STANDARD OPERATING PROCEDURES
PART B – AEROPLANE OPERATING MATTERS
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ATR-72 STANDARD OPERATING PROCEDURES
This ATR-72 STANDARD OPERATING PROCEDURES is published under the authorization of the Cambodia Angkor Air, Chief Operation Officer. Any questions with respect to the use of this manual or information contained herein should be addressed to: Flight Operations Department Cambodia Angkor Air 206A Norodom Blvd, Phnom Penh, Cambodia Tel: +855.23666787 Fax:+855.23224164 Email:
[email protected] [email protected]..
ATR-72 STANDARD OPERATING PROCEDURES
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LIST OF DISTRIBUTION TITLE
LOCATION
COPY No
PhnomPenh
01 HC
Aircraft
VN-B227
01 HC
Aircraft
VN-B231
01 HC
State Secretariat of Cambodia Aviation
Safety Quality and Security Division Technical Division Flight & Cabin Crew Department Flight Operation Department
PhnomPenh PhnomPenh PhnomPenh PhnomPenh
01 CD 01 CD 01 CD 01 HC
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ATR-72 STANDARD OPERATING PROCEDURES
SECTION 0 INTRODUCTION
ATR-72 STANDARD OPERATING PROCEDURES
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INTRODUCTION
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0.1
INTRODUCTION
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0.1.1
Manual Policy
0.1/P1
0.1.2
General Aircraft Information
0.1/P1
INTRODUCTION
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INTRODUCTION ATR-72 STANDARD OPERATING PROCEDURES
0.1
INTRODUCTION
0.1.1
Manual Policy
This ATR-72 Standard Operating Procedures Manual conforms to the CCAR manual format for Aeroplane Operating Matters – Type Related. This manual contains the Company ATR-72 Standard Operating Procedures and additional Company information and procedures that are to be used in conjunction with the ATR-72 Flight Crew Operating Manuals Volumes 1, 2 and 3 and the Quick Reference Handbook. In the interests of standardisation these Standard Operating Procedures do not duplicate, except where considered necessary, information available in the ATR-72 Flight Crew Operating Manuals. Amendment and revision of this manual shall be in accordance with Company Policy and Administration Manual, Chapter 0.2. It is the responsibility of all manual holders and offices holding copies of the manual to update them when revisions or bulletins are received, in accordance with the instructions included in the revision or bulletin. 0.1.2
General Aircraft Information
0.1.2.1
Units of Measurement
Company operations are based upon the use of metric units of measurement. 0.1.2.2
Abbreviations
Refer ATR-72 Flight Crew Operating Manual – Volume 1 for a listing of standard abbreviations. 0.1.2.3
Aircraft Dimensions
Refer ATR-72 Flight Crew Operating Manual – Volume 1, 1.00.10 for aircraft dimensions. 0.1.2.4
Conversion Tables
Refer Company Policy and Administration Manual, Chapter 0.1, page 21 for conversion tables.
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OPERATING PROCEDURES
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SECTION 1 LIMITATIONS
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LIMITATIONS
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1.1
LIMITATIONS
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1.1.1
General
1.1/P1
1.1.2
Passenger Configuration
1.1/P1
1.1.3
Mass and Centre of Gravity
1.1/P1
1.1.4
Speed and Weight Limitations
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1.1.5
Performance Limitations
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LIMITATIONS
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1.1
LIMITATIONS
1.1.1
General
Refer ATR-72 Flight Crew Operating Manual, Chapter 2.01 for applicable limitations. 1.1.2
Passenger Configuration
The aircraft seating capacity is 68 passengers in an all economy class configuration. 1.1.3
Mass and Centre of Gravity
Refer Part B Section 9 – Mass and Balance 1.1.4
Speed and Weight Limitations
1.1.4.1
General
Refer ATR-72 Flight Crew Operating Manual, Chapter 2.01 for applicable speed and weight limitations. 1.1.4.2
Crosswind Limitations
Company crosswind limitations are as follows: Runway Width (m)
Dry Runway (Kt)
Wet Runway (Kt)
45
30
25
30
25
15
Maximum cross wind 20 kts must be applied when aircraft stopping capability is degraded (ground spoiler and/or one brake is inoperative). Maximum cross wind 20 kts must be applied and visibility is degraded (RVR is 400 m or less).
Friction coeficient 0.4 and above
1.1.5
Breaking Action Good
Crosswind component(kt) Apply above mentioned table
0.39 -0.36
Good/medium
15
0.35 -0.30
Medium
15
0.29 -0.26
Medium/poor
10
0.25 -0.10
Poor
5
Performance Limitations
Refer Part B Section 4 – Performance and Runway Analysis Manual
LIMITATIONS
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.
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SECTION 2 NORMAL PROCEDURES
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ATR-72 STANDARD OPERATING PROCEDURES
2.1
OPERATING POLICY
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2.1.1
General
2.1/P1
2.1.2
Crew Coordination Concept (CCC)
2.1/P1
2.1.3
Checklists
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2.1.4
Task Sharing
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2.1.5
Standard Calls
2.1/P7
2.1.6
Briefings
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2.2
PRE-DEPARTURE
2.2/P1
2.2.1
Departure Clearance
2.2/P1
2.2.2
Flap Selection for Takeoff
2.2/P1
2.2.3
Takeoff Data
2.2/P1
2.2.4
First Officer Takeoff and Landing
2.2/P2
2.3
TAXI OUT
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2.3.1
ATC Clearance
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2.4
TAKEOFF
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2.4.1
Takeoff Minima
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2.4.2
Monitoring During Takeoff
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2.5
AFTER TAKEOFF
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2.5.1
Clean Up and Thrust Reduction Altitudes
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2.5.2
Maximum Angle of Bank
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2.5.3
Turns after Takeoff
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2.5.4
Departure Terrain Awareness
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2.5.5
Autopilot Engagement
2.5/P1
2.5.6
Fight Mode Annunciation (FMA) Mode Changes
2.5/P1
2.5.7
Flight in Turbulence
2.5/P2
2.5.8
Fuel Management
2.5/P2
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2.6
CRUISE FLIGHT AND DESCENT
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2.6.1
Cruise Flight
2.6/P1
2.6.2
Descent
2.6/P2
2.7
APPROACH AND LANDING
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2.7.1
General
2.7/P1
2.7.2
Deceleration Sequence
2.7/P1
2.7.3
CAT I ILS Procedure
2.7/P2
2.7.4
Non-Precision Approach
2.7/P3
2.7.5
Turns onto Final Approach
2.7/P4
2.7.6
Stabilised Approach Requirements
2.7/P4
2.7.7
Mandatory Missed Approach
2.7/P5
2.7.8
Monitoring During Approach
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2.7.9
Aiming Point
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2.7.10
Crosswind Landing
2.7/P6
2.7.11
Heavy Landing
2.7/P6
ATR-72 SOP APPENDIX
NORMAL PROCEDURES
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2.1
OPERATING POLICY
2.1.1
General
It is Company policy to operate the ATR-72 aircraft in accordance with the applicable ATR Flight Crew Operating Manuals and Quick Reference Handbook. The standard operating procedures outlined in this section are to be applied in conjunction with the procedures detailed in the ATR Flight Crew Operating Manuals. The following sets out the abbreviations used in this manual for the assignment of flight crew duties: (a)
CM 1 - Refers to the flight crew member in the left hand seat;
(b)
CM 2 - Refers to the flight crew member in the right hand seat;
(c)
PF – Refers to the pilot flying; and
(d)
PNF – Refers to the pilot not flying.
