 56-5B Engines and CFM LEAP-1A Engines) 1) Valves

2) Solenoids


3) Oil Temperature Sensors



N Registration

Page: 73.3


SUBJECT

73-11-02 Burner Staging Valve System (CFM Engines Only)

CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS This ITEM Burner Staging Valve System is only applicable to ENGINES CFM56-5A, therefore is not applicable to AVIANCA Engines. AVIANCA only operates ENGINES CFM56-5B

1) Valves (Without Mod. 25887, 26338, 26577, 27725, or 28307) 2) Valves (With Mod. 25887, 26338, 26577, 27725, or 28307) 3) Solenoid Wraps


N Registration

Page: 73.4


SUBJECT

CAT

No INS

MIN REQ


73-11-03 Fuel Metering Valve Systems 1) Feedback System



N Registration

Page: 73.5


SUBJECT

73-20-01 Engine FADEC System


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Incorporated into 71-00 sub item 1).

N Registration

Page: 73.6


SUBJECT

73-20-02 RESERVED


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Deleted, On MMEL Revision 1.

N Registration

Page: 73.7


SUBJECT

73-20-03 Minimum Idle on Ground

CAT

No INS

MIN REQ


C

2

0

(O) May be inoperative provided the Airplane Flight Manual performance penalties are applied. NOTE: Continuous ignition is permanently ON. (IAE Engines only)

OPERATIONS (O) 73-20-03 (Applicable to A318, A319 and A320 except N723AV, N726AV, N759AV, N761AV, N764AV, N765AV and A320 with Sharklets) Takeoff performance: Use the following penalties for takeoff performance determination if no takeoff data (predetermined by using OCTOPUS program or other equivalent program with present failure case taken into account) is available. Takeoff must be performed with full thrust. A318-111:

A318-112:

A319-112:

A319-115 except N723AV and N726AV:

A320-214 without Sharklets

Landing performance: No penalty. (Continued)


N Registration

Page: 73.8


SUBJECT

CAT

No INS

MIN REQ


73-20-03 Minimum Idle on Ground (Continued) OPERATIONS (O) 73-20-03 (Applicable to A320 with Sharklets, N723AV, N726AV, N759AV, N761AV, N764AV, N765AV and A321-211) FLIGHT PREPARATION/LIMITATIONS

Takeoff performance: The takeoff performance must be determined by using OCTOPUS program or other equivalent program with present failure case. Launch PEP.

Landing performance: No penalty.

OPERATIONS (O) 73-20-03 (Applicable to A320-233, A319-132 and A321-231) GENERAL INFORMATION Continuous ignition is permanently on. FLIGHT PREPARATION/LIMITATIONS

Takeoff performance: The takeoff performance must be determined by using OCTOPUS program or other equivalent program with present failure case. Launch PEP.

Landing performance: No penalty.


N Registration

Page: 73.9


SUBJECT

CAT

No INS

MIN REQ


C

2

0

(O) May be inoperative provided: a) N1 rated control Mode operates normally on both engines, b) Approach minimums do not require their use, and c) AFM performance penalties are applied.

73-20-04 EPR Control Modes (IAE Engines Only)

NOTE: Autothrust and alpha floor are inoperative. PLACARD Install INOP placard adjacent to upper ECAM display. OPERATIONAL (O) 73-20-04 GENERAL INFORMATION The autothrust function is inoperative. α floor is not available. β target is not available. Maximum landing capability is CAT 1. FLIGHT PREPARATION/LIMITATIONS Takeoff performance: The following method may be used for takeoff performance determination if no takeoff data (Predetermined by using OCTOPUS program or other equivalent program with present failure case taken into account) is available. Launch PEP. Single engine cruise: See "N1 MODE THRUST CONTROL" in Refer to FCOM/PER-THR-N1 MODE THRUST CONTROL. Go-Around performance: See "N1 MODE THRUST CONTROL" in Refer to FCOM/PER-THR-N1 MODE THRUST CONTROL. BEFORE ENGINE START ‐ ENG 1 N1 MODE pb-sw.......................................................................................................... ON ‐ ENG 2 N1 MODE pb-sw.......................................................................................................... ON FOR TAKEOFF Flexible takeoff is not permitted. The takeoff must be performed without FDs as follows: ‐ Set both FDs to OFF ‐ Select V2 on the FCU ‐ Acquire pitch attitude about 15 ° to maintain the speed target with two engines operative, about 12.5 ° in the case of an engine failure. (Continued) Revision: 27 May 20, 2014

N Registration

Page: 73.10


SUBJECT

CAT

No INS

MIN REQ


73-20-04 EPR Control Modes (IAE Engines Only) (Continued) Above 100 ft AGL, when appropriate: ‐ Set both FDs to ON (basic guidance modes engage) ‐ Engage OP CLB and select appropriate speed and lateral mode ‐ AP use as required. When reaching the thrust reduction altitude: Set both thrust levers to CL detent. When reaching the acceleration altitude: Resume normal acceleration and climb procedures. Note: CLB or LVR CLB will not flash on the FMA as the A/THR is not available. GO-AROUND Note: To perform a manual Go-Around with no FD, the PF simultaneously announces his/her intention, disengages the AP, applies TOGA and initiates the rotation. The Go-Around must be performed without FDs as follows: ‐ Set AP (if engaged) to OFF ‐ Set both FDs (if engaged) to OFF ‐ Acquire pitch attitude about 15 ° to maintain the speed target with two engines operative, about 12.5 ° in the case of an engine failure. ‐ Adjust pitch to maintain VAPP. When appropriate: ‐ Set both FDs to ON (basic guidance modes engage) ‐ Engage OP CLB and select appropriate speed and lateral mode ‐ AP use as required. When reaching the thrust reduction altitude: Set both thrust levers to CL detent. When reaching the acceleration altitude: Resume normal acceleration and climb procedures. Note: CLB or LVR CLB will not flash on the FMA as the A/THR is not available. FMS does not engage the GO AROUND phase.


N Registration

Page: 73.11


SUBJECT

73-20-05 Flex Temp Function


CAT

No INS

MIN REQ


C

2

0

May be inoperative provided takeoff is performed in TOGA or de-rated mode.

N Registration

Page: 73.12


SUBJECT

73-20-06 De-rated Takeoff Mode


CAT

No INS

MIN REQ

D

2

0

REMARKS OR EXCEPTIONS May be inoperative on one or both engines provided takeoff is performed in TOGA or FLX mode.

N Registration

Page: 73.13


SUBJECT

73-20-09 Aircraft 28V Power Supply (IAE Engines Only)


CAT

No INS

MIN REQ

C

4

2

REMARKS OR EXCEPTIONS Channel B power supply may be inoperative on one or both engines.

N Registration

Page: 73.14


SUBJECT

73-20-10 Engine Bump


CAT

No INS

MIN REQ

C

2

0

REMARKS OR EXCEPTIONS May be inoperative provided benefit of bump is not utilized for determination of takeoff performance.

N Registration

Page: 73.15


SUBJECT

73-20-11 Engine Overthrust Protection System (A318 or A319neo/A320neo/ A321neo)


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Applicable to A318 Aircraft and N759AV, N761AV, N764AV and N765AV.

A

2

1

One may be inoperative for six flight

N Registration

Page: 73.16


SUBJECT

CAT

No INS

MIN REQ


73-30-02 Fuel Used Indications Aircraft without Mod.30368/MP P6578 Aircraft with Mod. 30368/MP P6578

Not Applicable to Avianca Fleet. Avianca Fleet has incorporated Mod. 30368 C

2

0

(M) May be inoperative provided: a) Associated tank fuel quantity indication system operates normally, b) Fuel-On-Board indication operates normally, and c) F. USED 1+2 indication is considered inoperative.

MAINTENANCE (M) 73-30-02 1. 2. 3. 4. 5. 6.

Install Fuel Used Indications INOP adjacent to upper ECAM Display. On MCDU get access to the SYSTEM REPORT / TESTS menu. Push the Button shown by FUEL. Push the Button shown by SYSTEM STATUS. Push the Button shown by CH 1 FQIS STAUS. NO fault must be shown on the MCDU.


N Registration

Page: 73.17


SUBJECT

CAT

No INS

MIN REQ

C

2

1


73-30-03 Fuel Filter Clog Cautions on ECAM E/WD

1) IAE Engines and CFM Engines with Mod 28397 or Mod 28398 and CFM LEAP-1A Engines

Applicable to A318, A319, A320, A321 except N603AV, N690AV, N694AV, N695AV, N696AV, N725AV, N729AV and N730AV. (M) One may be inoperative provided associated filter is changed before the next flight and then once each flight day.

2) PW 6000 Engines

0

0


3) PW 1100G Engines

0

0


MAINTENANCE (M) 73-30-03 Replace the fuel filter in accordance with AMM TASK 73-11-10-920-001


N Registration

Page: 73.18


SUBJECT

73-30-04 Fuel Filter Clog Indication on ECAM System Display

CAT

No INS

MIN REQ

C

2

0


PLACARD Install 70-30-04 INOP placard adjacent to the ECAM display.


N Registration

Page: 73.19


SUBJECT

73-30-05 MINOR FAULT Cautions on ECAM E/WD (A319neo/A320neo/A321 neo)

CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Applicable to N759AV, N761AV, N764AV and N765AV

C

2

1

One may be inoperative.

PLACARD Install 70-30-05 INOP placard adjacent to the ECAM E/WD display.


N Registration

Page: 73.20


SUBJECT

CAT

No INS

MIN REQ


73-30-06 FUEL FILTER DEGRAD Cautions on ECAM E/WD (A319neo/A320neo/A321 neo with PW1100G Engines)


(A319neo/A320neo/ A321neo with CFM LEAP1A Engines)

Applicable to N759AV, N761AV, N764AV and N765AV A

2

1

One may be inoperative for a maximum of three flights or 6 flight-hours, whichever occurs first, provided ENG 1(2) FUEL SENSOR FAULT alert is not displayed on the EWD for the opposite engine.

C

2

1

(M) One may be inoperative provided associated filter is replaced before the next flight and then every 100 flight-hours.

PLACARD Install 70-30-06 INOP placard adjacent to the ECAM E/WD display. MAINTENANCE (M) 73-30-06 Replace the filter in accordance with AMM TASK 73-34-00-040-803-A


N Registration

Page: 73.21


No INS

MIN REQ

(A319neo/A320neo/A321 neo with PW1100G Engines)

0

0


(A319neo/A320neo/A321 neo with PW1100G)

0

0


SUBJECT

CAT


73-30-07 FUEL SENSOR FAULT Cautions on ECAM E/WD

Applicable to N759AV, N761AV, N764AV and N765AV

(A319neo/A320neo/ A321neo with CFM LEAP1A Engines) A

2

1

(A319neo/A320neo/ A321neo with CFM LEAP1A)

One may be inoperative for a maximum of three flights or 6 flight-hours, whichever occurs first, provided: a) Associated FUEL FILTER SENSOR subtitle is displayed on the EWD, and b) Associated ENG 1(2) FUEL FILTER DEGRAD alert was not displayed on the previous flight. Applicable to N759AV, N761AV, N764AV and N765AV

C

2

1

(M) One may be inoperative provided: a) Associated FUEL FILTER SENSOR subtitle is displayed on the EWD, and b) Associated filter is replaced before the next flight and then every 100 flight-hours

PLACARD Install 70-30-07 INOP placard adjacent to the ECAM E/WD display. MAINTENANCE (M) 73-30-07 Replace the filter in accordance with AMM TASK 73-34-00-040-803-A


N Registration

Page: 73.22


SUBJECT

CAT

No INS

MIN REQ


73-30-08 HEAT SYS DEGRAD Cautions on ECAM E/WD (A319neo/A320neo/A321n eo with PW1100G)


(A319neo/A320neo/A321n eo with PW1100G)



N Registration

Page: 73.23


SUBJECT

73-30-09 FUEL STRAINER CLOG Cautions on ECAM E/WD (A319neo/A320neo/ A321neo with CFM LEAP1A)

CAT

No INS

MIN REQ


A

2

1

One may be inoperative for 10 consecutive calendar-days provided: a) Associated ENG 1(2) FUEL FILTER DEGRAD alert is not displayed on the EWD, and b) ENG 1(2) FUEL SENSOR FAULT alert is not displayed on the EWD on the opposite engine.



N Registration

Page: 73.24


SUBJECT

73-30-10 HP FUEL VALVE Cautions on ECAM E/WD (A319neo/A320neo/ A321neo with CFM LEAP1A)

CAT

No INS

MIN REQ


C

2

1

One may be inoperative provided: a) Associated HP FUEL VALVE NOT OPEN subtitle is displayed on the EWD, and b) Affected engine can be started.



N Registration

Page: 73.25


SUBJECT

73-30-11 FADEC IDENT FAULT Cautions on ECAM E/WD (A319neo/A320neo/ A321neo with CFM LEAP1A)

CAT

No INS

MIN REQ


C

2

0

(M) One or both may be inoperative provided there is no disagreement between the associated engine identification contained in the FADEC and the identification written on the engine plate.

PLACARD Install 70-30-11 INOP placard adjacent to the ECAM E/WD display. MAINTENANCE (M) 73-30-11 Check the identification written on the engine plate in accordance with the AMM TASK 73-29-00-040-802-A


N Registration

Page: 73.26

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 74 IGNITION ITEM

CAT

No INS

MIN REQ

a) System A

C

2

2

(M) NOTE: A and B input or output from the exciter boxes may be swapped in order to restore System A operative.

b) System B (CFM 56-5A Engines With Mod. 22333 or CFM 56-5B Engines or CFM LEAP-1A Engines)

C

2

0

(O) May be inoperative provided System A is operative.

0

0

Not applicable to Avianca. Avianca fleet is powered by CFM-56-5B engines.

SUBJECT


74-31-01 Ignition Systems 1) CFM Engines

c) System B (CFM 56-5A Engines Without Mod. 22333) 2) IAE Engines a) System A

C

2

1

(O) Except for ER operations, may be inoperative on one engine only.

b) System B

C

2

0

(O) May be inoperative provided system A operates normally.

c) System A and B

C

4

2

(O) Except for ER operations, two igniters may be inoperative provided they are not on the same engine. NOTE: On IAE engines, system A must be considered inoperative on both engines if the common power supply line from 401XP 115VAC ESS BUS is inoperative as a result of either a loss of electrical continuity or a short circuit (C/B Engine/1 AND 2 IGN/SYS A (49VUA03) tripped).