At the end of this Section there is a Standard Operating Procedures Appendix that provides a summary of standard operating procedures for the ATR-72. To improve the service life on duplicated systems, system 1 should be used when operating on odd number days and system 2 when operating on even number days. 2.1.2
Crew Coordination Concept (CCC)
2.1.2.1
General
Standard operating procedures have been established to ensure that flight deck operations are conducted in a safe and efficient manner. It is essential that flight deck crew members are fully aware of the procedures outlined in this section and that they are adhered to in normal and emergency/abnormal operations. Standard Operating Procedures are designed to be: (a)
Simple;
(b)
Similar;
(c)
Self-explanatory; and
(d)
Safe
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To apply Standard Operating Procedures in a modern two crew aircraft, a coordinated effort must be made to fully utilize the available technology and is called - Crew-Coordination-Concept (CCC) 2.1.2.2
Purpose
The purpose of the Crew Coordination Concept (CCC) is to ensure the full leadership/responsibility of the Pilot-in-Command (PIC) regardless of whether he/she is the PF or the PNF. Tasks between PF and PNF must be shared such that the PF is able to pay full attention to flight manipulation and that both pilots work as a team to provide mutual supervision, information and assistance. 2.1.2.3
Subdivision of CCC
CCC is generally subdivided into the following: (a)
Operation of Flight Deck Switches and/or Levers (i)
If a switch or lever can only to be reached by ONE CM, then this CM shall only operate it;
(ii)
If a switch or lever is to be reached by both CM’s, the CM who is assigned, as the PNF shall operate such switch or lever;
(iii)
Once a CM is responsible for the operation of a particular switch or lever he shall continue to be responsible for its operation under all normal operation conditions. This procedure shall only be altered if the workload under a specific condition becomes too high for the actions of the normally scheduled CM;
(iv)
The PIC can at any time give a command to the other CM to transfer the responsibility for a certain action to that crewmember for a limited action.
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(b)
Communications Communication between CM’s must be systematic and standardized and is divided into the following three categories: (i)
Call-outs Call-outs are necessary for:
(ii)
•
The transferring of information;
•
Acknowledgment of a certain situation; and
•
Checking for any incapacitation
Announcements CM’s must provide announcements if deviation(s) from normal are experienced. These announcements serve the purpose of alerting the CM responsible for the deviation(s) from normal that a corrective action must be carried out (e.g. a “below glide slope” announcement should result in a corrective action to decrease the rate of descent). There must be a response to any announcement from the addressed CM. If there is no response the announcement shall be repeated. If there is still no response from the addressed CM this CM has to be considered incapacitated and control shall be taken by the other CM using the call out “I have control”.
(iii)
Commands A command is an order given to change the aircraft’s configuration such as flap setting, power setting and landing gear position. After a command is received, the addressed CM (the PNF) must acknowledge the actions required by the command and report the status of the new configuration. As a final confirmation the CM giving the command must confirm the new configuration. For example: 1.
Command
PF:
“FLAPS 15”
2.
Acknowledgment
PNF:
“FLAPS 15 selected”
3.
Report
PNF:
“FLAPS 15 set”
4.
Confirm
PF:
“Check”
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OPERATING POLICY
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
2.1.3
Checklists
2.1.3.1
General
The normal checklist is used to make sure that the aircraft is safely prepared for the next flight phase. It serves to verify actions already performed and shall be used as a “DO-AND-READ list”. Individual checklists for the particular phase of flight are kept as short as possible and include all safety and other necessary items. The checklist items generally follow the panel scan sequence. Individual checklists should be read in their entirety and should not be interrupted. If interruption cannot be avoided the complete particular checklist must be re-read from its beginning. 2.1.3.2
Requesting a Checklist
Prior to requesting a checklist, PF (on ground always CM 1) shall ensure: (a)
That the other CM is at their station;
(b)
That all required panel scan actions have been completed.
The PF can then request the appropriate checklist by announcing “XXXXX Checklist” 2.1.3.3
Reading a Checklist
All checklists are read by PNF (on ground always CM 2). Reading shall start with the complete checklist title. Only the left side of the print is to be read. The reader shall verify that the answers comply with the right side of the print before proceeding. Upon completion of the checklist the PNF shall announce “XXXXX Checklist completed” 2.1.3.4
Responding to a Checklist
For each item one or both CM’s are assigned to respond. Assignment depends on role (PF/PNF) or seat location (CM 1/CM 2) and is printed behind each checklist. If more than one CM is assigned, the response sequence is PF first followed by the PNF. The assigned CM shall only respond after having checked the existing configuration/condition. The other CM shall, whenever feasible, crosscheck the validity of the response to provide redundancy.
NORMAL PROCEDURES
2.1/P5
OPERATING POLICY
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
2.1.3.5
Deviations from Standard
If the actual configuration/condition is inadvertently not in accordance with the checklist standard, corrective action shall be initiated before proceeding. If the actual configuration/condition is purposely not in accordance with the checklist standard (e.g. abnormal operation or MEL procedure) the response must be modified to reflect the actual situation. Any such deviation(s) from the standard position must be fully understood by all CM’s. 2.1.4
Task Sharing
2.1.4.1
General
Normal procedures describe actions that are necessary for the routine operation of the aircraft. While the sequence of procedures follows the natural phases of flight the sequence of actions in a procedure normally follows the standardized scan of panels or equipment except in the case where out of sequence priority actions are required. All actions of a procedure are either required to operate the aircraft safely in the related phase of flight or to prepare the aircraft for the following phase of flight. Each action is assigned to a specific crewmember to ensure coordinated operation. Basic principle during preparation is the “Lights Out Concept”. For all procedures the general task sharing stated below is applicable and assumes that the PF remains as the pilot flying throughout the procedure: (a)
PF Responsibilities (i)
PL’s
(ii)
Flight path and airspeed control
(iii)
Aircraft configuration
(iv)
Navigation
NORMAL PROCEDURES
2.1/P6
OPERATING POLICY
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
(b)
2.1.4.2
PNF Responsibilities (i)
Reading of the checklist
(ii)
Execution of required actions
(iii)
Actions on the overhead panel
(iv)
Communications
Principles of Normal Checklist Application
Normal cockpit scan patterns are first performed by memory rather than by direct reference to the checklist. There are two versions of the Final Cockpit Preparation checklist: (a)
Complete Procedure Checklist This checklist is used for the first flight of the day, after any routine maintenance, if the aircraft has been left unattended by qualified personnel, if the previous crew completed the “Leaving Aircraft Procedure” or if there is any doubt about the status of the aircraft.
(b)
Transition Procedure Checklist This checklist follows the same scan pattern as the Complete Procedure but omits system functionality checks that are not required and is used in during transit stops or a series of flights.
NORMAL PROCEDURES
2.1/P7
OPERATING POLICY
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
2.1.5
Standard Calls
2.1.5.1
General
Standard calls are an established method of ensuring that the flight deck crew operates as a team and that both pilots are "in the loop" at all times. Standard calls are also an essential method of ensuring that undetected subtle incapacitation does not occur, particularly during critical stages of flight. 2.1.5.2
Takeoff
Condition
Positive climb indicated on VSI and altimeter after lift off. 2.1.5.3
Response PNF
PF
“Positive Climb”
“Gear Up”
Climb and/or Descent
Condition
Response PNF
PF
“1,000 feet to go”
“Check”
Transition altitude during climb:
“Transition altitude” “___Flight level” (Call out deviation)
“_____Flight level now”
Transition level during descent.
“Transition level” “___Feet” (Call out deviation)
“_____Feet now”
10,000 FT/FL100 during climb or descent.
“Crossing 10,000 or FL100”
“Checked”
1,000 FT to any assigned or limiting altitude or until established inbound on an instrument approach.
NORMAL PROCEDURES
2.1/P8
OPERATING POLICY
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
2.1.5.4
Visual Approach
Condition
When radio altitude displays at 2,500 FT When cleared for a visual approach:
Response PNF
PF
“Radio altitude alive”
“Checked”
“Missed approach ……feet set”
“Checked”
“Five hundred stable” or “Five hundred unstable________”( name of deviation)
“Checked continue” or “Correcting____” “Correcting____” (name of deviation)
“Go-around”
“Going around”
The altitude selector should be set to 1,500 FT once commencing final approach. 500 FT AGL
If deviation not corrected after two announcements. 100 FT
“One hundred” “Eighty” “Sixty” “Forty” “Twenty” “Ten”
NORMAL PROCEDURES
2.1/P9
OPERATING POLICY
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
2.1.5.5
CAT I ILS – Manual or Autopilot Approach
Condition
Response PNF
PF
“Radio altitude alive”
“Checked”
LOC* displayed
“Loc star”
“Checked”
Set runway heading
“Checked”
“Runway heading___set”
“Glide slope star”
“Checked”
“Checked
“Missed approach altitude_____feet altitude_____feet set”
“Final altitude checked”
“Checked_____feet”
When radio altitude displays at 2,500 FT
GS* displayed Missed approach altitude set on ADU Passing Outer Marker or Locator. 1,000 FT AGL
If deviation not corrected after two announcements.
“One thousand stable” “Checked continue” or or “Correcting____” “One thousand (name of deviation) unstable_________ (name of deviation) “Go-around”
“Going around”
500 FT above minima
“Five hundred to minimum”
“Checked”
100 FT above minima.
“One hundred to minimum”
“Checked”
At minimum.
“Minimum”
If visual contact established.
“Landing”
If no visual contact. At minimums – No response from PF Positive climb indicated on VSI and altimeter.
“Go-around” “I have control____” State intentions “Positive climb”
“Gear up”
NORMAL PROCEDURES
2.1/P10
OPERATING POLICY
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
Condition
Response PNF
100 FT
“One hundred” “Eighty” “Sixty” “Forty” “Twenty” “Ten”
PF
NORMAL PROCEDURES
2.1/P11
OPERATING POLICY
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
2.1.5.6
Non – Precision Approach – Manual or Autopilot
CONDITION
RESPONSE PNF
PF
“Timing”
“Timing__minutes” “Timing__minutes”
ALT* (Step down altitude)
“ALT star”
“Checked”
ALT HOLD
“ALT hold”
“Checked”
Setting of next step down altitude
“Checked”
“Pre-set altitude____feet”
“Radio altitude alive”
“Checked”
“Time ____out” “My side set”
“Final course____set”
FAF/FAP
“Final approach approac h fix”
“Checked” “Timing__minutes” (if required)
Established on final descent
“Rate of descent____feet per minute set”
“Checked”
“One thousand thousan d stable” or “One thousand unstable________”(n ame of deviation)
“Checked continue” or “Correcting____” “Correcting____” (name of deviation)
“Go-around”
“Going around”
500 FT above MDA
“Five hundred to MDA”
“Checked”
100 FT above MDA
“One hundred to MDA”
“Checked”
Over station outbound
When radio altitude displays at 2,500 FT Inbound turn
1,000 FT AGL
If deviation not corrected after two announcements.
NORMAL PROCEDURES
2.1/P12
OPERATING POLICY
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
CONDITION
RESPONSE PNF
At MAP.
“Minimum”
If visual contact established.
“Landing”
If no visual contact. At MAP – No response from PF Positive climb indicated on VSI and altimeter. 100 FT
PF
“Go-around” “I have control____” State intentions “Positive climb” “One hundred” “Fifty” “Forty” “Thirty” “Twenty” “Ten”
“Gear up”
NORMAL PROCEDURES
2.1/P13
OPERATING POLICY
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
2.1.5.7
Out of Tolerance Calls
CONDITION
Localiser:
RESPONSE PNF
PF
“Localiser”
“Check”
“Glideslope”
“Check”
“Track”
“Check”
“Track”
“Check”
“Speed”
“Check”
“Sink rate”
“Check”
When localiser deviation exceeds one dot. Glideslope: When glideslope deviation exceeds one dot. VOR approach: Course bar deviation exceeds ½ dot. NDB/Locator approach: Track outside +/- 5 degrees. Below 500 feet with airspeed +10/-0 knots from required speed. Below 500 feet with rate of sink in excess of 1,000 feet per minute.
The PNF should continue to repeat the appropriate call(s) until it is obvious that the PF has corrected the deviation and the flight path is returning to within tolerance.
NORMAL PROCEDURES
2.1/P14
OPERATING POLICY
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
2.1.6
Briefings
2.1.6.1
General
In order to ensure a safe, efficient and coordinated operation, briefings must be conducted as defined below. Briefings should be concise and only address important safety items. Prolonged briefings with unnecessary secondary information should be avoided. 2.1.6.2
Pre-Flight
(a)
Flight Deck Crew and Cabin Crew Briefing Prior to the first flight with new crew members or at a crew change the Commander is responsible to assemble together and brief other flight deck crew members, the Purser and all cabin crew on the following: (i)
Information relating to the flight such as flight time, cruise altitude, en-route and destination weather conditions and any other pertinent information;
(ii)
Any additional security measures (if applicable) for the flight(s);
(iii)
Other relevant information.
The Purser in turn is to advise the Commander on any special passengers such as deportees, stretcher case, etc. At transit stops with the same cabin crew the Commander should brief the Purser only on the information relating to the next flight sector and the Purser should in turn advise the Commander of any non-standard information. (b)
Flight Deck Technical Log Briefing Prior to the first flight on a particular aircraft the Commander must review the Technical Log and brief the First Officer on any MEL or ADD items, if applicable.
NORMAL PROCEDURES
2.1/P15
OPERATING POLICY
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
(c)
Pre-Takeoff Briefing Prior to takeoff the Commander or PF will ensure that all flight deck crew members are briefed on the procedures to be followed in the event of an emergency. A full briefing covering the items detailed in Standard Emergency Briefing below should be given on a flight deck crew’s first flight at the commencement of a tour of duty. On subsequent takeoffs with the same crew items (i), (ii), (iii) and (v) below should be covered. The term ‘standard emergency procedures’ can be used to cover item (iv). Standard Emergency Briefing (i)
Runway to be used including any weather considerations such as wet runway, possible windshear, cross-wind, etc;
(ii)
Obstacle information, if applicable;
(iii)
Normal departure procedure including the anticipated departure track (SID), MSA considerations, radio aid settings and transition altitude;
(iv)
Emergency procedure including: Up to 70 Kt takeoff may be rejected for less significant malfunctions; Between 70 Kt and V1 a rejected takeoff should only be conducted in the event of an engine failure (identified by at least two instruments), fire warning and/or severe damage or any malfunction or condition where there are unambiguous indications that the aircraft will not fly safely. Note:
Either pilot may call ‘STOP’. However, in all cases the rejected takeoff procedure shall be carried out by the pilot in the left hand seat.
No action will be taken up to acceleration altitude, except in the case of an engine flame out when the PNF must confirm “Engine 1 or 2 (as applicable) – “Up trim” and “Auto feather”;(confirm manually if necessary) ,or engine fire when memory items must be execute immediately above an 400ft AGL.
NORMAL PROCEDURES
2.1/P16
OPERATING POLICY
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
(v) (d)
2.1.6.3
•
Acceleration altitude
•
Single engine procedure
•
Checklist sequence
Any other additional information.
Jumpseat/Observer Briefing A briefing is to give to any approved observers traveling in the jumpseat and it is the PIC’s responsibility to ensure that this is completed. The briefing may be given by either pilot and is to include safety equipment located in the cockpit and the procedures for the observer to adhere to in the event of an emergency. The briefing is to include in the cockpit and how to use the cockpit overhead emergency exit.
Approach
Prior to commencement of descent the PF must brief the PNF on the salient points of the arrival including STAR (if applicable) and the instrument approach. An instrument approach briefing should include the following: (a)
Chart number and runway;
(b)
Chart date;
(c)
Transition level;
(d)
MSA;
(e)
Initial approach altitude and holding procedures including holding pattern entry, minimum altitude, time/distance limits, wind corrections;
(f)
Altitude at outer marker, locator or any limiting altitude on the approach;
(g)
Minimum altitude and visibility including radio altimeter setting (if applicable);
(h)
Field/touch down elevation;
(i)
Missed approach procedure and if applicable, circling altitude and anticipated manoeuvring;
(j)
Glideslope and VASI angle;
(k)
Runway length and condition.
The briefing should also include the Vref setting and the wind and gust additive.
NORMAL PROCEDURES
2.1/P17
OPERATING POLICY
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
2.1.6.4
Post Flight
Following a flight or the last flight in a series of flights the Commander should assemble the flight deck crew and the cabin crew to:
2.1.7
(a)
Conduct a review of the flight(s) including a review of any matters applicable for inclusion in the Captain’s or the Purser’s Report; and
(b)
Complete and agree the crew duty and rest time data sheet.