PLACARD Install INOP placard adjacent to engine mode selector. OPERATIONAL (O) 74-31-01 1) CFM Engines and CFM LEAP-1A for A320-251N (NEO) only System B BEFORE ENGINE START On ground, if the FADEC selects the Ignition System B during an automatic start, the engine fails to start and the ENG 1(2) START FAULT [IGNITION FAULT] alert appears on the EWD. Then, the FADEC automatically initiates a second engine start attempt with both ignition systems selected.

(Continued)


N Registration

Page: 74.1


SUBJECT

CAT

No INS

MIN REQ


74-31-01 Ignition Systems (Continued) To prevent a possible start, abort with the triggering of the ENG 1(2) START FAULT [IGNITION FAULT] alert, perform one of the following: A manual engine start: Refer to FCOM/PRO-NOR-SUP-ENG Manual Engine Start - Procedure. An automatic engine start:

 Before Engine Start. ENGINE/IGN/(affected) ENG 1 (or 2)/SYS B (121 VU P41/P42) C/B …………………..PULL  After Engine Start ENGINE/IGN/ENG 1(2)/SYS B (121VU P41 or P42) C/B..................................................... PUSH

OPERATIONAL (O) 74-31-01 1) Applicable to CFM LEAP-1A A321-253N (NEO) only BEFORE ENGINE START On ground, if the FADEC selects the Ignition System B during an automatic start, the engine fails to start and the alert related to the failure of the Ignition System B appears on the EWD. Then, the FADEC automatically initiates an additional engine start attempt with both ignition systems selected. To maximize the probability to start the engine at the first attempt, the Ignition System A must be selected by the FADEC. Perform one of the following engine starts: An automatic engine start:

 Before Engine Start. ENGINE/IGN/(affected) ENG 1 (or 2)/SYS B (121 VU P41/P42) C/B …………………..PULL  After Engine Start ENGINE/IGN/ENG 1(2)/SYS B (121VU P41 or P42) C/B..................................................... PUSH A manual engine start: Refer to FCOM/PRO-NOR-SUP-ENG Manual Engine Start - Procedure. It remains possible to perform an automatic engine start without pulling the circuit breakers of the Ignition System B. The first start attempt may be successful because the FADEC may select the Ignition System A. However, the first start attempt may fail because the FADEC may select the Ignition System B.

(Continued)


N Registration

Page: 74.2


SUBJECT

CAT

No INS

MIN REQ


74-31-01 Ignition Systems (Continued) OPERATIONAL (O) 74-31-01 2) IAE Engines BEFORE ENGINE START On ground, if the FADEC selects the Ignition System B during an automatic start, the engine fails to start and the ENG 1(2) START FAULT [IGNITION FAULT] alert appears on the EWD. To prevent a possible start abort with the triggering of the ENG 1(2) START FAULT [IGNITION FAULT] alert, perform a manual engine start. Refer to FCOM/PRO-NOR-SUP-ENG Manual Engine Start - Procedure

MAINTENANCE (M) 74-31-01 Refer to Aircraft Maintenance Manual (AMM) Task Number 74-31-00-040-005. Ignition Systems. 1. The A System is also called Right Spark Igniter. 2. The Right Spark igniter must be operative always. 3. In order to sure that the Right Spark igniter is always operative, do a swapped between Left Spark igniter and Right spark igniter following the information located in AMM subtask 74-31-00-020-051


N Registration

Page: 74.3


SUBJECT

CAT

No INS

MIN REQ


C

4

0

(M) May be inoperative provided IGN FAULT warning is verified to operate normally on ECAM.

74-31-02 ECAM Indications (Lower Display) 1) Selected igniter

OPERATIONAL NOTE: Refer to OpsProc 74-07-01A Selected Igniter Indication on the ENGINE SD page MAINTENANCE (M) 74-31-02 Refer to Aircraft Maintenance Manual (AMM) Task Number 74-31-00-040-002 Check of Ignition Fault Warning 1. Install Selected Igniter INOP adjacent to lower ECAM Display. 2. After Engines Start do the following: 

If Engine 1 is affected. 1. C/B ENGINE/1 and 2/IGN/SYS A (49VU A03) 2. C/B ENGINE/IGN/ENG 1 (121 VU P39) 3. C/B ENGINE/IGN/ENG 1 (121 VU P41)



OPEN. OPEN. OPEN.

If Engine 2 is affected. 1. C/B ENGINE/1 and 2/IGN/SYS A (49VU A03) 2. C/B ENGINE/IGN/ENG 2 (121 VU P40) 3. C/B ENGINE/IGN/ENG 2 (121 VU P42)

OPEN. OPEN. OPEN.

Note: Check on ECAM upper display that IGN FAULT Warning is triggered Above C/B


CLOSE.

N Registration

Page: 74.4


SUBJECT

CAT

No INS

MIN REQ


C

4

3

(M) One may be inoperative provided associated ignition system is verified to operate normally once each flight day.

C

4

2

(M) Two may be inoperative provided associated ignition system is verified to operate normally before each departure.

C

4

2

One or two may be inoperative

74-31-03 IGN FAULT Caution on ECAM 1) CFM Engines

2) IAE Engines MAINTENANCE (M) 74-31-03

1. Put a Warning Notice in the Cockpit to tell persons that the ignition warning system does not operate. 2. Do the operational test of the Ignition system in accordance with AMM TASK 74-31-00-040-001 Reference 74-00-00-710-043 Operational Test of the Ignition System and MAKE SURE that the ignition system is operative. 3. Make and entry in the log book.


N Registration

Page: 74.5


SUBJECT

CAT

No INS

MIN REQ




N Registration

Page: 74.6

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 75 BLEED AIR ITEM

SUBJECT

CAT

No INS

MIN REQ


75-21-01 HP Turbine Active Clearance Control System (CFM 56 Engines Only) 1) HPTC Valves


2) Feedback Systems


3) HPTC Torque Motor Wraps


4) HPTC Thermocouples HP Turbine Active Clearance Control System (CFM LEAP-1A Engines Only)

Incorporated into 73-20-01. C

2

0

Applicable to N759AV, N761AV, N764AV and N765AV (M) One or both may be inoperative provided the affected HPTACC valve is deactivated in the closed position.

PLACARD 75-21-01 Install INOP placard adjacent to the ECAM / EWD MAINTENANCE 75-21-01 Deactivate the HPTACC valve in accordance the AMM task 75-21-00-040-801-A


N Registration

Page: 75.1


SUBJECT

75-21-02 Active Clearance Control Actuators(V2500 Engines Only)


CAT

No INS

MIN REQ


N Registration

Page: 75.2


SUBJECT

CAT

No INS

MIN REQ


75-22-01 LP Turbine Active Clearance Control (CFM Engines Only) 1) LPTC Valves


2) Feedback Systems


3) LPTC Torque Motors



N Registration

Page: 75.3


SUBJECT

75-22-02 Buffer Air Check Valve (A319neo/A320neo/ A321neo with PW 1100G engines)


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not Applicable to Avianca.

N Registration

Page: 75.4


SUBJECT

CAT

No INS

MIN REQ


75-23-01 Rotor Active Clearance Control (CFM Engines Only)


1) RACC Valves


2) Feedback Systems


3) RACC Torque Motors


N Registration

Page: 75.5


SUBJECT

CAT

No INS

MIN REQ


75-25-01 TCC/TACC Valve


a) A318 with PW 6000 engines


b) A319neo/A320neo /A321neo with PW1100G Engines


N Registration

Page: 75.6


SUBJECT

75-25-02 TCA Valve (PW 6000 engines only)


CAT

No INS

MIN REQ


N Registration

Page: 75.7


SUBJECT

CAT

No INS

MIN REQ


75-30-01 Compressor Control System 1) VSV (V2500 Engines only)


2) VSV (CFM Engines Only)


a) Torque Motors


b) Feedback Systems


N Registration

Page: 75.8


SUBJECT

CAT

No INS

MIN REQ


75-30-02 Compressor Control System VBV (CFM Engines Only)


1) Feedback Systems


2) Torque Motors


N Registration

Page: 75.9


SUBJECT

CAT

No INS

MIN REQ




N Registration

Page: 75.10

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 76 ENGINE CONTROL SUBJECT

CAT

No INS

76-11-01 Thrust Lever Position Sensor

A

4

ITEM

MIN REQ


3

One may be inoperative on one engine provided: a) The A/THR is operative, b) Both LGCIUs are operative, and c) Repairs are made within 3 flight days.



N Registration

Page: 76.1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 76 ENGINE CONTROL ITEM

SUBJECT

CAT

No INS

MIN REQ




N Registration

Page: 76.2

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 77 ENGINE INDICATING ITEM

CAT

No INS

MIN REQ

a) Aircraft without Mod. 30368/MP P6578

B

2

1

Not applicable to Avianca Fleet. Avianca fleet has the Mod 30368

b) Aircraft with Mod. 30368/MP P6578

B

2

1

May be inoperative provided the total fuel flow indication is considered inoperative.

B

1

0

May be inoperative or replaced by XX

SUBJECT


77-00-01 ECAM Indications(Upper Display) 1) Fuel Flow (Upper Display)

2) Total Fuel Flow Indication (Fuel Page) (With Mod. 30368/MP P6758) 3) Bleed Configuration Indication on the EWD (PACKS, NAI, WAI) (A319neo/A320neo/ A321neo)

Applicable to N759AV, N761AV, N764AV and N765AV C

3

0

May be inoperative.

D

3

0


PLACARD Install 77-00-01 INOP placard adjacent to the ECAM upper display


N Registration

Page: 77.1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 77 ENGINE INDICATING ITEM

CAT

No INS

MIN REQ

1) Nacelle Temperature

C

2

0

2) N1 Vibration

C

2

1

3) N2 Vibration

C

2

1

SUBJECT


77-00-02 ECAM Indications (Lower Display)


N Registration

Page: 77.2

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 78 EXHAUST ITEM

SUBJECT

CAT

No INS

MIN REQ


78-11-09 T/R Door Tertiary Lock 1) A318 with PW600 Engines


2) A319neo/A320neo /A321neo with PW 1100G Engines


3) A319neo/A320neo /A321neo with CFM LEAP-1A Engines

Applicable to N759AV, N761AV, N764AV, and N765AV. C

2

1

One may be failed locked provided the associated T/R is considered inoperative.

C

2

0

(M)(O) One or both may be inoperative provided: a) Associated thrust reverser door tertiary lock is secured in the open position, and b) ENG 1(2) REV LOCKED alert associated with the affected thrust reverser is not displayed on the EWD after deactivation.

PLACARD Install 78-11-09 INOP placard near upper ECAM display MAINTENANCE PROCEDURE 78-11-03-3 Deactivate the door tertiary lock system in accordance AMM task 78-37-00-040-803A OPERATIONS 78-11-03-3 DURING COCKPIT PREPARATION After application of the maintenance procedure: Check that the ENG 1(2) REV LOCKED alert that is NOT displayed on the EWD. Disregard the ENG 1(2) REV MINOR FAULT alert that is displayed on the EWD.


N Registration

Page: 78.1


SUBJECT

78-11-10 T/R Tertiary Lock Valve (PW 6000 Engines Only)


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Not applicable to Avianca.

N Registration

Page: 78.2


SUBJECT

CAT

No INS

MIN REQ

C

2

1


78-30-01 Thrust Reverser Systems (A318/A319ceo/A320ceo/ A321ceo)

(M)(O) One may be inoperative provided: a) Inoperative reverser is deactivated and secured in the stowed position, and no operations or procedures require its use, b) All stow and deploy switches on the inoperative reverser operate normally (CFM 56 only), c) Both LVDT on the inoperative reverser are checked operative (IAE only), d) ENG 1 (2) REV INHIBITED caution is displayed on ECAM E/WD after deactivation (PW 6000 only), e) ENG 1 (2) REV UNLOCKED caution is not present on ECAM E/WD after deactivation (PW 6000 only), f) ENG 1 (2) REV PRESSURIZED caution is not present on ECAM E/WD after deactivation, g) Wheel brake tachometers operate normally, h) Main wheel braking system operates normally, and i) Flight crew is provided with the following statement via appropriate means (e.g. dispatch release, MEL (O) procedure, etc.):

j)

“For a landing conducted with one deactivated thrust reverser, ensure that both engine thrust levers are retarded to the IDLE detent for the flare and the touchdown. Select both thrust levers to reverse when applying reverse thrust”, and Appropriate performance adjustments are applied.

(Continued)


N Registration

Page: 78.3


SUBJECT

CAT

No INS

MIN REQ


78-30-01 Thrust Reverser Systems (Continued) Applicable to N759AV, N761AV, N764AV and N765AV (A319neo/A320neo/A321 neo)

C

2

1

(M)(O) One may be inoperative provided:

a) Inoperative reverser is deactivated and secured in the stowed position, and no operations or procedures require its use, b) ENG 1 (2) REV INHIBITED caution is displayed on ECAM E/WD after deactivation, c) ENG 1 (2) REV UNLOCKED caution is not present on ECAM E/WD after deactivation, d) ENG 1 (2) REV PRESSURIZED caution is not present on ECAM E/WD after deactivation, e) Wheel brake tachometers operate normally, f) Main wheel braking system operates normally, g) Flightcrew is provided with the following statement via appropriate means (e.g., dispatch release, MEL (O) procedure, etc.): “For a landing conducted with one deactivated thrust reverser, ensure that both engine thrust levers are retarded to the IDLE detent for the flare and the touchdown. Select both thrust levers to reverse when applying reverse thrust”, and h) Appropriate performance adjustments are applied.