Automation of the flight
The automation for the task can be followed by AP or manually. (a)
With HDG mode (Heading)
(b)
With NAV mode ( Radial, Localizer, LNAV)
(c)
With APP mode (ILS approach)
The AFCS and any automation task have to be monitored by: (a)
Cross-checking the status with other sources
(b)
Observing the result of any change
(c)
Supervising the resulting guidance and aircraft performance
NORMAL PROCEDURES
2.1/P18
OPERATING POLICY
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
NORMAL PROCEDURES
2.2/P1
PRE-DEPARTURE
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
2.2
PRE-DEPARTURE
2.2.1
Departure Clearance
Both pilots must be in the flight deck for the receipt of the ATC clearance. The clearance must be recorded on the computer flight plan adjacent to the route line. After ATC clearance has been received both pilots must be absolutely certain that the clearance is understood before "read back" to ATC. The review of the clearance must be conducted in the following manner, assuming expected SID or departure tracking has already been entered into the GNSS;
2.2.2
(a)
The First Officer will read the clearance while the Commander will observe the GNSS to ensure compatibility with the actual ATC clearance received;
(b)
If the comparison between the ATC clearance and the data in the GNSS are different the Commander will re-program the GNSS for the clearance received;
(c)
The Commander will set the MCP altitude selector to the initial cleared altitude, which is to be cross checked by the First Officer;
(d)
The Commander will set the HDG select to the required initial after takeoff heading.
Flap Selection for Takeoff
The standard Company flap setting for takeoff is Flaps 15. 2.2.3
Takeoff Data
Takeoff performance should be calculated in accordance with the following: (a)
Reference the RTOW charts to obtain the maximum takeoff weight for the airport at the actual temperature and enter this as the MTOW on the takeoff data card. The Commander shall inform the Station Manager or Load Controller of the MTOW;
(b)
On the takeoff data card, note whether takeoff will be conducted as a bleeds ON or bleeds OFF takeoff, in accordance with the departure temperature and wind conditions;
NORMAL PROCEDURES
2.2/P2
PRE-DEPARTURE
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
2.2.4
(c)
Once the load sheet has been received, cross checked and signed by the Commander the First Officer shall obtain the takeoff speeds for that particular weight from the QRH and enter on the takeoff data card;
(d)
The First Officer should read out the V1, VR and V2 speeds which shall be set and cross checked;
(e)
The F/O shall enter the zero fuel weight (ZFW) on the GNSS performance page which shall be cross checked by the Commander.
First Officer Takeoff and Landing
Commanders are approved, at their discretion, to give First Officers takeoffs and landings with the exception that initial command Commanders must complete a minimum of 50 hours or 10 landings, which ever occurs first, before giving First Officers takeoffs or landings. Prior to giving a First Officer a takeoff or landing the Commander should assess the existing conditions and the First Officer's experience; both total and recent. If there are any doubts the Commander must conduct the takeoff or landing. During takeoff and landing the Commander must always be in a position to take over control of the aircraft with feet lightly on the rudder pedals, one hand adjacent to the control column and the other hand adjacent to the thrust levers. In the event of an engine failure after V1, the First Officer should continue to fly the aircraft until the Commander, at his discretion, takes over control. Such take over, if required, should not take place before the landing gear has been selected up. Any transfer of control should be clearly understood between both pilots with the Commander (CM1) stating "I have control" or “You have control” and the First Officer (CM2) responding with the words "You have control" or “I have control”.
NORMAL PROCEDURES TAXI ATR-72 STANDARD
2.3/P1
Rev 00 15 Jul 09
OPERATING PROCEDURES
2.3
TAXI
2.3.1
ATC Clearance
Prior to takeoff the PF will brief the PNF on the salient points of the ATC clearance. If the ATC clearance has not been obtained prior to taxi it should be reviewed in accordance with 2.2.1 Departure Clearance. 2.3.2
Taxi consideration
(a) Taxi operations must be conducted by the pilot in the left hand seat (b) Maintain outside vigilance during taxi (c) PM will advise taxi route by airport diagram. (d) In case of captain incapacipitation, the first officer requests to tow the aircraft to parking bay.
NORMAL PROCEDURES TAXI
2.3/P2
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
NORMAL PROCEDURES
2.4/P1
TAKEOFF
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
2.4
TAKEOFF
2.4.1
Takeoff Minimum
Takeoff minima are not less than the minima specified in the Jeppesen chart 10-9. The lowest authorised takeoff minima for the ATR-72 aircraft is 400 m provided the runway is equipped with operational runway edge lighting operational and the runway centreline markings are clearly visible. Note: The Commander is solely responsible for ensuring the applicable takeoff minima exists when conducting reduced visibility takeoffs. The visibility minima must be available at the threshold and in the lift-off zone. Where visibility information is not available for the lift-off zone, the latter is deemed to be between 1,300 m and 1,500 m from the threshold. 2.4.2
Monitoring During Takeoff
The PF must observe his/her airspeed during takeoff with the "V1" and "Rotate" calls from the PNF serving as backup only. During all instrument takeoffs the PNF must positively monitor flight instruments to at least 500 FT and alert the PF if tolerances are being exceeded.
NORMAL PROCEDURES
2.4/P2
TAKEOFF
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
NORMAL PROCEDURES
2.5/P1
AFTER TAKEOFF
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
2.5
AFTER TAKEOFF
2.5.1
Clean Up and Thrust Reduction Altitudes
It is required that thrust reduction, flap retract and clean up heights as promulgated in the Flight Crew Operating Manual or Runway Analysis Manual be adhered to. Subject to published exceptions, 800 FT (AGL) should be used as the standard thrust reduction altitude. 2.5.2
Maximum Angle of Bank
Twenty-five degrees is the normal angle of bank with a maximum of thirty degrees that must be closely monitored, particularly during instrument flight. 2.5.3
Turns after Takeoff
Turns after takeoff at altitudes below 500 FT (AGL), except for noise abatement procedures, are to be avoided. An appropriate cockpit PA announcement should be made advising passengers when such a turn is necessary. 2.5.4
Departure Terrain Awareness
On all IMC departures, without a published SID, speed should be held at normal climb speed as published in the Flight Crew Operating Manual, unless in icing conditions. In icing conditions, the speed shall be red bug speed for that particular weight, until reaching the Minimum Sector Altitude (MSA) the Minimum Off-route Altitude (MORA) or the Minimum En-route Altitude (MEA). Pilots must always assess departure terrain and at some airports it may be necessary to climb in the circuit area to set heading over the top at the MSA, MORA or MEA, as applicable. 2.5.5
Autopilot Engagement
The PF must advise the PNF when the autopilot is engaged and the selected active modes. Note: Autopilot is not to be engaged below 100 FT (AGL). 2.5.6
Fight Mode Annunciation (FMA) Mode Changes
During any flight phase any change in FMA annunciation must be called by the pilot first observing this change.
ATR-72 STANDARD OPERATING PROCEDURES
2.5.7
NORMAL PROCEDURES
2.5/P2
AFTER TAKEOFF
Rev 00 15 Jul 09
Flight in Turbulence
Refer Flight Crew Operating Manual, Chapter 2.01.03 for turbulence penetration speed. 2.5.8
Fuel Management
At any time that the configuration of the fuel system is changed from normal operation, e.g. Cross-feeding, both pilots are to be aware of the changed configuration and an estimated time calculated and recorded to return the fuel system to normal operation.
NORMAL PROCEDURES
2.6/P1
CRUISE FLIGHT AND DESCENT
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
2.6
CRUISE FLIGHT AND DESCENT
2.6.1
Cruise Flight
2.6.1.1
Flight Level Check
On reaching initial cruise flight level (and any subsequent amended flight level) the crew must conduct a positive check between the altimeters and the flight level displayed in the altitude alert window. 2.6.1.2
Oxygen Masks
Both crew members must wear oxygen masks with the diluter demand regulator in the NORMAL position at all times while the cabin altitude exceeds 10,000 FT. 2.6.1.3
En-Route Weather Monitoring
Pilots shall regularly monitor the weather reports of suitable en-route alternates, the destination and the destination alternate(s). 2.6.2
Descent
2.6.2.1
Arrival Procedures
In IMC or VMC (day or night) on a track without a published STAR, the aircraft must maintain the MEA, MORA or MSA, as applicable, until commencement of the instrument approach procedure. Under VMC (day or night) the aircraft should complete the appropriate instrument approach procedure except at airports where it is safe to conduct a visual approach once the aircraft is within the relevant circling area. Under radar vectoring the aircraft may be assigned altitudes below the MEA, MORA or MSA. Under these circumstances pilots must continue to remain aware of terrain clearance requirements. 2.6.2.2
Rate of descent at lower heights At the lower altitudes the rates of descent are restricted as: Bellow 3.000ft…………………..
3.000ft/min or less
Bellow 2.000 ft…………………
2.000ft/min or less
Bellow 1.000ft…………………….1.000ft/min or less
NORMAL PROCEDURES
2.6/P2
CRUISE FLIGHT AND DESCENT
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
NORMAL PROCEDURES
2.7/P 1
APPROACH AND LANDING
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
2.7
APPROACH AND LANDING
2.7.1
General
In preparation for any instrument approach the briefing requirements as set out in 2.6.3 and the Standard Calls, including the Out of Tolerance Calls, as set out in 2.1.5 apply. Whenever weather conditions are such that an instrument approach is necessary the autopilot(s) should be engaged to fly the approach. Operations are permitted to CAT I minima all engines or one engine out, with or without the autopilot and/or flight director engaged. First Officers are not permitted to operate as the PF during an instrument approach where the reported landing minima are below 200 FT and visibility is less than 800 m, or 550 m RVR. In the event of an engine out go-around following an instrument approach the level off altitude listed for the takeoff on the particular runway should be used as the acceleration altitude. 2.7.2
Deceleration Sequence
2.7.2.1
IMC Approach Deceleration Sequence 0
Commence deceleration on glide slope (3 ) and: Maintain IAS=240 Kt
2.7.2.2
(a)
At 180 Kt extend flaps 15;
(b)
At 170 Kt select landing gear down;
(c)
At 150 Kt select flaps 30;
(d)
Adjust speed to Vapp - Vapp + 10 Kt not later than 1,000 FT (AGL).
VMC Approach Deceleration Sequence 0
Maintain a 3 descent path with IAS=240 Kt, retard PL to FI at altitude = (IAS x 10), adjusted for head or tailwind, and: (a)
At 180 Kt extend flaps 15;
(b)
At 170 Kt select landing gear down;
(c)
At 150 Kt select flaps 30;
(d)
Adjust speed to Vapp - Vapp + 10 Kt not later than 500 FT (AGL).
ATR-72 STANDARD OPERATING PROCEDURES
2.7.3
NORMAL PROCEDURES
2.7/P2
APPROACH AND LANDING
Rev 00 15 Jul 09
CAT I ILS Procedure
During the briefing for the approach the DH should be set, for reference only, to the CAT I minimum. The PF will nominate whether the approach will be conducted as a manual or autopilot approach. The aircraft should be configured for the ILS approach in accordance with the Normal Procedures detailed in the ATR-72 Flight Crew Operating Manual. The PNF must primarily monitor flight instruments throughout the approach and provide the appropriate standard calls. The PF must primarily monitor flight instruments until after the “500 feet to minimum” call. After this call the PF should expand instrument scan to include outside visual cues. The PNF should call “visual” any time visual reference is established above the minimum. At the “minimum” call by the PNF the PF should assess outside conditions and declare either “landing” or “go-around” as the case may be. The “landing” call at the minimum by the PF must be based upon the observation of the approach lights, runway lights, runway or touchdown zone lights and that the approach can be continued in visual conditions on the normal approach profile to a safe landing. After the “landing” call, by the PF the PNF MUST maintain concentration on the flight instruments in order to monitor the glideslope and localiser for the remainder of the approach. If the PF calls “go-around” at the minimum, or if visual contact is lost after the minimum, an immediate go-around in accordance with the Normal Procedures detailed in the ATR-72 Flight Crew Operating Manual must be conducted.
ATR-72 STANDARD OPERATING PROCEDURES
2.7.4
Non Precision Approach
2.7.4.1
Procedure
NORMAL PROCEDURES
2.7/P3
APPROACH AND LANDING
Rev 00 15 Jul 09
During the briefing for the approach the applicable minimum should noted on the Landing Data Pad. The DH should be set to zero for non-precision approaches. The PF will nominate whether the approach will be conducted as a manual or autopilot approach. The aircraft should be configured for the non-precision approach in accordance with the Normal Procedures detailed in the ATR-72 Flight Crew Operating Manual. The final segment of a non-precision approach should be flown at a constant descent profile. The PNF must primarily monitor flight instruments throughout the approach and provide the appropriate standard calls. The PF must primarily monitor flight instruments until the “500 feet to minimum” call. After this call the PF should expand instrument scan to include outside visual cues. The PNF should call “visual” any time visual reference is established above the minimum. At the “minimum” call by the PNF the PF should assess outside conditions and declare either “landing” or “go-around” as the case may be. The “landing” call at the minimum by the PF must be based upon the observation of the approach lights, runway lights, runway or touchdown zone lights and that the approach can be continued in visual conditions on the normal approach profile to a safe landing. After the “landing” call, by the PF the PNF MUST continue to maintain concentration on the flight instruments to monitor the remainder of the approach. If the PF calls “go-around”, at the minimum, or if visual contact is lost after the minimum, an immediate go-around in accordance with the Normal Procedures detailed in the ATR-72 Flight Crew Operating Manual.
NORMAL PROCEDURES
2.7/P4
APPROACH AND LANDING
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
2.7.4.2
Circling Approach
The aircraft should be configured for the circling approach in accordance with the procedures detailed in the ATR-72 Flight Crew Operating Manual. During a circling approach the PNF must primarily monitor the flight instruments and alert the PF to any out of tolerance manoeuvring. 2.7.5
Turns onto Final Approach
Turns on to final approach are to be made by at least 800 FT AGL (except for a circling approach when the minimum altitude is 500 FT AGL). 2.7.6
Stabilised Approach Requirements
Any significant deviation from the planned flight path, airspeed, or descent rate must be announced. The decision to execute a go-around is no indication of poor performance. Note:
Do not attempt a landing from an unstable approach.
All approaches must be stabilised by 1,000 FT above airport elevation in IMC and 500 FT above airport elevation in VMC. An approach is considered stabilised when all of the following criteria are met: (a)
The aircraft is on the correct flight path;
(b)
Only small changes of heading/pitch are required to maintain the correct flight path;
(c)
The aircraft speed is not more than Vref + 20 Kt IAS and not less than Vref;
(d)
The aircraft is in the correct landing configuration;
(e)
Rate of descent is no greater than 1,000 feet per minute (if an approach requires a rate of descent greater than 1,000 feet per minute a special briefing should be conducted);
(f)
Power setting is appropriate for the aircraft configuration;
(g)
All briefings and checklists have been completed.
NORMAL PROCEDURES
2.7/P5
APPROACH AND LANDING
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
Specific types of approaches are stabilised if they also meet the following additional criteria: (a)
ILS approaches should be flown within one (1) dot of the glideslope and localizer;
(b)
During a circling approach wings should be level on final when the aircraft reaches 300 feet above airport elevation.
Note:
An approach that becomes unstabilised below 1,000 FT above airport elevation in IMC or below 500 feet above airport elevation in VMC requires an immediate go-around.
The above criteria should be maintained through the rest of the approach for it to be considered a stabilised approach. If the above criteria cannot be established and maintained at and below 500 FT above airport elevation an immediate go-around should be initiated. At 100 FT above airport elevation for all visual approaches the aircraft should be positioned so that the flight deck is within, and tracking so as to remain within, the lateral confines of the runway’s extended centre-line. As the aircraft crosses the threshold it should be: (a)
Stabilised on target airspeed to within 10 Kt until arresting descent rate at flare;
(b)
On a stabilised flight path using normal manoeuvring;
(c)
Positioned to make a normal landing in the touch down zone.
If the above criteria cannot be maintained a go-around should be initiated. 2.7.7
Mandatory Missed Approach
On all instrument approaches execute an immediate missed approach if any of the following occurs: (a)
A navigation radio aid or flight instrument failure occurs that affects the ability to safely complete the approach in instrument conditions;
(b)
When on ILS final approach in IMC and either the localiser and/or glideslope indicator shows full deflection;
(c)
When the navigation instruments show significant disagreement and visual contact with the runway has not been established;
NORMAL PROCEDURES
2.7/P6
APPROACH AND LANDING
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
2.7.8
(d)
On a radar approach radio communication is lost;
(e)
On reaching the minima the required visual contact is not established.
Monitoring During Approach
On all approaches the PNF must monitor airspeed and rate of descent, particularly below 500 FT and call if either is outside tolerance. In adverse conditions the PNF should call height, airspeed and rate of descent each 100 FT below 500 FT. 2.7.9
Aiming Point
An aiming point of 300 m should be used. 2.7.10
Crosswind Landing
Prior to landing in crosswind conditions consideration must be given to the following factors: (a)
Cross wind limitations; Note:
Any crosswind corrections (e.g. for a wet or slippery runway) must be applied to the steady state wind speed.