(Continued)


N Registration

Page: 78.4


SUBJECT

CAT

No INS

MIN REQ


78-30-01 Thrust Reverser Systems (Continued) Applicable to N759AV, N761AV, N764AV and N765AV (A319neo/A320neo/ A321neo with CFM LEAP-1A Engines)

C

2

1

(M)(O) One may be inoperative provided: a) Inoperative reverser is deactivated and secured in the stowed position, and no operations or procedures require its use, b) ENG 1 (2) REV INHIBITED caution is displayed on ECAM E/WD after deactivation, c) ENG 1 (2) REV UNLOCKED caution is not present on ECAM E/WD after deactivation , d) The ICV is checked closed before each flight, e) Wheel brake tachometers operate normally, f)

Main wheel braking system operates normally,

g) Flightcrew is provided with the following statement via appropriate means (e.g., dispatch release, MEL (O) procedure, etc.): “For a landing conducted with one deactivated thrust reverser, ensure that both engine thrust levers are retarded to the IDLE detent for the flare and the touchdown. Select both thrust levers to reverse when applying reverse thrust”, and h) Appropriate performance adjustments are applied.

(Continued)


N Registration

Page: 78.5


SUBJECT

CAT

No INS

MIN REQ


78-30-01 Thrust Reverser Systems (Continued) OPERATIONAL (O) 78-30-01 (Applicable to Aircraft equipped with CFM engines only except CFM LEAP-1A engines). NOTE: For a landing conducted with one deactivated thrust reverser, ensure that both

engine thrust levers are retarded to the IDLE detent for the flare and the touchdown. Select both thrust levers to reverse when applying reverse thrust FLIGHT PREPARATION/LIMITATIONS Performance Adjustments:

DURING COCKPIT PREPARATION (Not applicable to A318) - If affected engine is fitted with EEC Software standard SCN21 (refer to Note 1 at the End of this operational procedure): After application of the maintenance procedure And When the FADEC have power: Check that the ENG (AFFECTED SIDE) REV INHIBITED alert is displayed on the EWD. FOR TAKEOFF During the takeoff briefing, the flight crew must review: ‐ The status of the thrust reversers, and ‐ The use of the thrust reversers REJECTED TAKEOFF Ensure that both engine thrust levers are set to IDLE detent, then: - If one thrust reverser is inoperative: Use both thrust levers when applying reverse thrust. ( Continued )


N Registration

Page: 78.6


SUBJECT

CAT

No INS

MIN REQ


78-30-01 Thrust Reverser Systems (Continued) Note: ENG (AFFECTED SIDE) REVERSER FAULT alert is displayed on the EWD after selection of the reverse thrust. (Not applicable to N195AV, N454AV, N477AV, N519AV, N536AV, N538AV, N557AV, N562AV, N632AV, N723AV, N724AV, N726AV, N728AV, N740AV, N741AV, N742AV, N743AV, N744AV, N745AV, N746AV, N748AV, N750AV, N751AV, N753AV, N754AV. - If both thrust reversers are inoperative: Do not move the thrust levers to reverse. IN FLIGHT Should a failure occur with "LDG DIST PROC.......APPLY" message displayed on the STATUS SD page, and Whatever the actual thrust reversers selection at landing: To calculate the LDG DIST with the in-flight failure, do not take credit of the inoperative thrust reversers (Refer to QRH PER-A). DURING APPROACH During the approach briefing, the flight crew must review: ‐ The status of the thrust reversers, and ‐ The use of the thrust reversers Before the touchdown, ensure that both engine thrust levers are set to IDLE detent for the flare. - After touchdown, if one thrust reverser is inoperative: Use both thrust levers when applying reverse thrust. For automatic roll-out with one thrust reverser inoperative, Refer to AFM/LIM-22-FGS CAT II / CAT III Operations (Applicable to A318 only). Note: ENG (AFFECTED SIDE) REVERSER FAULT alert is displayed on the EWD after selection of the reverse thrust. (Not applicable to N195AV, N454AV, N519AV, N536AV, N538AV, and N557AV) - After touchdown, if both thrust reversers are inoperative: Do not move the thrust levers to reverse. ( Continued)


N Registration

Page: 78.7


SUBJECT

CAT

No INS

MIN REQ


78-30-01 Thrust Reverser Systems (Continued) .OPERATIONAL (O) 78-30-01 (Applicable to Aircraft equipped with IAE and A321-253N (neo) N759AV and N761AV). NOTE: For a landing conducted with one deactivated thrust reverser, ensure that both

engine thrust levers are retarded to the IDLE detent for the flare and the touchdown. Select both thrust levers to reverse when applying reverse thrust. FLIGHT PREPARATION/LIMITATIONS Performance Adjustments:

DURING COCKPIT PREPARATION - If affected engine is fitted with EEC Software standard SCN21 (refer to Note 1 at the End of this operational procedure): - After application of the maintenance procedure and When the FADEC have power: Check that the ENG (AFFECTED SIDE) REV INHIBITED alert is displayed on the EWD. FOR TAKEOFF During the takeoff briefing, the flight crew must review: ‐ The status of the thrust reversers, and ‐ The use of the thrust reversers REJECTED TAKEOFF Ensure that both engine thrust levers are set to IDLE detent, then: - If one thrust reverser is inoperative: Use both thrust levers when applying reverse thrust. ( Continued) Revision: 36 June 30, 2017

N Registration

Page: 78.8

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 78 EXHAUST ITEM (78-3001

SUBJECT

CAT

No INS

MIN REQ


Thrust Reverser Systems (Continued)

Note: If the affected engine is not fitted with EEC Software standard SCN21 (refer to Note 1 at the End of this operational procedure): ENG (AFFECTED SIDE) REVERSER FAULT alert is displayed on the EWD after selection of the reverse thrust. - If both thrust reversers are inoperative: Do not move the thrust levers to reverse. IN FLIGHT Should a failure occur with "LDG DIST PROC.......APPLY" message displayed on the STATUS SD page, and Whatever the actual thrust reversers selection at landing: To calculate the LDG DIST with the in-flight failure, do not take credit of the inoperative thrust reversers (Refer to QRH FPE-IFL). DURING APPROACH During the approach briefing, the flight crew must review: ‐ The status of the thrust reversers, and ‐ The use of the thrust reversers FOR LANDING Before the touchdown, ensure that both engine thrust levers are set to IDLE detent for the flare. - After touchdown, if one thrust reverser is inoperative: Use both thrust levers when applying reverse thrust. For automatic roll-out with one thrust reverser inoperative, Refer to AFM/LIM-22-FGS CAT II / CAT III Operations. Note: If the affected engine is not fitted with EEC Software standard SCN21 (refer to Note 1 at the End of this operational procedure): ENG (AFFECTED SIDE) REVERSER FAULT alert is displayed on the EWD after selection of the reverse thrust. - After touchdown, if both thrust reversers are inoperative: Do not move the thrust levers to reverse.

(Continued)


N Registration

Page: 78.9


SUBJECT

CAT

No INS

MIN REQ


78-30-01 Thrust Reverser Systems (Continued) OPERATIONAL (O) 78-30-01 (Applicable to A320-251N (neo) Aircraft equipped with CFM LEAP-1A engines only). FLIGHT PREPARATION/LIMITATIONS Performance Adjustments:

DURING COCKPIT PREPARATION After application of the maintenance procedure and When the FADEC have power: Check that the ENG (AFFECTED SIDE) REV INHIBITED alert is displayed on the EWD FOR TAKEOFF During the takeoff briefing, the flight crew must review: ‐ The status of the thrust reversers, and ‐ The use of the thrust reversers REJECTED TAKEOFF Ensure that both engine thrust levers are set to IDLE detent, then: If one thrust reverser is inoperative: Use both thrust levers when applying reverse thrust. If both thrust reversers are inoperative: Do not move the thrust levers to reverse

(Continued)


N Registration

Page: 78.10


SUBJECT

CAT

No INS

MIN REQ


78-30-01 Thrust Reverser Systems (Continued) IN FLIGHT Should a failure occur with "LDG DIST PROC.......APPLY" message displayed on the STATUS SD page, and Whatever the actual thrust reversers selection at landing: To calculate the LDG DIST with the in-flight failure, do not take credit of the inoperative thrust reversers (Refer to QRH PER-A). DURING APPROACH During the approach briefing, the flight crew must review: ‐ The status of the thrust reversers, and ‐ The use of the thrust reversers FOR LANDING Before the touchdown, ensure that both engine thrust levers are set to IDLE detent for the flare. After touchdown, if one thrust reverser is inoperative: Use both thrust levers when applying reverse thrust. For automatic roll-out with one thrust reverser inoperative, Refer to AFM/LIM-22-FGS CAT II / CAT III Operations. After touchdown, if both thrust reversers are inoperative: Do not move the thrust levers to reverse.

MAINTENANCE (M) 78-30-01 To deactivation of the Thrust Reverser System to aircraft equipped with CFM engines refer to AMM 78-3000-040-040. To deactivation of the Thrust Reverser System to aircraft equipped with IAE engines refer to AMM 78-3000-040-013. To deactivation of the Thrust Reverser System to aircraft equipped with CFM LEAP-1A engines refer to AMM 78-30-00-040-810 (Continued)


N Registration

Page: 78.11


SUBJECT

CAT

No INS

MIN REQ


78-30-01 Thrust Reverser Systems (Continued) Note 1: To determine if EEC software standard is SCN21, follow the next procedure: 1. On the overhead maintenance panel 50VU, make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is on 2. On the MCDU do the following Test:  Push the line key adjacent to the ENG indication. The SYSTEM REPORT/TEST ENG menu comes into view.  Push the line key adjacent to the FADEC 1(2) A (B) indication. The ENGINE 1(2) MAIN MENU page comes into view.  Push the line key adjacent to the TROUBLE SHOOTING indication. The FADEC 1(2) A(B) TROUBLE SHOOTING MENU page comes into view.  Push the line key adjacent to the EEC CONFIGURATION indication. The FADEC 1(2) EEC CONFIGURATION page comes into view.  Read the data from the MCDU; locate EEC P/N in order to determine the EEC software standard SCN21. EECs P/Ns that has incorporated standard SCN21 must be: P/N 824972-X-(022) or P/N 808050-X-(068).  On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.  Stop the MCDU. 3. On the overhead maintenance panel 50VU, make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off


N Registration

Page: 78.12


SUBJECT

78-30-02 Thrust Reverser Inhibition Relay Contacts (CFM) (Thrust Reverser Permission Switches (V2500)

CAT

No INS

MIN REQ

C

4

2

REMARKS OR EXCEPTIONS (M)Two contacts may be inoperative provided they are on the same engine and the associated reverser is deactivated.

MAINTENANCE (M) 78-30-02 Refer to Maintenance procedure on AVA A318/A319/A320 MEL on item 78-30-01, in order to follow the same instructions for Thrust Reverser deactivation.


N Registration

Page: 78.13


SUBJECT

78-30-03 T/R Directional Valve Solenoid Wraps (CFM Engines Only)


CAT

No INS

MIN REQ


N Registration

Page: 78.14


SUBJECT

78-30-04 T/R Pressure Switches (CFM Engines Only)


CAT

No INS

MIN REQ


N Registration

Page: 78.15


SUBJECT

78-30-05 T/R Stow Switches (CFM Engines Only)


CAT

No INS

MIN REQ


N Registration

Page: 78.16


SUBJECT

78-30-06 T/R Deploy Switches (CFM Engines Only)


CAT

No INS

MIN REQ


N Registration

Page: 78.17


SUBJECT

78-30-07 T/R Indications (IAE, CFM, and PW Engines)


CAT

No INS

MIN REQ


C

2

1

One may be inoperative provided the associated T/R is considered inoperative.

N Registration

Page: 78.18


SUBJECT

78-30-08 Thrust Reverser Stow & Lock Sensors (V2500 Engines Only)


CAT

No INS

MIN REQ


N Registration

Page: 78.19


SUBJECT

78-30-09 T/R Pressurizing Valve Solenoid Wraps (CFM Engines Only)


CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Incorporated into 73-20-01. (formerly 30-02), Rev. 10 MMEL.

N Registration

Page: 78.20


SUBJECT

78-31-01 REVERSER CTL FAULT Caution on ECAM EWD (A319neo/A320neo/A321 neo)

CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Applicable to N759AV, N761AV, N764AV and N765AV.

C

2

1

(O) One may be inoperative provided: a) Wheel brake tachometers operate normally, b) Main wheel braking system operates normally, c) Flightcrew is provided with the following statement via appropriate means (e.g., dispatch release, MEL (O) procedure, etc.): “For a landing conducted with REVERSER CTL FAULT on one side, ensure that both engine thrust levers are retarded to the IDLE detent for the flare and the touchdown. Select both thrust levers to reverse when applying reverse thrust”, and d) Appropriate performance adjustments are applied.

PLACARD Install 78-31-01 INOP placard adjacent to ECAM EWD display. OPERATIONAL (O) 78-30-01 (Applicable to A320-251N (neo) Aircraft equipped with CFM LEAP-1A engines only). NOTE: For a landing conducted with one deactivated thrust reverser, ensure that both

engine thrust levers are retarded to the IDLE detent for the flare and the touchdown. Select both thrust levers to reverse when applying reverse thrust.

( Continued )


N Registration

Page: 78.21


SUBJECT

CAT

No INS

MIN REQ


78-31-01 REVERSER CTL FAULT Caution on ECAM EWD ( Continued) FLIGHT PREPARATION/LIMITATIONS Performance Adjustments:

DURING COCKPIT PREPARATION After application of the maintenance procedure and When the FADEC have power: Check that the ENG (AFFECTED SIDE) REV INHIBITED alert is displayed on the EWD FOR TAKEOFF During the takeoff briefing, the flight crew must review: ‐ The status of the thrust reversers, and ‐ The use of the thrust reversers REJECTED TAKEOFF Ensure that both engine thrust levers are set to IDLE detent, then: If one thrust reverser is inoperative: Use both thrust levers when applying reverse thrust. If both thrust reversers are inoperative: Do not move the thrust levers to reverse

( Continued )


N Registration

Page: 78.22


SUBJECT

CAT

No INS

MIN REQ


78-31-01 REVERSER CTL FAULT Caution on ECAM EWD ( Continued) IN FLIGHT Should a failure occur with "LDG DIST PROC.......APPLY" message displayed on the STATUS SD page, and Whatever the actual thrust reversers selection at landing: To calculate the LDG DIST with the in-flight failure, do not take credit of the inoperative thrust reversers (Refer to QRH PER-A). DURING APPROACH During the approach briefing, the flight crew must review: ‐ The status of the thrust reversers, and ‐ The use of the thrust reversers FOR LANDING Before the touchdown, ensure that both engine thrust levers are set to IDLE detent for the flare. After touchdown, if one thrust reverser is inoperative: Use both thrust levers when applying reverse thrust. For automatic roll-out with one thrust reverser inoperative, Refer to AFM/LIM-22-FGS CAT II / CAT III Operations. After touchdown, if both thrust reversers are inoperative: Do not move the thrust levers to reverse.