(b)
Runway length;
(c)
Runway width;
(d)
Runway conditions;
(e)
Wind gust factor;
(f)
Expected turbulence on approach;
(g)
Correct crosswind landing technique.
The PF must be prepared to conduct a go around if the aircraft is not positioned for a safe landing. 2.7.11
Heavy Landing:
A heavy landing whether above or below the structural landing weight limit must be reported in the Technical Log with all relevant information such as actual weight, sink rate, touch down forces etc. 2.7.12
Minimum Fuel expected for Landing
When the minimum fuel quantity of 320 kgs or equipvalent of 30’ is expected upon crossing the threhold of the arrival/alternate airport, the PIC must declare an emergency using appropriate terminology and file a report immediately upon landing.
ATR72 FINAL COCKPIT PREPARATION
GROUND PHASE EVENT
Starting engine 2 in HOTEL mode should be postponed until the all passengers are on board (with GPU and Ground A/C) or 10 min before if
CM 1
- Command “Start engine number 2 in hotel mode”
ground A/C is not available (with or without GPU) Both pilots on their stations and cleared by ground staff to start engine number 2 in Hotel Mode.
-
Monitor starting
-
When NH increases announce “NH rising” or “No NH”
CM 2
- Parking brake ON -
Check FU value at zero Check EEC 2 FAULT light extinguished Check PWRMGT is in TO position Check PROP/BRAKE is ON Service door closed Select fuel PUMP ENG 2 to RUN Select start rotary selector to START A or START B (according to day). If any malfunction use START A & B - Check right side clear and announce “Right side clear” - Announce “Starting engine number 2” - Select START 2, check ON light illuminates and announce “Starter on” - *Monitor NH and announce “Check”. When NH passes 10%, advance CL 2 to FTR *Passing from FUEL SO to FTR is recommended between 10%-19% and when ITT>200 C Command “Timing” ˚
-
ATR-72 SOP’s
Start timing and respond “Timing”
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION PAGE 1
GROUND PHASE EVENT
Engine number 2 in hotel mode(continued)
CM 1
-
-
Ground power unit disconnection
ATR-72 SOP’s
When fuel flow increases announce “Fuel flow rising” or “No fuel flow” When ITT rising announce “ITT rising” or “No ITT” When positive oil pressure indicated announce “Oil pressure rising” or “No oil pressure”
Check start light extinguished and announce “Starter light off” or “Starter light not off” Stop timing
-
Check DC GEN 2 on line and BTC NORM illuminates
-
Request ground staff to “Disconnect GPU”
15 Jul 09 - REV 00
CM 2
- Monitor and respond “Checked” - Monitor and respond “Checked” - Monitor and respond “Checked”
- When NH passing 45% announce “NH 45” - Check ITT drop and engine number 2 idle parameters stabilized and announce “ITT drop. Stable” - Select start rotary selector to OFF & START ABORT
- Release EXT PWR switch and verify DC GEN 2 on line and BTC NORM illuminates - Select ENG 2 BLEED to ON - Select EMERG light to ON - Conduct engine number 1 fire test - Conduct CVR test - Select oxygen MAIN SUPPLY to ON - Select FDU RESET
FINAL COCKPIT PREPARATION PAGE 2
GROUND PHASE EVENT
Load sheet on board
Takeoff briefing: PF takeoff briefing to include: Read takeoff data card Any red light before V1, Captain will stop aircraft Any failure after V1, takeoff will continue. No action EXCEPT in case of engine flame out when gear up, up-trim and auto-feather must be confirmed; and in case of eng fire the memory items must be done immediately above 400ft AGL. Acceleration altitude is …….. Single engine procedure is……... Final cockpit preparation checklist
CM 1
CM 2
-
Load sheet check and sign
-
Set takeoff data bugs
- Load sheet copy received - Takeoff Data Card file - Set takeoff data bugs
-
PF gives takeoff briefing
- PF gives takeoff briefing
• •
•
• •
- Command “Final cockpit preparation checklist” RESPONSE: -
“Prop brake, no smoking, seat belts on”
READ: - “Memo panel”
-
“Three on board”
- “Gear pins and covers”
-
“___kilograms checked”
- “Fuel quantity”
-
“Left side set”
- “Takeoff data bugs” - “Right side set”
ATR-72 SOP’s
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION
PAGE 3
GROUND PHASE EVENT
CM 1
CM 2 - “Trims”
-
“____Set”
-
“___set” (cross check)
-
___set”
-
“ ______ Set”
- “Altimeters” - “___set” (cross check) - “Landing elevation” - “COM/NAV” - “Engine test”
-
“Performed”
-
“Set/PRESS CHK”
- “Parking brake”
- “Completed” -
“Checked” * Request from ground staff to start engine number 2 in Hotel Mode (Refer page 1). * Can be done before receipt of load sheet
Purser to inform “We have ___passengers, tail prop on board, may I close the door?”
-
Check passenger number agrees with load sheet and if correct command “Close the door”
Start, or push back and start clearance
- Command “Request start clearance” or “Request push back and start”
Ground air-conditioning truck disconnected and clear of aircraft
- “Takeoff briefing” - Announce “Final cockpit preparation checklist completed” - Start engine number 2 in Hotel Mode (Refer page 1)
Passengers on board:
ATR-72 SOP’s
15 Jul 09 - REV 00
- Request start, or push back and start clearance from ATC FINAL COCKPIT PREPARATION-PAGE 4
GROUND PHASE EVENT
Push back procedure:
CM 1
-
CM 2
Select NOSE WEEL STEERING to OFF
- Call ground: “Cockpit to ground”
Ground: “Ground to cockpit” “Ready for push back and start”
Ground: “Parking brake release”
- Release parking brake “ Parking brake released”
Ground: “Commencing push back”
Release of PROP BRAKE Ground: “Clear to release prop brake”
-
Select DC AUX PUMP to ON Check DOOR lights extinguished Select BEACON to ON Check PROP BRAKE green light illuminates Command “Check right side”
-
After request from ground staff “Release prop brake” Announce “Releasing number 2” Set PROP BRAKE to OFF, check red UNLK light and both blue Lights extinguished (On both MEMO and overhead panel) Select flap lever to 15 position Select ANTI SKID test (All 4 lights “F” should Illuminate and then extinguish)
-
ATR-72 SOP’s
- Check right side area clear and announce “Right side clear”
˚
Set RADAR to STBY 15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 4a
GROUND PHASE EVENT
Start engine number 1
Ground: “Clear to start engine No.1”
CM 1
CM 2
- Request ground engineer for permission to start engine number 1: “Request to start Engine No.1” - Check EEC 1 FAULT light extinguished - Select fuel PUMP ENG 1 to RUN - Select start rotary selector to START A or START B (according to day). if any malfunction use START A & B - Check left side clear and announce “Left side clear” - Announce “Starting engine number 1” - Select START 1, check ON light illuminates and announce “Starter on”
- *Monitor NH and respond “Check”. When NH passes 10%, advance CL 1 to FTR * Passing from FUEL SO to FTR is recommended Between 10%-19% and when ITT>200 C
- Monitor starting - When NH increases announce “NH Rising” or “No NH”
˚
- Command “Timing” - Start timing and respond “Timing”
- Monitor and respond “Checked” - Monitor and respond “Checked” - Monitor and respond “Checked”
ATR-72 SOP’s
15 Jul 09 - REV 00
- When fuel flow increases announce “Fuel flow rising” or “No fuel flow” - When ITT rising announce “ITT rising” or “No ITT” - When positive oil pressure indicated announce “Oil pressure rising” or “No oil pressure”
FINAL COCKPIT PREPARATION-PAGE 4b
GROUND PHASE EVENT
CM 1
- When NH passing 45% announce “NH 45”
When push back completed Ground: “Parking brake ON”
Ground staff disconnect interphone, remove chocks and stand on the side of aircraft and show the nose gear PIN. “Disconnecting”
ATR-72 SOP’s
- Check ITT drop and engine number 1 idle parameters stabilized and announce “ITT drop. Stable” - Select start rotary selector to OFF & START ABORT