N Registration

Page: 78.23


SUBJECT

78-31-02 REV MINOR FAULT Caution on ECAM EWD (A319neo/A320neo/A321 neo)

CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Applicable to N759AV, N761AV, N764AV and N765AV.

C

2

0

May be inoperative.

PLACARD Install 78-31-02 INOP placard adjacent to ECAM EWD display.


N Registration

Page: 78.24

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 79 ENGINE OIL ITEM

SUBJECT

79-20-01 Air Exchanger Air Valves (V2500 Engines Only)

CAT

No INS

MIN REQ

C

2

1

REMARKS OR EXCEPTIONS (O) One may be inoperative open provided the tank fuel temperature is above -20 degrees C at takeoff.

OPERATIONAL PROCEDURE BEFORE TAKEOFF On the FUEL SD page, check that the fuel temperature in the inner tank is above -20 °C.


N Registration

Page: 79.1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 79 ENGINE OIL SUBJECT

CAT

No INS

79-20-02 EMCD Visual Pop-Out Indicator (CFM-5B)

D

2

ITEM


MIN REQ

0

N Registration


Page: 79.2


SUBJECT

79-20-03 Air Oil Cooler Valve (PW 6000 Engines Only)


CAT

No INS

MIN REQ

0

0


N Registration

Page: 79.3


SUBJECT

CAT

No INS

MIN REQ

A

2

0


79-23-01 ENG 1(2) BEARING 4 OIL SYS Alert (IAE Engines With Mod. 24871/MP P3704)


May be inoperative provided: a) HI PRESS message is not displayed under ENG 1 (2) BEARING 4 OIL SYS caution on ECAM E/WD, and b) Repairs are made within three flight days.

N Registration

Page: 79.4


SUBJECT

79-31-01 Oil Quantity Indications

CAT

No INS

MIN REQ

B

2

1

REMARKS OR EXCEPTIONS (M) One may be inoperative provided: a) Associated oil quantity is verified before each departure, b) There is no evidence of abnormal consumption or leakage, and c) Associated ENG OIL PRESS, OIL TEMP indications operate normally.

MAINTENANCE (M) 79-31-01 1. Install Oil Quantity Indications INOP adjacent to lower ECAM Display, and put a WARNING notice in the cockpit to tell that the oil quantity indications does not operate. 2. On panel 115 VU put a warning notice to tell persons NOT to star the engine 1(2). 3. On panel 50VU make sure that the “ON” legend of the ENG/FADEC GND PWR/1(2) push button switch is off, and install a warning notice, to tell persons not to energize the FADEC 1 (2). 4. Check Oil quantity in the Oil Tank. 5. Add Oil if is necessary. 6. Open, safety and tag these C/B´s: Panel 121VU 1EN1 and 1EN2. 7. Remove the Warning notices from panel 50VU and 115VU. 8. Put a warning notice in the cockpit to tell persons that the oil quantity indication does not operate.


N Registration

Page: 79.5


SUBJECT

79-33-02 OIL LO PR Warning on ECAM (IAE or CFM56 Engines only)


CAT

No INS

MIN REQ

C

2

1

C

2

0


May be inoperative provided RCDR GND CTL is verified ON after engines are started.

N Registration

Page: 79.6


CAT

No INS

MIN REQ

C

2

1

2) IAE Engines S/N V10600 To V11304 and V11315, V11330, V11335 (Not Including V11280, V11302) Without #3 FAG Bearing P/N2A1165 Installed

0

0

Not applicable by IAE Engines S/N affected.

3) IAE Engines S/N V10600 To V11304 and V11315, V11330, V11335 (Not Including V11280 V11302) With#3 FAG Bearing P/N 2A1165 Installed

0

0

Not applicable by IAE Engines S/N affected.

4) PW Engines

0

0


SUBJECT


79-35-01 OIL FILTER CLOG Indications on ECAM Engine System Page 1) CFM or IAE Engines Excluding Those With S/N's V10600 To V11304 and V11315, V11330, V11335 (Not Including V11280, V11302)


N Registration

Page: 79.7


SUBJECT

CAT

No INS

MIN REQ


0

0

Not applicable to Avianca fleet. Avianca fleet is powered by CFM56-5B engines.

2

1

(M) One may be inoperative provided: a) Associated filter is replaced once each flight day, and b) Visual indicator (pop-out) on the electrical master chip detector is inspected when the filter is replaced and does not reveal the presence of metal chips or other contaminants.

0

0

Not applicable to Avianca fleet. Avianca fleet is powered by CFM56-5B engines.

79-35-02 OIL FILTER CLOG Caution on ECAM E/WD 1) CFM 56-5A Engines

2) CFM 56-5B Engines

C

3) PW 6000 Engines

Applicable to N759AV, N761AV, N764AV, and N765AV

4) PW1100G and CFM LEAP-1A Engines C

2

1

(M) One may be inoperative provided: a) Associated filter is replaced before the next flight and then every 150 flight-hours, and b) Associated magnetic chip detectors are inspected when the filter is replaced and do not reveal the presence of chips.

C

2

1

(M) One may be inoperative provided: a) Associated filter is replaced before the next flight and then every 150 flight-hours, b) Associated Oil Debris Monitoring System is verified operative when the filter is replaced, and c) Associated ENG 1(2) OIL CHIP DETECTED was not displayed on the EWD during the previous flight.

(Continued)


N Registration

Page: 79.8


SUBJECT

CAT

No INS

MIN REQ


A

2

1

(M) One may be inoperative for a maximum of 3 days or 30 flight-hours, whichever occurs first, provided: a) Associated ENG 1(2) OIL FILTER DEGRAD was not displayed on the EWD during the previous flight, and b) Associated magnetic chip detectors are inspected and do not reveal the presence of chips.

A

2

1

(M) One may be inoperative for a maximum of 3 days or 30 flight-hours, whichever occurs first, provided: a) Associated ENG 1(2) OIL FILTER DEGRAD was not displayed on the EWD during the previous flight, b) Associated ENG 1(2) OIL CHIP DETECTED was not displayed on the EWD during the previous flight, and c) Associated Oil Debris Monitoring System is verified operative.

79-35-02 OIL FILTER CLOG ECAM Caution on ECAM E/WD ( Continued) 4) PW1100G and CFM LEAP-1A Engines (Continued)

PLACARD Install 79-35-02 INOP placard adjacent to ECAM E/WD MAINTENANCE (M) 79-35-02-2 1. Put a WARNING NOTICE to tell persons NOT to start the engine. 2. Follow the AMM 79-35-00-040-044 procedure in order to replacement Main Oil filter. MAINTENANCE (M) 79-35-02-4 1. 2. 3. 4.

Put a WARNING NOTICE to tell persons NOT to start the engine. Follow the AMM 79-35-00-040-809-A procedure to replace the Main Oil filter. Follow the AMM 79-35-00-040-807-A to inspect the Magnetic Bar Follow the AMM 79-35-00-040-806-A to Check for no fault of the Oil Debris Monitoring System


N Registration

Page: 79.9


SUBJECT

CAT

No INS

MIN REQ

79-35-03 OIL FILTER DEGRAD Caution on ECAM EWD (PW 1100G and CFM LEAP-1A Engines)


Applicable to N759AV, N761AV, N764AV, and N765AV A

2

1

One may be inoperative for a maximum of 3 days, or 30 flight-hours, whichever occurs first.

C

2

1


C

2

1

(M) One may be inoperative provided: a) Associated filter is replaced before the next flight and then every 150 flight-hours, b) Associated Oil Debris Monitoring System is verified operative when the filter is replaced, and c) Associated ENG 1(2) OIL CHIP DETECTED was not displayed on the EWD during the previous flight.

PLACARD Install 79-35-03 INOP placard adjacent to the ECAM EWD

MAINTENANCE (M) 79-35-03 1. 2. 3. 4.



N Registration

Page: 79.10


SUBJECT

79-35-04 OIL SENSOR FAULT Caution on ECAM EWD (PW 1100G and CFM LEAP-1A Engines)

CAT

No INS

MIN REQ

REMARKS OR EXCEPTIONS Applicable to N759AV, N761AV, N764AV, and N765AV.

A

2

1

One may be inoperative for a maximum of 3 days, or 30 flight-hours, whichever occurs first, provided associated ENG 1(2) OIL FILTER DEGRAD was not displayed during the previous flight on the EWD.

C

2

1


C

2

1

(M) One may be inoperative provided: a) Associated filter is replaced before the next flight and then every 150 flighthours, b) Associated Oil Debris Monitoring System is verified operative when the filter is replaced, and c) Associated ENG 1(2) OIL CHIP DETECTED was not displayed on the EWD during the previous flight.

PLACARD Install 79-35-04 INOP placard adjacent to the ECAM EWD MAINTENANCE (M) 79-35-04 1. 2. 3. 4.



N Registration

Page: 79.11


SUBJECT

CAT

No INS

MIN REQ

79-35-05 OIL CHIP DETECTED Caution on ECAM EWD (PW1100G and CFM LEAP-1A Engines)

REMARKS OR EXCEPTIONS Applicable to N759AV, N761AV, N764AV, and N765AV.

A

2

1

One may be inoperative on the EWD for 10 flighthours.

A

2

1

(M) One may be inoperative on the EWD for 300 flight-hours or 20 consecutive calendar-days, whichever occurs first, provided associated magnetic chip detectors are inspected and do not reveal the presence of chips.

PLACARD Install 79-35-05 INOP placard adjacent to the ECAM EWD MAINTENANCE (M) 79-35-04 1. Put a WARNING NOTICE to tell persons NOT to start the engine. 2. Follow the AMM 79-35-00-040-807-A to inspect the Magnetic Bar


N Registration

Page: 79.12

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 80 STARTING ITEM

SUBJECT

CAT

No INS

MIN REQ

C

2

1


80-11-01 Start Valve System 1) Valves a) CFM/IAE Engines

b) PW6000 Engines

(M)(O) One may be inoperative provided: a) Valve is manually closed after engine start, and b) Associated igniter system operates normally. Not Applicable to Avianca

2) Solenoids


PLACARD Install 80-11-01 INOP adjacent to start valve switch. OPERATIONAL (O) 80-11-01 BEFORE ENGINE START Refer to FCOM/PRO-SUP-70 Start Valve Manual Operation MAINTENANCE (M) 80-11-01 To Manually Operate the Starter Valve to aircraft equipped with CFM engines refer to AMM 80-11-00-040 045. To Manually Operate the Starter Valve to aircraft equipped with IAE engines refer to AMM 80-11-00-040043.


N Registration

Page: 80.1


SUBJECT

80-11-02 ENG MAN START Controls


CAT

No INS

MIN REQ

C

2

0

N Registration


Page: 80.2


SUBJECT

80-11-03 FAULT light on ENGINE MASTER Panel


CAT

No INS

MIN REQ

C

2

0

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Page: 80.3


SUBJECT

80-11-04 ECAM Start Valve Position Indicators (Lower Display) (IAE Engines, CFM Engines or PW 6000 Engines)

CAT

No INS

MIN REQ

C

2

0

REMARKS OR EXCEPTIONS (M) May be inoperative provided start valve is verified closed after engine start.

MAINTENANCE (M) 80-11-04 1. Install a warning notice in the cockpit to tell the persons that the starter valve 1 (2) indicating system is inoperative. 2. Open the access door on fan cowl: a. FOR 1000EM1 b. 438CR c. FOR 1000EM2 d. 448CR 3. After the Engine cycle check on starter valve that the manual handle is in closed position. 4. Close the access door. Make an entry in the log book


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Page: 80.4

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST ATA 80 STARTING SUBJECT

CAT

No INS

80-11-05 AUTOSTART Controls

C

2

ITEM

MIN REQ

0

REMARKS OR EXCEPTIONS (O) May be inoperative provided manual start procedures are used.

OPERATIONS (O) 80-11-05 Refer to FCOM/PRO-SUP-70 Start Valve Manual Operation.


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Page: 80.5

Avianca AIRBUS A318/A319/A320 MINIMUM EQUIPMENT LIST ATA 80 STARTING



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Page: 80.6

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX CAT II/III

The purpose of CAT II/III operations is to provide an adequate and safe environment whenever our operations are conducted under low visibility and/or ceiling. Category II/III constitutes the main part of All Weather Operations (AWO), which also consists of Category I, takeoff and taxiing in low visibility conditions. Category II approach to the performance defined by FAA Advisory Circular 120-29, this approval shall apply to the autopilot flight director system in the fail-operative, fail-passive, and single channel autopilot configurations and dual flight director displays. Category III automatic approach and landing to the performance defined in the FAA Advisory Circular 12028C. This approval shall apply to the automatic landing system in the fail-passive (50 foot decision height) and fail-operative (no decision height limitation) configurations on ILS facilities approved for this operation. Avianca has issue "Maintenance & Operational Procedures Manual CAT II/III” to establish procedures to certify, operate and maintain operations under Meteorological Minimums CAT II/III. Those procedures and tasks are based on the Maintenance Planning Document (MPD) and Aircraft Maintenance Manual (AMM), and assure that the A318/A319/A320 aircraft is maintained for the operation in which was Type Certified, for more instructions and requirements refer to Avianca A318/A319/A320/A321 CAT II/III Manual.


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Page: CAT-1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX CAT II/III Number Installed Minimum required to CAT II Minimum required to CAT III Single Minimum required to CAT III Dual REMARKS OR EXCEPTIONS 2 1 1 2 2 2 2 2 2 1 1 1 1 1 1 1 1 0 1 1 1 0 1 1 2 1 1 2 2 1 1 2 If FAC 2 is inoperative downgrade the aircraft to CAT III Single

ITEM 22-10-01 22-10-03 22-10-04 22-10-05 22-30-01 22-30-03 22-63-01 22-66-01

SUBJECT Autopilot System 1) AP Disconnect Function Autoland Lights AP Disengagement Warning Autothrust Function AT Disengagement Warning SW Yaw Dampers Flight Augmentation Computer

22-81-03 1) c) 22-83-01 22-83-02

Auto Flight Control Panel APPR

1

1

1

1

FMGC Electrical Supply Split FMA indications on PFD

2 2

0 1

0 2

1 2

1) 2) 3)

AP/FD Related Indications Autothrust Related Indications Approach and landing capabilities

Two (2) FMA’s are required for CAT III single and CAT III dual operations, One (1) FMA is required for CAT II Operations. If one (1) FMA indication is INOP downgrade the aircraft to CAT II. If two (2) or more FMA indications are INOP downgrade the aircraft to CAT I

27-22-01 27-23-01

Rudder Trim Systems Rudder Travel Limiter Systems

2 2

1 1

1 1

2 1

27-93-01 29-10-03 30-42-03

ELAC Hydraulic Circuit Windshield Heating Systems

2 3 2

1 2 1

1 2 1

2 3 1

30-45-01

Windshield Wiper Systems

2

1

1

1

30-45-02

Rain Repellent Systems

2

1

1

1

31-53-01 31-63-01

Flight Warning Computer Display Units

32-31-01 32-42-01

Landing Gear Control & Interface Units Main Wheel Braking Systems BSCU Channels Systems

2 2 2 2 4 2

1 2 1 1 3 1*

1 2 2 1 3 1*

2 2 2 1 4 1

Nose Wheel Steering Systems

2

1*

1*

1

32-42-03

32-51-01

One (1) Rudder Travel Limiter System is required only for autoland with crosswind higher than 12 Kts.

For CAT II/III CAPT (LH) Windshield Heating Systems must operative. For CAT II/III CAPT (LH) Windshield Wiper Systems must operative. For CAT II/III CAPT (LH) Rain Repellent must operative. Primary Flight Display Units (PFD) Navigation Display Units (ND)

*For automatic rollout, one(1) is required. For autoland without automatic rollout, none is required. *For automatic rollout, one(1) is required. For autoland without automatic rollout, none is required.

(Continued)


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Page: CAT-2


ITEM

SUBJECT

Number Installed Minimum required to CAT II Minimum required to CAT III Single Minimum required to CAT III Dual REMARKS OR EXCEPTIONS For automatic rollout, one(1) is required. For 1 1* 1* 1 autoland without automatic rollout, none is required.

32-60-03

Antiskid

34-10-01

ADIRS IR

3

2

2

3

34-14-04 34-36-01 34-42-01

ADR Attitude Indication ILS Navigation Systems Radio Altimeter Systems

3 2 2 2

2 * 2 1

2 * 2 2

3 * 2 2

34-42-02

Automatic Call Out System

1

1

1

1

34-55-02

Marker Beacon

2

1

1

1


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If any Attitude Indicators are INOP downgrade the aircraft to CAT I *N1 + N2 + STBY If one (1) RA is INOP downgrade the aircraft to CAT II (both displays must be operative) One (1) Automatic Call out System is required only for autoland with crosswind higher than 12 Kts.

Page: CAT-3




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Page: CAT-4

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX PBN (RNAV-RNP) OPERATIONS

ICAO’s Performance Based Navigation (PBN) Concept aims to ensure global standardization of RNAV and RNP specifications and to limit the proliferation of navigation specifications in use world-wide. It is a new concept based on the use of Area Navigation Systems. Significantly, it is a move from a limited statement of required performance accuracy to more extensive statements of required performance in terms of accuracy, integrity, continuity and availability, together with descriptions of how this performance is to be achieved in terms of aircraft and crew requirements. ICAO´S PBN Concept replaces the RNP concept of the 1990s. Consequently, much of the terminology associated with the RNP Concept (such as RNP Type and RNP Value) does not exist in the PBN Concept. While the expression RNP is still used in the PBN Concept its only connotation relates to RNP specifications or applications requiring on-board-performance monitoring and alerting. ICAO’s PBN Concept may be used in route to reduce aircraft separation, and in terminal area to optimize arrival and departure procedures. For more instructions and requirements refer to the Avianca PBN Manual. Avianca has issued "Performance Based Navigation PBN Manual” to establish procedures to certify, operate and maintain operations under RNAV-RNP procedures. Those procedures are based on aircraft manufacture recommendations, authority requirements and assure that the A318/A319/A320/A321 aircraft is maintained for the operation in which was Type Certified. The appendix PBN (RNAV- RNP) OPERATIONS provide information about minimum equipment required to RNAV-RNP operations.


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Page: PBN-1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX PBN (RNAV-RNP) OPERATIONS Number Installed Minimum required to RNAV 10 Minimum required to RNAV 5 Minimum required to RNAV 2 or RNAV 1 Minimum required to RNP 2 ITEM

Minimum required to RNP 1

SUBJECT

Minimum required to Baro V/NAV Minimum required to RNP APPROACH Minimum required to RNP AR 0.1 Minimum Required to RVFP 22-10-01

Autopilot Systems.

2

NRa NRa NRa

1n

22-10-02

Flight Director Systems.

2

NR

NR

1

1n

1

2

NR

NR

NR

NR

Take Over p.b. Switch AP 22-10-03 1) Disconnect Function

NRa NR

NR

2

1

1

1

2

1

NR

NR

NR

2

NR

22-10-05

AP Disengagement Warning System.

1

NR

NR

NR

NR

NR

NR

NR

1

NR

22-10-06

Side Sticks and Rudder Locking Solenoids in AP Mode.

3

NR

NR

NR

NR

NR

NR

NR

1

NR

22-66-01

Flight Augmentation Computers (FAC). FAC 2.

1

NR

NR

NR

NR

NR

NR

NR

1

NR

22-72-01

Lateral Navigation.

2

1

1

1

1n

1

1

1

2

1

22-73-01

Performance Information and/or Vertical Navigation.

2

NR

NR

NR

NR

NR

NR

NR

1r

1O

2

NR

NR

NR

NR

NR

1

2

2

2

1

NR

NR

NR

NR

NR

NR

NR

1

NR

22-81-01 1) FCU Channels. Auto Flight 22-81-03 1) Control Panelc) APPR Engagement p.b.

(Continued)


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Page: PBN-2



SUBJECT

Minimum required to Baro V/NAV Minimum required to RNP APPROACH Minimum required to RNP AR 0.1 Minimum Required to RVFP Auto Flight Control Panel22-81-03 3) FCU Selection

Window (SPDMACH, HDG-TRK, ALT, V/S-FPA).

22-81-03 4)

22-81-03 7)

22-81-03 8)

22-81-03 9)

22-81-04 1)

22-81-04 2) a) b)

Auto Flight Control PanelHDG-V/S TRK-FPA Change Over p.b.

Auto Flight Control PanelEngagement p.b. Light Bars.

Auto Flight Control PanelV/S-FPA Selection Knob.

Auto Flight Control PanelV/S-FPA Push-to level OFF function.

EFIS Control PanelBaro Reference Display Windows.

4

NR

NR

NR

NR

NR

NR

NR

4

NR

1

NR

NR

NR

NR

NR

NR

NR

1

NR

3

NR

NR

NR

NR

NR

NR

NR

3s

NR

1

NR

NR

NR

NR

NR

NR

NR

1

NR

1

NR

NR

NR

NR

NR

NR

NR

1

NR

2

NR

NR

NR

NR

NR

NR

NR

2

NR

2

NR

NR

NR

NR

NR

NR

NR

2

NR

EFIS Control PanelBaro Reference Sel Outer Ring (Hg/hPa).

(Continued)


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Page: PBN-3



SUBJECT

Minimum required to Baro V/NAV Minimum required to RNP APPROACH Minimum required to RNP AR 0.1 Minimum Required to RVFP

22-81-04 4)

EFIS Control PanelOptional Data Display p.b.

EFIS Control 22-81-04 5) Panel-

10

NR

NR

NR

NR

NR

NR

NR

1m

NR

2

NR

NR

NR

NR

NR

NR

NR

2

NR

2

NR

NR

NR

NR

NR

NR

NR

2

NR

14

NR

NR

NR

NR

NR

NR

NR

6n

NR

2

2

1

1

2

1

1

1

2

1

4

NR

NR

NR

NR

NR

NR

NR

4

NR

2

2c

1

1

2c

1

1

1

2

1

2

NR

NR

NR

NR

NR

NR

NR

2

NR

3

NR

NR

NR

NR

NR

NR

NR

2t

NR

2

NR

NR

NR

NR

NR

NR

NR

2

NR

2

NR

NR

NR

NR

NR

NR

NR

2

NR

ND Range.

EFIS Control 22-81-04 6) PanelND Mode Select.

22-81-04 8)

22-82-01

EFIS Control PanelDisplay p.b. Light Bars.

MCDU

MCDU 22-82-01 3) Annunciator Lights 22-83-01

FMGC

FMA Indications on PFD Stabilizer 27-44-01 Actuator Electrical Motors Slat/Flap Control 27-51-01 1) System (SFCS)22-83-02 1)

FLAP Channels

Slat/Flap Control 27-51-01 2) System (SFCS)SLAT Channels

(Continued)


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Page: PBN-4



SUBJECT

Minimum required to Baro V/NAV Minimum required to RNP APPROACH Minimum required to RNP AR 0.1 Minimum Required to RVFP 27-54-02

Flap PCU Valve Blocks

2

NR

NR

NR

NR

NR

NR

NR

2

NR

27-84-02

Slat PCU Valve Blocks

2

NR

NR

NR

NR

NR

NR

NR

2

NR

27-93-01

Elevator Aileron Computers (ELAC)

2

NR

NR

NR

NR

NR

NR

NR

2

NR

27-93-03

ECAM ELAC Indications

2

NR

NR

NR

NR

NR

NR

NR

2

NR

31-63-01

Display Unit (DU)

6

2e

2e

2e

2e

2e

2f

2f

4l

2f

34-10-01

ADIRS

3

2

1

1

2

1

3

3

3p

3

3

NR

NR

NR

NR

NR

NR

NR

3

NR

ADIRS CDU34-10-02 1) Mode Rotary Selectors

NR

NR

NR

NR

NR

NR

NR

1

NR

ADIRS CDU ADR 3 p.b Switch

1

NR

NR

NR

NR

NR

NR

NR

1

NR

ADIRS MSU 34-10-03 1) Mode Rotary selectors

3

NR

NR

NR

NR

NR

NR

NR

3

NR

ADIRS MSU - IR 34-10-03 2) 2 p.b Switch

1

NR

NR

NR

NR

NR

NR

NR

1

NR

1

NR

NR

NR

NR

NR

NR

NR

1

NR

1

NR

NR

NR

NR

NR

NR

NR

1

NR

1

NR

NR

NR

NR

NR

NR

NR

1

NR

34-10-02 12)

ADIRS MSU - IR 3 p.b Switch ADIRS MSU 34-10-03 6) ADR 2 p.b. Switch ADIRS MSU 34-10-03 7) ADR 3 p.b. Switch 34-10-03 3)

1

11)

ADIRS CDU ADR 2 p.b Switch

34-10-02

(Continued)


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Page: PBN-5



SUBJECT

Minimum required to Baro V/NAV Minimum required to RNP APPROACH Minimum required to RNP AR 0.1 Minimum Required to RVFP Vertical SpeedInertial Mode

2

NR

NR

NR

NR

NR

NR

NR

2

NR

34-13-07

Ground Speed indications on ND

2

NR

NR

NR

NR

NR

NR

NR

2

NR

34-13-08

True Airspeed indications on ND

2

NR

NR

NR

NR

NR

NR

NR

2

NR

34-13-09

Wind indications on ND

2

NR

NR

NR

NR

NR

NR

NR

2

NR

34-14-02

EIS Heading indications on ND

4

NR

NR

NR

NR

NR

NR

NR

4

NR

34-40-07

GPWS – G/S pbsw

2

NR

NR

NR

NR

NR

NR

NR

1

NR

34-42-01

Radio Altimeter (RA) Systems

2

NR

NR

NR

NR

NR

NR

NR

2

NR

34-42-02

Automatic Call Out System

1

NR

NR

NR

NR

NR

NR

NR

1

NR 1

34-13-05 1)

34-48-01

GPWS

1

NR

NR

NR

NR

NR

1

1

1q

34-48-02

GPWS FAULT Light

1

NR

NR

NR

NR

NR

NR

NR

1

NR

NR

2g

2h

NR

NR

NR

NR

NR

NR

NR

NR

NR

NR

NR

NR

NR

34-51-01

DME

2

34-55-01

VOR Navigation

2

NR

1k

34-58-01

Global Position System

2

1v

1h

1i

1

1

1

1

2

1

4-61-01

Navigation Databases

2

2l

2l

2l

2l

2l

2l

2l

2l

2i

(Continued


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Page: PBN-6

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX PBN (RNAV-RNP) OPERATIONS The superscript of the minimum required corresponds to the follow notes.

Notes: a. b. c. d. e. f. g. h. i. j. k. l. m. n. o. p. q. r. s. t. u. v.

Refer to RVSM requirements. FCU with both channels. Two (2) FMGC or one (1) FMGC + one (1) BACK UP NAV. Two (2) FM required for RNAV approach (RNP APPROACH). Two NDs (the temporary display on ND information via the PFD/ND switch is permitted on one side. One (1) PFD and one (1) ND (on the PF side) Both (2) DME could be replaced by one (1) GPS or one (1) VOR/DME. Refer to en route requirements. Both (2) DME could be replaced by one (1) GPS. Refer to procedure requirements One (1) GPS or one (1) VOR/DME or two (2) DMEs to update FM position. Refer to en route requirements. One (1) GPS or two (2) DMEs to update FM position. Refer to procedure requirements. One (1) VOR/DME could be replaced by one (1) GPS or two (2) DMEs. Refer to procedure requirements Navigation Databases Update is required. CSTR Display p.b. is required. To RNP-2 route, one Autopilot System or one Flight Director System or one Lateral Navigation is required. Two (2) ND and Two (2) PFD with L/DEV and V/DEV displays. (FD p.b. light bar and CSTR Display p.b. light bar is required.) 2 PFDU and 2 NDU are required. 3 ADIRS in NAV mode are required GPWS, related modes and functions are required. The Performance Information is required. AP1, AP2 and AT/THR p.b. light Bars are required. Stabilizer Actuator Electrical Motors 1 and 2 are required. One (1) GPS if the flight time outside radio navaid coverage is longer than: 6.2H from the time of IRS ground alignment or 5.7H from the time of the last FM position update.

Procedure: When a report is transferred to the DMI list, the following statement must be entered in the aircraft log book: “FLIGHT PLAN MUST BE CONSISTENT WITH AIRCRAFT RNAV-RNP STATUS”. Install the placard with (P/N: RNAV-RNP) PBN OP restriction adjacent to lower ECAM Display, notify restriction(s) to MCC and Operations Dispatch Department for performed penalties. Return to service of aircraft after performing maintenance activities or corrective actions on PBN (RNAV-RNP) systems: The technician responsible for issuing the aircraft release to service, has to record in the aircraft log book the corrective action taken to correct the pilots / maintenance report, or the differed maintenance item DMI (if any) that generated the PBN (RNAV-RNP) operation restriction. Additionally to the corrective action, the following statement has to be entered in the airplane log book (in accordance with the aircraft PBN capability): “ACCOMPLISHED MAINTENANCE MAKES THIS AIRCRAFT COMPLIANT WITH ALL RNAV-RNP REQUIREMENTS” (Continued) Revision: 34 May 26, 2016

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Page: PBN-7

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX PBN (RNAV-RNP) OPERATIONS Placard P/N RNAV-RNP must be removed from Captains Instrument Panel. The person who gives the release has to inform MCC that the PBN (RNAV-RNP) limitations for this aircraft have been removed. Nomenclature: -

NR = Non Required RNAV 10 (RNP 10) RNAV 5 (BRNAV) RNAV 1 (PRNAV)


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Page: PBN-8

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS GENERAL Before entering in the MEL, troubleshooting actions should have already been conducted in order to determine and confirm which equipment, component, system or function is inoperative. The objective of the present Section is only to help the airline identify the corresponding MEL ENTRY point (If applicable) when a caution/warning has been displayed on ECAM E/WD. The present Section does not substitute troubleshooting actions. The following pages give correspondence between ECAM caution/warning messages and MEL item number. CAUTION 1. This section is, normally, not intended to cover false cautions/warnings. However, if a caution/warning is determined to be false by troubleshooting , the crew should refer to the concerned caution/warning message item (if listed) in the associated ATA chapter. 2. In order to help the crew to determine the MEL ENTRY point corresponding to a caution/warning message, the REMARK column contains the text : a) "Actual warning" or "Actual caution". The associated MEL item number is the MEL ENTRY point which gives the dispatch conditions corresponding to an actual failure of the system/component monitored by the caution/warning. b) "False warning" or "False caution". The associated MEL item number is the MEL ENTRY point which gives the dispatch conditions corresponding to the failure of the warning, determined by troubleshooting. The system/component monitored by the caution/warning being still operative 3. When the REMARK column contains neither, "Actual caution/warning", nor "False caution/warning" texts, the MEL ENTRY point corresponds to an actual warning which indicates an actual failure of the system/component monitored by the caution/warning. 4. When either an actual, or a false caution/warning is activated, this section gives the MEL ENTRY point to be considered. But the crew MUST CHECK THAT THE AIRCRAFT SYSTEMS/COMPONENTS ARE IN A CONDITION WHICH COMPLIES WITH THE DISPATCH CONDITIONS. IF NOT AIRCRAFT DISPATCH IS NOT ALLOWED. 5. When a caution/warning is associated with the wording "Not applicable" in the Dispatch Condition column, this means that the MEL is not the appropriate document to be consulted. When such cautions/warnings have been triggered, application of associated procedure, if any (refer to FCOM Vol 3 Abnormal/Emergency procedures), and/or accomplishment of maintenance action, if required, would permit to fix the problem.


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Page: ECAM-1

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS GENERAL EXAMPLES 1) If the "BAT FAULT" caution message is displayed on ECAM, the crew must refer to the MEL 24-30-02 (Battery channel). 2) If the "AC BUS 1 FAULT" caution message is displayed on ECAM, A/C dispatch is not allowed. 3) If the "GEN 1 OFF" caution message is displayed on ECAM no MEL entry is required, and the text "Not applicable" is written in the Remark column. In this example, the crew must switch on the GEN pb sw. 4) If "PACK 1 +2 FAULT" caution message is displayed the crew must refer to FCOM for "FLIGHT WITHOUT PRESSURIZATION". Note: The ECAM warnings and cautions listed in APPENDIX ECAM WARNINGS are generic. example : ECAM WARNING

DISPATCH CONDITION

FCU 1(2) (1+2) FAULT

Refer to MEL 22-81-01

REMARK

Wording FCU 1(2) (1+2) FAULT represents the three messages : "FCU 1 FAULT" "FCU 2 FAULT" "FCU 1+2 FAULT"


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Page: ECAM-2

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS ATA 21 AIR CONDITIONING ECAM WARNING AIR AFT CRG VENT FAULT(If Installed) AIR COND CTL 1(2)-A(B) AIR FWD CRG VENT FAULT (If Installed) AIR PACK 1(2) FAULT AIR PACK 1+2 FAULT AIR PACK 1(2) FLOW REDUCED AIR PACK 1(2) OFF AIR PACK 1(2) OVHT

DISPATCH CONDITION Refer to MEL 21-28-04 Refer to MEL 21-63-06 Refer to MEL 21-28-01 Refer to MEL 21-52-01 Refer to MEL 21-52-01 Apply ECAM procedure. Refer to MEL 21-52-01 Refer to MEL 21-52-01 Refer to MEL 21-52-01 Refer to MEL 21-61-01

AIR PACK 1(2) REGUL FAULT Refer to MEL 21-61-02 Refer to MEL 21-63-05 Refer to MEL 21-63-05 AIR PACK 1(2) REGUL FAULT

CAB PR EXCESS CAB ALT CAB PR EXCES RESIDUAL PR CAB PR LDG ELEV FAULT CAB PR LO DIFF PR CAB PR OFV NOT OPEN CAB PR SAFETY VALVE OPEN CAB PR SYS 1(2) FAULT CAB PR SYS 1+2 FAULT COND AFT CAB DUCT OVHT (If Installed) COND AFT CRG ISOL VALVE (If Installed) COND CKPT DUCT OVHT COND FWD CAB DUCT OVHT COND FWD CRG ISOL VALVE (If Installed) COND HOT AIR FAULT COND L+R CAB FAN FAULT COND LAV+GALLEY FAN FAULT

Refer to MEL 21-51-06 Refer to MEL 21-52-01 Refer to MEL 21-52-02 Refer to MEL 21-61-02 Not related to MEL Apply ECAM procedure Refer to MEL 21-31-05 Not related to MEL NO DISPATCH Refer to FCOM/PRO-SPO-20FLIGHT WITHOUT CABIN PRESSURIZATION Refer to Item 21-31-08 Refer to Item 21-31-01 Refer to FCOM/PRO-SPO 20 Flight Without Cabin Pressurization Refer to Item 21-63-02

If pack ram air inlet flap is affected If pack controller, pack anti–ice valve or water exchanger temperature sensor are affected If turbine bypass valve is affected If pack outlet temperature is affected If pack compressor outlet temperature is affected If pack flow sensor is affected If pack flow control valve is affected If pack ram air inlet is affected If turbine bypass valve is affected

Actual alert False alert

Refer to Item 21-28-05 Refer to Item 21-63-02 Refer to Item 21-63-02 Refer to Item 21-28-02 Refer to Item 21-63-03 NO DISPATCH Refer to Item 21-23-01 Refer to Item 21-63-02 Refer to Item 21-63-02 Refer to Item 21-63-02

COND TRIM AIR SYS FAULT Refer to Item 21-63-02 Refer to Item 21-63-02


REMARK

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If the trim air valves are closed If associated with the AFT CAB TRIM VALVE subtitle If associated with the FWD CAB TRIM VALVE subtitle If associated with the CKPT TRIM VALVE subtitle If associated with the TRIM AIR HI PR subtitle

Page: ECAM-3

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS ATA 21 AIR CONDITIONING ECAM WARNING

DISPATCH CONDITION Refer to Item 21-26-04

Refer to Item 21-26-05 VENT AVNCS SYS FAULT

VENT BLOWER FAULT VENT EXTRACT FAULT

VENT SKIN VALVE FAULT


Refer to Item 21-26-03 or Refer to Item 21-26-07 or Refer to Item 21-26-08 or Refer to Item 21-26-06 or Refer to Item 21-26-10 Refer to Item 21-26-01 Refer to Item 21-26-11 Refer to Item 21-26-02 Refer to Item 21-26-12 Refer to Item 21-26-04 Refer to Item 21-26-04

N Registration

REMARK If the VENT SKIN VALVE FAULT alert is displayed on the EWD due to the Avionics Skin Air Outlet valve. If the VENT SKIN VALVE FAULT alert is displayed on the EWD due to the Avionics Skin Air Inlet valve.

Actual alert False alert Actual alert False alert Outlet valve determined faulty on the CAB PRESS SD page Inlet valve determined faulty on the CAB PRESS SD page

Page: ECAM-4

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS ATA 22 AUTO FLIGHT ECAM WARNING AUTO FLT A/THR LIMITED AUTO FLT A/THR OFF AUTO FLT AP OFF AUTO FLT FAC 2 FAULT AUTO FLT FAC 1+2 FAULT AUTO FLT FCU 1(2) FAULT AUTO FLT FCU 1+2 FAULT AUTO FLT REAC W/S DET FAULT (If Installed) AUTO FLT RUD TRIM 1(2) FAULT AUTO FLT RUD TRIM SYS AUTO FLT RUD TRV LIM 1(2) AUTO FLT RUD TRV LIM SYS AUTO FLT TCAS MODE FAULT AUTO FLT YAW DAMPER 1(2) AUTO FLT YAW DAMPER SYS T.O SPEEDS NOT INSERTED T.O SPEEDS TOO LOW T.O V1/VR/V2 DISAGREE


DISPATCH CONDITION Not related to MEL Refer to MEL 22-30-01 Refer to MEL 22-10-01 Refer to MEL 22-10-05 Refer to MEL 22-10-05 NO DISPATCH Refer to MEL 22-81-01 NO DISPATCH Refer to MEL 22-66-03

REMARK


Refer to MEL 27-22-01 NO DISPATCH Refer to MEL 27-23-01 NO DISPATCH Refer to MEL 22-10-08 Refer to MEL 22-63-01 NO DISPATCH Not related to MEL Not related to MEL Not related to MEL

N Registration

Page: ECAM-5

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS ATA 23 COMMUNICATIONS ECAM WARNING COM ACARS FAULT (If Installed) COM CIDS 1+2 FAULT COM HF 1(2) DATA FAULT (If Installed)

DISPATCH CONDITION

Refer to MEL 23-51-05 COM HF 1(2) EMITTING (If Installed)

Refer to MEL 23-51-08 Refer to MEL 23-51-02

COM SATCOM DATA FAULT (If Installed) COM SATCOM FAULT (If Installed)

COM SINGLE PTT STUCK

Refer to MEL 23-28-01 Refer to MEL 23-51-05 Refer to MEL 23-51-08



If hand microphone PTT pb is jammed in the transmitting position If sidestick PTT pb is jammed in the transmitting position If a transmission Key on one ACP is jammed in the transmitting position


COM VHF 1(2)(3) EMITTING



Refer to MEL 23-51-02 COM VHF 3 DATA FAULT (If Installed)

REMARK

Refer to MEL 46-21-01 NO DISPATCH Refer to MEL 23-11-01

N Registration


Page: ECAM-6

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS ATA 24 ELECTRICAL POWER ECAM WARNING ECAM Alert C/B TRIPPED ELEC AC BUS 1 FAULT ELEC AC BUS 2 FAULT ELEC AC ESS BUS ALTN ELEC AC ESS BUS FAULT ELEC AC ESS BUS SHED ELEC APU GEN FAULT ELEC APU GEN OVERLOAD ELEC BAT 1(2) FAULT ELEC BAT 1(2) OFF ELEC DC BAT BUS FAULT ELEC DC BUS 1 FAULT ELEC DC BUS 2 FAULT ELEC DC BUS 1+2 FAULT ELEC DC EMER CONFIG ELEC DC ESS BUS FAULT ELEC DC ESS BUS SHED ELEC EMER CONFIG ELEC EMER GEN 1 LINE OFF ELEC ESS BUSSES ON BAT ELEC GEN 1(2) FAULT ELEC GEN 1(2) OFF ELEC GEN 1(2) OVERLOAD ELEC IDG 1(2) DISCONNECTED ELEC IDG 1(2) OIL LO PR ELEC IDG 1(2) OIL OVHT ELEC STATIC INV FAULT ELEC TR 1(2) FAULT


DISPATCH CONDITION CONDITION OF DISPATCH Refer to affected system Refer to MEL 24-50-01 NO DISPATCH NO DISPATCH NO DISPATCH NO DISPATCH NO DISPATCH Refer to MEL 24-20-02 Refer to MEL 24-56-01 NO DISPATCH Not related to MEL NO DISPATCH NO DISPATCH NO DISPATCH NO DISPATCH NO DISPATCH NO DISPATCH NO DISPATCH NO DISPATCH Not related to MEL NO DISPATCH Refer to MEL 24-22-01 Not related to MEL Refer to MEL 24-56-01 Refer to MEL 24-20-01 Refer to MEL 24-20-01 Refer to MEL 24-20-01 NO DISPATCH Refer to MEL 24-30-01

N Registration

REMARK AIRCRAFT STATUS Actual alert False alert

Actual alert

Page: ECAM-7

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS ATA 26 FIRE PROTECTION ECAM WARNING APU FIRE APU FIRE DET FAULT APU FIRE LOOP A(B) FAULT AVIONICS SMOKE CARGO SMOKE AFT BTL SQUIB FAULT (If Installed) CARGO SMOKE FWD BTL SQUIB FAULT (If Installed) ENG 1(2) FIRE ENG 1(2) FIRE DET FAULT ENG 1(2) FIRE LOOP A FAULT ENG 1(2) FIRE LOOP B FAULT SMOKE AFT CARGO SMOKE

SMOKE AFT CRG BTL FAULT

SMOKE AFT CRG DET FAULT SMOKE FWD CARGO SMOKE

SMOKE FWD CRG BTL FAULT

SMOKE FWD CRG DET FAULT SMOKE DET FAULT SMOKE LAVATORY DET FAULT SMOKE LAVATORY SMOKE


DISPATCH CONDITION NO DISPATCH Refer to MEL 49-10-01 Refer to MEL 26-13-01 Refer to MEL 26-13-01 NO DISPATCH Refer to MEL 26-15-01 Refer to MEL 26-23-02

REMARK Actual alert False alert Actual alert False alert

Refer to MEL 26-23-02 NO DISPATCH NO DISPATCH Refer to MEL 26-12-01 Refer to MEL 26-12-01 Refer to MEL 26-12-01 Refer to MEL 26-12-01 NO DISPATCH Refer to MEL 26-23-01 Refer to MEL 26-23-01 Refer to MEL 26-16-02 NO DISPATCH Refer to MEL 26-23-01 Refer to MEL 26-23-01 Refer to MEL 26-16-03 Refer to MEL 26-17-02 or Refer to MEL 23-73-01 Refer to MEL 26-17-01 NO DISPATCH Refer to MEL 26-17-01

N Registration

If engine 1 is affected If engine 2 is affected If engine 1 is affected If engine 2 is affected If the SMOKE FWD CRG BTL FAULT alert is not displayed on the EWD If the SMOKE FWD CRG BTL FAULT alert is displayed on the EWD If the SMOKE AFT CRG BTL FAULT alert is not displayed on the EWD If the SMOKE AFT CRG BTL FAULT alert is displayed on the EWD


Page: ECAM-8

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS ATA 27 FLIGHT CONTROLS ECAM WARNING CONFIG L(R) SIDESTICK FAULT CONFIG PITCH TRIM NOT IN T.O. RANGE CONFIG RUD TRIM NOT IN T.O. RANGE CONFIG SLATS(FLAPS) NOT IN T.O. CONFIG CONFIG SPEED BRK NOT RETRACTED F/CTL AIL SERVO FAULT F/CTL ALTN LAW F/CTL DIRECT LAW F/CTL ELAC 1 FAULT F/CTL ELAC 1 PITCH FAULT F/CTL ELAC 2 FAULT F/CTL ELAC 2 PITCH FAULT F/CTL ELEV SERVO FAULT F/CTL FCDC 1 FAULT F/CTL FCDC 2 FAULT F/CTL FCDC 1+2 FAULT F/CTL FLAP ATTACH SENSOR F/CTL FLAP LVR NOT ZERO

DISPATCH CONDITION

NO DISPATCH NO DISPATCH NO DISPATCH Refer to MEL 26-14-01 NO DISPATCH NO DISPATCH Refer to MEL 27-93-01 Refer to MEL 27-93-01 NO DISPATCH NO DISPATCH NO DISPATCH Refer to MEL 27-93-01 NO DISPATCH Refer to MEL 27-95-02 NO DISPATCH NO DISPATCH Not related to MEL NO DISPATCH Refer to MEL 27-54-01

F/CTL FLAP SYS 1 FAULT

Refer to MEL 27-51-01 Refer to MEL 27-54-01 F/CTL FLAP SYS 2 FAULT

F/CTL FLAP TIP BRK FAULT F/CTL FLAPS(SLATS) FAULT F/CTL FLAPS(SLATS) LOCKED F/CTL GND SPLR FAULT F/CTL GND SPLR 1+2(3+4) FAULT F/CTL GND SPLR 5 FAULT

Refer to MEL 27-51-01 NO DISPATCH NO DISPATCH Refer to MEL 32-42-05 Refer to MEL 27-92-02 Refer to MEL 27-92-02 Refer to MEL 27-92-02 Not related to MEL

F/CTL GND SPLR NOT ARMED F/CTL L(R) AIL FAULT F/CTL L(R) ELEV FAULT F/CTL L+R ELEV FAULT F/CTL L(R) SIDESTICK FAULT F/CTL PITCH TRIM/MCDU/CG DISAGREE


REMARK

NO DISPATCH NO DISPATCH

If the servo-control is affected If the servo-control position transducer is affected.

If the maintenance check confirms that the F/CTL FLAP SYS 1 FAULT alert is displayed on the EWD due to a flap motor failure If the maintenance check confirms that the F/CTL FLAP SYS 2 FAULT alert is displayed on the EWD due to a flap motor failure.

If the braking system is affected If the braking system is not affected

Ground spoilers are not armed while on approach below 500 ft (150 m) AGL with the landing gears down.

NO DISPATCH NO DISPATCH NO DISPATCH NO DISPATCH Not related to MEL

N Registration

Page: ECAM-9

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS ATA 27 FLIGHT CONTROLS ECAM WARNING F/CTL SEC 1 FAULT F/CTL SEC 2 FAULT F/CTL SEC 3 FAULT F/CTL SIDESTICK PRIORITY F/CTL SLAT SYS 1 FAULT

DISPATCH CONDITION Refer to MEL 27-94-01 Refer to MEL 27-94-01 Refer to MEL 27-94-01 Refer to FCOM/PRO-ABN-27 F/CTL SIDESTICK PRIORITY NO DISPATCH Refer to MEL 27-84-01 Refer to MEL 27-81-01 Refer to MEL 27-84-01

F/CTL SLAT SYS 2 FAULT

F/CTL SLAT TIP BRK FAULT F/CTL SPD BRK DISAGREE F/CTL SPD BRK FAULT F/CTL SPD BRK STILL OUT F/CTL SPD BRK 2(3+4) FAULT F/CTL SPLR FAULT F/CTL STABILIZER JAM


REMARK

If the maintenance check confirms the F/CTL SLAT SYS 2 FAULT alert is displayed on the EWD due to a slat motor failure.

Refer to MEL 27-81-01 Refer to MEL 27-92-01 Refer to MEL 27-92-01 Not related to MEL Refer to MEL 27-92-01 Refer to MEL 27-92-02 or Refer to MEL 27-64-01 NO DISPATCH

N Registration

Page: ECAM-10

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS ATA 28 FUEL ECAM WARNING FUEL ACT PUMP LO PR FUEL ACT UNUSABLE

FUEL ACT XFR FAULT

FUEL APU LP VALVE FAULT FUEL AUTO FEED FAULT FUEL AUTO TRANSFER FAULT FUEL CTR L(R) XFR FAULT FUEL CTR L+R XFR FAULT FUEL CTR TK PUMP 1(2) LO PR FUEL CTR TK PUMPS LO PR FUEL CTR TK PUMPS OFF FUEL CTR TK XFR OFF FUEL ENG 1(2) LP VALVE OPEN FUEL FQI CH 1(2) FAULT FUEL F.USED/FOB DISAGREE FUEL IDG 1(2) COOL FAULT FUEL LO LVL DET FAULT FUEL L(R) INNER(OUTER) TK HI TEMP FUEL L(R) INNER(OUTER) TK HI TEMP FUEL L(R) WING TK HI TEMP FUEL L(R) WING TK HI TEMP FUEL L(R) INNER(OUTER) TK LO TEMP FUEL L(R) WING TK LO TEMP FUEL L(R) OUTER XFR CLOSED FUEL L(R) OUTER XFR OPEN FUEL L(R) TK PUMP 1(2) LO PR FUEL L(R) TK PUMP 1+2 LO PR FUEL L(R) WING TK LO LVL FUEL L+R WING TK LO LVL FUEL L(R) WING TK OVERFLOW FUEL X FEED VALVE FAULT


DISPATCH CONDITION Refer to MEL 28-28-03 Not related to MEL Refer to MEL 28-12-01 or Refer to MEL 28-25-03 or Refer to MEL 28-28-01 or Refer to MEL 28-28-02 or Refer to MEL 28-28-04 or Refer to MEL 28-28-05 or Refer to MEL 28-40-01 Refer to MEL 28-40-09 Refer to MEL 49-30-02 Refer to MEL 28-20-01 Refer to MEL 28-21-02 Refer to MEL 28-21-02 Refer to MEL 28-21-02 Refer to MEL 28-21-02 Refer to MEL 28-21-02 Not related to MEL Not related to MEL NO DISPATCH Refer to MEL 28-40-06 Refer to MEL 28-40-02 Not related to MEL Refer to MEL 23-73-01 NO DISPATCH Dispatch possible only if “delay T.O” is not displayed on ECAM Refer to MEL 28-40-09 NO DISPATCH Refer to MEL 28-40-09 Dispatch possible only if “delay T.O” is not displayed on ECAM Refer to MEL 28-40-09 NO DISPATCH Refer to MEL 28-40-09 NO DISPATCH Refer to MEL 28-40-09 NO DISPATCH Refer to MEL 28-40-09 Refer to MEL 28-15-01 Refer to MEL 28-15-01 Refer to MEL 28-21-01 NO DISPATCH NO DISPATCH Refer to MEL 28-40-01 NO DISPATCH NO DISPATCH NO DISPATCH

N Registration

REMARK

False alert


Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert


Page: ECAM-11

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS ATA 29 HYDRAULICS ECAM WARNING HYD B ELEC PUMP LO PR HYD B ELEC PUMP OVHT HYD B RSVR LO AIR PR HYD B RSVR LO LVL HYD B RSVR OVHT HYD B SYS LO PR HYD B+G SYS LO PR HYD B+Y SYS LO PR HYD G ENG 1 PUMP LO PR HYD G RSVR LO AIR PR HYD G RSVR LO LVL HYD G RSVR OVHT HYD G SYS LO PR HYD G+Y SYS LO PR HYD PTU FAULT HYD RAT FAULT HYD Y ELEC PUMP LO PR HYD Y ELEC PUMP OVHT HYD Y ENG 2 PUMP LO PR HYD Y RSVR LO AIR PR HYD Y RSVR LO LVL HYD Y RSVR OVHT HYD Y SYS LO PR


DISPATCH CONDITION NO DISPATCH Refer to MEL 29-30-04 NO DISPATCH Refer to MEL 29-30-04 NO DISPATCH Refer to MEL 29-30-04 NO DISPATCH Refer to MEL 29-30-04 NO DISPATCH NO DISPATCH Refer to MEL 29-30-04 NO DISPATCH Refer to MEL 29-30-04 NO DISPATCH Refer to MEL 29-30-04 NO DISPATCH Refer to MEL 29-30-04 NO DISPATCH Refer to MEL 29-30-04 NO DISPATCH Refer to MEL 29-30-04 NO DISPATCH Refer to MEL 29-30-04 NO DISPATCH Refer to MEL 29-30-04 NO DISPATCH Refer to MEL 29-30-04 NO DISPATCH Refer to MEL 29-30-04 NO DISPATCH Refer to MEL 29-30-04 Refer to MEL 29-24-01 Refer to MEL 29-30-04 Refer to MEL 29-24-01 Refer to MEL 29-30-04 NO DISPATCH Refer to MEL 29-30-04 NO DISPATCH Refer to MEL 29-30-04 NO DISPATCH Refer to MEL 29-30-04 NO DISPATCH Refer to MEL 29-30-04 NO DISPATCH Refer to MEL 29-30-04

N Registration

REMARK Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert

Page: ECAM-12

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS ATA 30 ICE AND RAIN PROTECTION ECAM WARNING ANTI ICE ALL PITOT ANTI ICE CAPT(F/O)(STBY) AOA ANTI ICE CAPT(F/O)(STBY) L(R) STAT ANTI ICE CAPT(F/O)(STBY) PITOT ANTI ICE CAPT+F/O PITOT ANTI ICE CAPT+STBY PITOT ANTI ICE CAPT(F/O)(STBY) PROBES ANTI ICE CAPT(F/O) TAT ANTI ICE DETECT FAULT

ANTI ICE ENG 1(2) CTL FAULT

ANTI ICE ENG 1(2) OVER PRESS ANTI ICE ENG 1(2) VALVE CLSD ANTI ICE ENG 1(2) VALVE OPEN ANTI ICE F/O+STBY PITOT ANTI ICE ICE DETECTED

DISPATCH CONDITION

Refer to MEL 30-31-02 NO DISPATCH NO DISPATCH Refer to MEL 30-31-01 Refer to MEL 30-31-01 Refer to MEL 30-81-02 Refer to MEL 30-21-03 Refer to MEL 30-21-03 NO DISPATCH Refer to MEL 30-21-01 Refer to MEL 30-21-01 NO DISPATCH Not related to MEL Refer to MEL 30-42-01

ANTI ICE L(R) WINDOW Refer to MEL 30-42-02 Refer to MEL 30-42-01 ANTI ICE L(R) WINDSHIELD ANTI ICE L+R WINDSHIELD SEVERE ICE DETECTED WING ANTI ICE L(R) HI PR WING ANTI ICE L(R) VALVE OPEN WING ANTI ICE OPEN ON GND WING ANTI ICE SYS FAULT


REMARK

NO DISPATCH Refer to MEL 30-31-04 Refer to MEL 30-31-03

If the ENG 1(2) A.ICE VALVE OPEN subtitle is displayed on the EWD: If the ENG 1(2) A.ICE MON FAULT subtitle is displayed on the EWD:

If the Window Heat Computer is affected If the Window Heat Computer is affected

Refer to MEL 30-42-03 NO DISPATCH Not related to MEL Refer to MEL 30-11-01 Refer to MEL 30-11-01 Refer to MEL 30-11-01 Refer to MEL 30-11-01

N Registration

Page: ECAM-13

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS ATA 31 INDICATING/RECORDING SYSTEM ECAM WARNING EIS DMC 1 FAULT EIS DMC 2 FAULT EIS DMC 3 FAULT EIS DMC/FWC COM FAULT FWS FWC 1 FAULT FWS FWC 2 FAULT FWS FWC 1+2 FAULT FWS OEB/FWC DISCREPANCY FWS SDAC 1 FAULT FWS SDAC 2 FAULT FWS SDAC 1+2 FAULT RECORDER DFDR FAULT RECORDER SYS FAULT


DISPATCH CONDITION

REMARK

Refer to MEL 31-63-02 Refer to MEL 31-63-02 Refer to MEL 31-63-02 NO DISPATCH NO DISPATCH Refer to MEL 31-53-01 NO DISPATCH NO DISPATCH NO DISPATCH Refer to MEL 31-55-01 NO DISPATCH Refer to MEL 31-30-02 Refer to MEL 31-30-03

N Registration

Page: ECAM-14

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS ATA 32 LANDING GEAR ECAM WARNING BRAKES ALTN BRK FAULT BRAKES ALTN L(R) RELEASED BRAKES A/SKID N/WS FAULT BRAKES A/SKID N/WS OFF

DISPATCH CONDITION NO DISPATCH NO DISPATCH NO DISPATCH Not related to MEL NO DISPATCH Refer to MEL 32-42-04

BRAKES AUTO BRK FAULT Refer to MEL 32-42-05 BRAKES AUTO BRK FAULT BRAKES BRK Y ACCU LO PR BRAKES SYS 1 FAULT BRAKES SYS 2 FAULT BRAKES HOT BRAKES NORM BRK FAULT BRAKES NORM+ALT FAULT

Refer to MEL 32-42-04 NO DISPATCH Refer to MEL 32-42-02 Refer to MEL 32-42-03 Refer to MEL 32-42-03 NO DISPATCH Refer to MEL 32-42-02 NO DISPATCH NO DISPATCH NO DISPATCH

BRAKES PARK BRK FAULT Apply ECAM procedure BRAKES PARK BRK LO PR BRAKES PARK BRK ON BRAKES RELEASED BRAKES-N/WS MINOR FAULT CONFIG PARK BRK ON L/G DOORS NOT CLOSED L/G GEAR NOT DOWN L/G GEAR NOT DOWNLOCKED L/G GEAR NOT UPLOCKED L/G GEAR UPLOCK FAULT L/G LGCIU 1 FAULT L/G LGCIU 2 FAULT L/G LGCIU 1+2 FAULT L/G SHOCK ABSORBER FAULT L/G SYS DISAGREE WHEEL HYD SEL FAULT

Not related to MEL Not related to MEL Refer to MEL 32-42-02 Refer to MEL 32-42-05 Refer to MEL 32-09-04 NO DISPATCH NO DISPATCH Not related to MEL Not related to MEL Not related to MEL Refer to MEL 32-31-00 NO DISPATCH Refer to MEL 32-31-01 NO DISPATCH NO DISPATCH NO DISPATCH NO DISPATCH Refer to MEL 32-51-03

WHEEL N/W STRG FAULT WHEEL TYRE LO PR


Refer to MEL 32-51-01 NO DISPATCH Refer to MEL 32-49-03

N Registration

REMARK

If normal braking is lost (BRAKE RELEASED message is not displayed) If the autobrake function is affected (BRAKE RELEASED message is displayed) If a tachometer is affected (BRAKE RELEASED message is displayed) Actual alert False alert


If associated with the BRK PRESS STILL APPLIED subtitle If associated with the BRK PRESS RELEASED subtitle

If green brake supply affected If a tachometer is affected

If the LGCIU 2 is inoperative

If the NWS electrical deactivation box is failed In the other cases Actual alert False alert

Page: ECAM-15

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS ATA 34 NAVIGATION ECAM WARNING NAV ADR DISAGREE NAV ADR 2 FAULT NAV ADR 3 FAULT NAV ADR 1+2(1+3)(2+3) FAULT NAV ADR 1+2+3 FAULT NAV ALTI DISCREPANCY NAV ATC/XPDR 1(2)(1+2) FAULT NAV ATC/XPDR STBY NAV ATT DISCREPANCY NAV BARO REF DISCREPANCY NAV L(R) CAPT(F/O) STATIC FAULT NAV FM/GPS POS DISAGREE NAV GPS 1(2) FAULT NAV GPWS FAULT NAV GPWS TERR DET FAULT NAV HDG DISCREPANCY NAV IAS DISCREPANCY NAV ILS 1(2)(1+2) FAULT NAV IR DISAGREE NAV IR NOT ALIGNED NAV IR 1 FAULT NAV IR 2 FAULT NAV IR 3 FAULT NAV IR 1+2(1+3)(2+3) FAULT NAV LS TUNING DISAGREE NAV PRED W/S DET FAULT

DISPATCH CONDITION

NAV RA DEGRADED

Not related to MEL Refer to MEL 34-58-01 Refer to MEL 34-48-01 Refer to MEL 34-48-01 Refer to MEL 34-10-01 Refer to MEL 34-10-01 Refer to MEL 34-30-04 NO DISPATCH Refer to MEL 34-10-01 Refer to MEL 34-10-01 Refer to MEL 34-10-01 Refer to MEL 34-10-01 NO DISPATCH Not related to MEL Refer to MEL 34-52-03 or Refer to MEL 34-41-01 Refer to MEL 34-42-01

NAV RA 1(2) FAULT NAV TCAS FAULT NAV TCAS STANDBY OVERSPEED SURV ROW/ROP LOST

Refer to MEL 34-42-01 Refer to MEL 34-43-01 Not related to MEL Not related to MEL Refer to MEL 34-40-09


REMARK

NO DISPATCH Refer to MEL 34-10-02 Refer to MEL 34-10-02 NO DISPATCH NO DISPATCH Refer to MEL 34-10-02 Refer to MEL 34-52-01 Not related to MEL Refer to MEL 34-10-01 Not related to MEL NO DISPATCH

N Registration

During the previous flight, both RA s disagreed. If the RA 1(2) is confirmed faulty by troubleshooting, the radio altimeter 1(2) must be considered inoperative.

Page: ECAM-16

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS ATA 36 PNEUMATIC ECAM WARNING AIR APU BLEED FAULT AIR APU BLEED LEAK AIR APU LEAK DET FAULT AIR BLEED 1(2) OFF AIR BLEED LEAK AIR ENG HP VALVE FAULT AIR ENG 1(2) BLEED ABNORM PR AIR ENG 1(2) BLEED FAULT AIR ENG 1(2) BLEED FAULT AIR ENG 1(2) BLEED HI TEMP AIR ENG 1(2) BLEED LEAK AIR ENG 1(2)(1+2) BLEED LO TEMP AIR ENG 1(2) BLEED NOT CLSD AIR ENG 1(2) LEAK DET FAULT AIR ENG 1(2) LEAK DET FAULT AIR ENG 1+2 BLEED FAULT AIR L(R) WING LEAK AIR L(R) WNG LEAK DET FAULT

DISPATCH CONDITION Refer to MEL 36-12-02 NO DISPATCH Refer to MEL 36-22-17 Refer to MEL 36-11-01 NO DISPATCH Refer to MEL 36-11-07 Refer to MEL 36-11-01 Refer to MEL 36-11-01 Refer to MEL 36-11-01 Refer to MEL 36-11-02 Apply ECAM procedure NO DISPATCH Refer to MEL 36-22-15 Refer to MEL 36-11-04 Refer to MEL 36-11-02 Refer to MEL 36-22-01 NO DISPATCH NO DISPATCH NO DISPATCH NO DISPATCH Refer to MEL 36-12-04

AIR X BLEED FAULT Refer to MEL 36-12-04 BLEED MONITORING FAULT BLEED MONIT SYS 1(2) FAULT


REMARK

If the associated BLEED NOT CLOSED subtitle is displayed Actual alert False alert

For NEO Aircraft Only For NEO Aircraft Only

If the automatic control of the crossbleed valve is affected If the manual control of the crossbleed valve is affected

NO DISPATCH Refer to MEL 36-11-08

N Registration

Page: ECAM-17

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS ATA 46 INFORMATION SYSTEMS ECAM WARNING DATA LINK ATC FAULT (If Installed) DATA LINK ATSU FAULT DATA LINK COMPANY FAULT


DISPATCH CONDITION

REMARK

Refer to MEL 46-21-01 Refer to MEL 46-21-01 Refer to MEL 46-21-01

N Registration

Page: ECAM-18

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS ATA 47 INERT GAS SYSTEM ECAM WARNING FUEL INERTING SYS FAULT


DISPATCH CONDITION

REMARK


N Registration

Page: ECAM-19

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS ATA 49 AIRBORNE AUXILIARY POWER UNIT ECAM WARNING APU AUTO(EMER) SHUT DOWN


DISPATCH CONDITION

REMARK


N Registration

Page: ECAM-20

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS ATA 52 DOORS ECAM WARNING DOOR AFT(BULK)(FWD) CARGO DOOR L(R) AFT AVIONICS DOOR L(R) AFT CABIN DOOR L(R) AFT EMER EXIT DOOR L(R) EMER EXIT DOOR L(R) FWD AVIONICS DOOR L(R) FWD CABIN DOOR L(R) FWD EMER EXIT


DISPATCH CONDITION NO DISPATCH Refer to MEL 52-70-01 NO DISPATCH Refer to MEL 52-70-01 NO DISPATCH Refer to MEL 52-70-01 NO DISPATCH Refer to MEL 52-70-01 NO DISPATCH Refer to MEL 52-70-01 NO DISPATCH Refer to MEL 52-70-01 NO DISPATCH Refer to MEL 52-70-01 NO DISPATCH Refer to MEL 52-70-01

N Registration

REMARK Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert Actual alert False alert

Page: ECAM-21

Avianca AIRBUS A318/A319/A320/A321 MINIMUM EQUIPMENT LIST APPENDIX ECAM WARNINGS ATA 70 ENGINE ECAM WARNING

DISPATCH CONDITION

ENG ALL ENGINES FAILURE ENG COMPRESSOR VANE ENG DUAL FAILURE ENG THR LEVERS NOT SET ENG REV SET ENG SAT ABOVE FLEX TEMP ENG THRUST LOCKED ENG TYPE DISAGREE ENG VIB SYS FAULT ENG 1(2) A/C FADEC SUPPLY ENG 1(2) AIR EXCHANGR FAULT ENG 1(2) BEARING 4 OIL SYS ENG 1(2) BEARING 4 OIL SYS ENG 1(2) BLEED STATUS FAULT

Not related to MEL NO DISPATCH Not related to MEL Refer to MEL 73-20-01 Not related to MEL Apply ECAM procedure Not related to MEL NO DISPATCH Refer to MEL 77-00-02 Refer to MEL 73-20-09 NO DISPATCH NO DISPATCH Refer to MEL 79-23-01 Apply ECAM procedure

ENG 1(2) COMPRESSOR VANE ENG 1+2 COMPRESSOR VANE ENG 1(2) CTL SYS FAULT ENG 1(2) CTL VALVE FAULT ENG 1(2) EGT(FF)(N1)(N2) DISCREPANCY ENG 1(2) EGT(EPR)(FF)(N1)(N2) DISCREPANCY ENG 1(2) EGT EXCEEDED DURING AIR START ENG 1(2) EIU FAULT ENG 1(2) EPR MODE FAULT ENG 1(2) FADEC A(B) FAULT ENG 1(2) FADEC ALTERNATOR ENG 1(2) FADEC BLOWER FAULT ENG 1(2) FADEC FAULT ENG 1(2) FADEC HI TEMP ENG 1(2) FADEC OVHT ENG 1(2) FADEC IDENT FAULT ENG 1(2) FADEC PLUG FAULT ENG 1(2) FADEC SYS FAULT ENG 1(2) FAIL

NO DISPATCH NO DISPATCH NO DISPATCH NO DISPATCH NO DISPATCH

ENG 1(2) FAN COWL NOT CLSD ENG 1(2) FUEL CTL FAULT ENG 1(2) FUEL FILTER CLOG ENG 1+2 FUEL FILTER CLOG


REMARK

AIR VALVE CLOSED HI PRESS SCAVENGE VALVE FAULT If this alert is displayed on the EWD before the first engine start, check that no amber cross is displayed on the ENG SD page for OIL TEMP indication of the affected engine. If an amber cross is displayed, the associated EIU may be the cause of the failure (associated engine start not possible).

NO DISPATCH NO DISPATCH NO DISPATCH Refer to MEL 73-20-04 NO DISPATCH NO DISPATCH NO DISPATCH NO DISPATCH NO DISPATCH NO DISPATCH Refer to MEL 73-30-01 NO DISPATCH NO DISPATCH Not related to MEL NO DISPATCH Refer to MEL 71-10-01 NO DISPATCH NO DISPATCH Refer to MEL 73-30-03 NO DISPATCH

N Registration

Actual alert False alert Actual alert False alert FOR NEO Aircraft Only

Page: ECAM-22


DISPATCH CONDITION

ENG 1(2) FUEL FILTER DEGRAD ENG 1(2) FUEL RETURN VALVE ENG 1(2) FUEL SENSOR FAULT ENG 1(2) FUEL STRAINER CLOG ENG 1+2 FUEL STRAIN CLOG ENG 1(2) FUEL VALVE FAULT ENG 1(2) HIGH VIBRATION

Refer to MEL 73-30-06 Refer to MEL 73-11-01 Refer to MEL73-30-07 Refer to MEL 73-30-09 NO DISPATCH NO DISPATCH Not related to MEL

ENG 1(2) HOT FUEL ENG 1(2) HP FUEL VALVE ENG 1(2) HP FUEL VALVE ENG 1(2) HP TIP CTL FAULT

NO DISPATCH NO DISPATCH



N Registration

REMARK

FOR NEO Aircraft Only FOR NEO Aircraft Only

Page: ECAM-23


DISPATCH CONDITION

REMARK



N Registration

Page: ECAM-24

MEL-A318A319A320A321-N

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