Set parking brake ON Announce: “Parking brake ON” Set Nose Wheel Steering ON Check NP >14% and stable CL 2 then CL 1 to AUTO (or MAX RPM – ATR72 – 200) - Check both SGL CH lights illuminate and then extinguish and announce “SGL channel” - Check both LO PITCH lights illuminate and announce “Low pitch” - Check ACW BUS TIE (after CL2) - Check ACWILD ELEC PWR panel on line and hydraulic pressure - Select Windshield HTG to ON - Select Anti-icing as RQD - Announce to ground staff “You may disconnect”
CM 2
-
-
Check start light extinguished and announce “Starter light off” or “Starter light not off” Stop timing
-
- Announce “Testing radar”. Test radar and set to STBY mode
15 Jul 09 - REV 00
-
Check both SGL CH lights illuminate and then extinguish and respond “Checked” - Check both LO PITCH lights illuminate and respond “Checked”
- Respond “Checked”
FINAL COCKPIT PREPARATION-PAGE 4c
GROUND PHASE EVENT
Push back procedure
CM 1
-
CM 2
Select NOSE WEEL STEERING to OFF
At TAN SON NHAT AIRPORT ONLY
- Call ground: “Cockpit to ground”
Ground: “Ground to cockpit” “Ready for push back and start”
Ground: “Parking brake release” - Release parking brake “ Parking brake released”
Ground: “Commencing push back”
When push back completed
Ground: “Parking brake on”
ATR-72 SOP’s
- Set Parking brake -Announce: “Parking brake on” -Set Nose wheel steering ON
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 4d
GROUND PHASE EVENT
Release of PROP BRAKE: 1. ( Without push back procedure) or 2. (After push back procedure, when push back car disconnect at TAN SON NHAT airport ONLY)
CM 1
- Select DC AUX PUMP to ON - Check DOOR lights extinguished - Select BEACON to ON - Check PROP BRAKE green light illuminates - Command “Check right side” -
-
ATR-72 SOP’s
CM 2
- Check right side area clear and announce “Right side clear”
After request from ground staff to “Release prop brake” Announce “Releasing number 2” Set PROP BRAKE to OFF, check red UNLK light and both blue Lights extinguished (On both MEMO and overhead panel) Select flap lever to 15 position Select ANTI SKID test (All 4 lights “F” should Illuminate and then extinguish) ˚
Set RADAR to STBY
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 5
GROUND PHASE EVENT
Start engine number 1
CM 1
- Request ground engineer for permission to start engine number 1: - Check EEC 1 FAULT light extinguished - Select fuel PUMP ENG 1 to RUN - Select start rotary selector to START A or START B (according to day). if any malfunction use START A & B - Check left side clear and announce “Left side clear” - Announce “Starting engine number 1” - Select START 1, check ON light illuminates and announce “Starter on” - *Monitor NH and respond “Check”. When NH passes 10%, advance CL 1 to FTR * Passing from FUEL SO to FTR is recommended Between 10%-19% and when ITT>200 C
CM 2
- Monitor starting - When NH increases announce “NH Rising” or “No NH”
˚
- Command “Timing”
- Monitor and respond “Checked” - Monitor and respond “Checked”
- Start timing and respond “Timing” - When fuel flow increases announce “Fuel flow rising” or “No fuel flow” - When ITT rising announce “ITT rising” or “No ITT” - When positive oil pressure indicated announce “Oil pressure rising” or “No oil pressure”
- Monitor and respond “Checked”
ATR-72 SOP’s
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 6
GROUND PHASE EVENT
CM 1
- When NH passing 45% announce “NH 45” - Check ITT drop and engine number 1 idle parameters stabilized and announce “ITT drop. Stable” - Select start rotary selector to OFF & START ABORT
- Check NP >14% and stable - CL 2 then CL 1 to AUTO (or MAX RPM – ATR72 – 200) - Check both SGL CH lights illuminate and then extinguish and announce “SGL channel” - Check both LO PITCH lights illuminate and announce “Low pitch” - Check ACW BUS TIE (after CL2) - Check ACW ELEC PWR panel on line and hydraulic pressure, 3 x 3000psi - Select Windshield HTG to ON - Select Anti-icing as RQD Ground staff disconnect interphone, remove chocks and stand on LEFT side of aircraft
-
-
Check start light extinguished and announce “Starter light off” or “Starter light not off” Stop timing
-
Check both SGL CH lights illuminate and then extinguish and respond “Checked” - Check both LO PITCH lights illuminate and respond “Checked”
- Announce to ground staff “You may disconnect” - Announce “Testing radar”. Test radar and set to STBY mode
ATR-72 SOP’s
CM 2
15 Jul 09 - REV 00
- Respond “Checked”
FINAL COCKPIT PREPARATION-PAGE 7
GROUND PHASE EVENT
Before taxi checklist
CM 1
CM 2
- Command “Before taxi checklist” READ: RESPONSE: - “Tail prop” - “Removed and on-board” - “Cockpit door” - “Locked” - “Doors” - “Closed” - “Beacon” - “On” - “Prop brake” - “Released” - “Windshield HTG” - “On” - “Anti-icing” - “ON or OFF” (As RQD) - “CL’s” - “Auto” or “Max RPM” - “Flaps” - “15/15” - “Antiskid” - “Tested” - “Radar” - “Tested and standby” - Announce “Before taxi checklist completed”
- “Checked”
ATR-72 SOP’s
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 8
GROUND PHASE EVENT
CM 1
Before taxi checklist completed
- Command “Request taxi clearance”
Taxi clearance obtained
-
Taxi
Obtain taxi release from ground staff Check left side clear and announce “Left side clear. Check right side”
- Taxi & TO light select to ON - Conduct normal brake check - Conduct emergency brake check and announce “Left side brake checked. Check right side”
CM 2
- Request taxi clearance from ATC
- Check right side clear and announce “Right side clear”
- Conduct normal brake check and announce “Right side brake checked” - Receive ATC clearance
ATC clearance obtained PF departure briefing to include: • • •
PF reviews key points from ATC clearance and if necessary reviews the takeoff briefing
- PF reviews key points from ATC clearance and if necessary reviews the takeoff briefing
Departure clearance is……….. FL…………. Squawk……
ATR-72 SOP’s
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 9
GROUND PHASE EVENT
Taxi checklist
CM 1
-
CM 2
Command “Taxi checklist” READ: RESPONSE: - “Taxi & TO lights”
- “ON” - “Brakes”
-
“Checked”
-
“Closed”
-
“ _______ Set”
-
“Tested”
-
“Completed”
-
“Checked”
-
Receive Purser report
- “Cockpit com hatch”
- “AFCS” - “Takeoff configuration” - “Departure briefing” - Announce “Taxi checklist completed”
Purser report to Captain “Cabin ready for takeoff”
ATR-72 SOP’s
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE10
GROUND PHASE EVENT
Before takeoff actions – Line up and wait
CM 1
- Command “Before takeoff actions” -
Check left spoiler by looking outside and announce “Left spoiler up”
-
Check spoiler light panel and announce “Light on” Check full rudder travel to the left then to the right and announce “Rudder checked” Set rudder CAM (Rudder pedals centered and brief action on rudder trim) Line up runway HDG and check lateral FD bars centered Select radar as required
-
PA announcement
ATR-72 SOP’s
15 Jul 09 - REV 00
CM 2
- Release gust lock and announce “Flight control check” - Turn control wheel to full forward and to the left - Check spoiler light panel and announce “Light on” - Turn control wheel to full forward and to the right - Check right spoiler by looking outside and announce “Right spoiler up” - Pull control wheel without any bank input fully backwards and release to the neutral position - Select ENG 1 BLEED and ENG 2 BLEED as required with FLOW to NORM - Select Probe HTG to ON - Select start rotary selector CONT RELIGHT as RQD - Select LAND L, LAND R, TAXI & TO and STROBE lights ON - Press TO INHI on CCAS - Select transponder to ALT - Select TCAS to AUTO - Make PA announcement “Cabin crew be seated for takeoff” - Announce “Before takeoff actions completed”
FINAL COCKPIT PREPARATION-PAGE11
GROUND PHASE EVENT
Before takeoff checklist
CM 1
-
CM 2
Command “Before takeoff checklist” READ: RESPONSE:
- “Gust lock” -
“Released” - “Flight controls – Right side checked”
-
“Left side checked”
-
“ON” or “OFF” (As RQD)
-
“Normal”
- “Bleed valves” - “Air flow” - “ Probe HTG” - “Continuous relight”
- “ ON” - “External lights” -
“ON or OFF” (As RQD)
-
“ON”
-
“Takeoff inhibit”
-
“Standby” or “On” (As RQD)
-
“ALT”
-
“Centered and CAM”
- “CCAS” - “Radar” - “Transponder” - “Rudder” - “TCAS” - “FD bars” - “AUTO” -
ATR-72 SOP’s
“Centered”
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE12
GROUND PHASE EVENT
CM 1
Before takeoff checklist (continued)
- “PA” -
“Completed”
-
“Checked”
- Announce “Before takeoff checklist completed”
Takeoff clearance
Takeoff run
CM 2
- Receive takeoff clearance and announce “Cleared for takeoff. Wind 0 _____ /______knots” - Announce “Takeoff, timing, flight control left or right” -
Advance PL’s to notch position and announce “Notch”
- Select clock to RUN and CHR - Hold control column forward and into wind - Check ATPCS ARM light illuminates and announce “ATPCS arm” - Check FDAU bars on RTO value - Check engine parameters TQ, NP, ITT, NH oil and announce “Power set” - Continue to scan airspeed and engine instruments throughout takeoff and announce “Engine instruments checked normal” - Announce “Seventy knots”
At 70 Kt Note: If CM2 is PF takeoff power is set by CM1. CM1must keep his/her hands on the PL’s until reaching V1 in order to be ready to retard the PL’s in the case of an aborted takeoff
ATR-72 SOP’s
-
Release nose wheel steering and announce “I have control” or “You have control” (CM2 as PF)
15 Jul 09 - REV 00
- Confirm “You have control” or “I have control” (CM2 as PF)
FINAL COCKPIT PREPARATION-PAGE13
FLIGHT PHASE EVENT
PF
PNF
V1
-
Check speed Release hand from PL’s
- Announce “V1”
VR
-
Check speed Rotate aircraft
- Announce “Rotate”
Positive climb established on VSI - Command “Gear up” -
Command “Yaw damper on”
-
Check no lights on LDG GEAR panel and respond “Checked” - Command “Taxi light off”
Acceleration altitude - Command “Speed to white bug” or “Speed to red bug” (icing conditions) - Check selected speed on ADU and respond “Checked” Speed at white or red bug speed
ATR-72 SOP’s
-
Check ASI speed and command “Flaps zero”
-
Check flap indicator shows 0 and respond “Checked”
0
15 Jul 09 - REV 00
- Announce “Positive climb” - Select gear lever to the UP position and announce “Gear up selected” - Engage yaw damper and announce “Yaw damper on” - Check no lights on LDG GEAR panel and announce “Gear up set” - Select TAXI & TO light OFF and announce “Taxi light off” - Announce “Acceleration altitude” - Increase IAS to white or red bug speed (as applicable) and announce “White bug speed set” or “Red bug speed set” (as applicable) - Announce “White bug” or “Red bug” (as applicable) 0 - Select flap lever to 0 and announce “Flaps zero selected” 0 - Check flap indicator shows 0 and announce “Flaps zero set” FINAL COCKPIT PREPARATION-PAGE14
FLIGHT PHASE EVENT
PF
Command “Climb sequence”
Climb sequence
-
Climb
- Command “Speed 170 knots” or “White bug” (obstacle clearance) or “Red bug” (icing conditions) - Check selected speed on ADU and respond “Checked”
After takeoff checklist
-
PNF
- Set PWR MGT to CLB - Retard CL’s to 86% - Select ENG BLEED 1 and ENG BLEED 2 to ON (if not already selected ON prior to takeoff) - Select start rotary selector as required and announce “Climb sequence completed” - Select speed as requested and announce “170 knots set” or “White bug set” or “Red bug set”
Command “After takeoff checklist” READ: RESPONSE:
- “Landing gear”
-
“Up”
- “Taxi light”
-
“Off”
- “Power management and condition levers”
-
“Climb auto” or “Climb 86%” - “Flaps”
-
ATR-72 SOP’s
“Zero, zero”
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE15
FLIGHT PHASE EVENT
PF
PNF
- “Bleed valves”
After takeoff checklist (continued) -
“On” - “Continuous relight”
- “ON or OFF” (As RQD) - Announce “After takeoff checklist completed to altimeters”
-
“Checked”
-
At 5,000 FT select SEAT BELTS sign OFF to signal cabin crew that cabin service activities can be commenced. If not possible to select the SEAT BELTS sign OFF due turbulence advise Purser by interphone to remain seated or can commence service with the SEAT BELTS sign ON
-
Set QNE (29.92/1013) and cross check and announce “_____Flight level, now”
Transition altitude
10,000 FT or FL100
-
Check crossing 10,000 FT or FL100 and command “Landing lights off”
-
Check landing lights off and respond
After takeoff checklist (continued) RESPONSE:
ATR-72 SOP’s
-
“Set QNH 29.92/1013”
-
“Checked”
“Checked”
- Announce “Transition altitude”
- Set QNE (29.92/1013) and cross check. Announce “_____Flight level” (call out deviation) - Announce “Crossing ten thousand” or “Crossing flight level 100” - Select landing lights off and announce “Landing lights off” READ: - “Altimeters” - “Memo panel”
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 16
FLIGHT PHASE EVENT
PF
PNF - “LAND lt”
- “OFF”
-
1,000 FT to any assigned altitude or flight level (climb or descent)
- Announce “After takeoff checklist completed”
“Checked”
- Announce “One thousand to go” -
Level off (climb or descent)
Check EADI with amber light ON and respond “Checked”
-
Check ALT* on ADU illuminates and respond “Checked” - Check ALT HOLD illuminates on ADU and respond “Checked”
At target speed
ATR-72 SOP’s
-
Set speed inner bug and respond “Checked”
-
Check TQ bug set to target % and respond “Checked”
-
Select PWR MGT to CRZ and command “Power management to cruise”
15 Jul 09 - REV 00
- Check ALT* illuminates on ADU and announce “ALT star” - Check ALT HOLD illuminates on ADU and announce “Altitude hold” - Check SAT, compute delta ISA and cruise parameters. Announce “Cruise target speed____knots” - Set speed inner bug - Announce “Cruise target TQ___%, set” - Set TQ bug to target %
- Check PWR MGT to CRZ and respond “Checked”
FINAL COCKPIT PREPARATION-PAGE 17
FLIGHT PHASE EVENT
Cruise checklist
PF
- Command “Cruise checklist” RESPONSE:
Approach briefing to include: • TOD, weather and runway information • Read Landing Data card details Brief in accordance with 2.2.1 •
ATR-72 SOP’s
READ:
-
“Cruise”
- “Power management”
-
“OFF” or “ON” (as required)
- “Seat belts”
-
Descent preparation
PNF
“Observed” If entering icing conditions: ■ Select anti-ice “ON” ■ Set CL’s to “AUTO/ 82%” (ATR-72-500) ■ Set CL’s to “Set 86%” ■ Set CL’s to “AUTO/ 86%” (ATR-72-500PEC) ■ MIN icing speed “observed”
-
“Checked”
-
Compute top of descent
-
Set speed bugs * DA (DH) set Set NAVAIDS GA TQ bugs set (100%)
- Transfer monitoring flight path - Make Approach briefing * The DH is only to be set for precision approach for reference only
15 Jul 09 - REV 00
- “Flight conditions”
- Announce “Cruise checklist completed”
- Obtain airport landing information (ATIS or ATC) and complete Landing Data card - Set speed bugs - * DA (DH) set - Set NAVAIDS
- Monitoring flight path (navigate) - Confirm briefing
* The DH is only to be set for precision approach for reference only
FINAL COCKPIT PREPARATION-PAGE 18
FLIGHT PHASE EVENT
PF
Top of descent
- Command “Request descent”
Descent clearance obtained
-
- Request descent clearance
Select cleared FL/Altitude on ADU Select calculated rate of descent on ADU Select RCL on CCAS SEAT BELTS sign ON (PIC only) - Make PA announcement “Cabin crew prepare for landing”
PA announcement
Descent checklist
PNF
-
Command “Descent checklist” READ: RESPOND: - “CCAS”
-
“Recall”
-
“ _______ Left side set”
- “Landing data – Right side set” - “GA TQ bugs” -
“ ______%Set”
-
“On”
-
“Completed”
- “Seat belts” - “PA” - “Approach briefing” - “Completed” - Announce “Descent checklist complete” -
ATR-72 SOP’s
“Checked”
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 19
FLIGHT PHASE EVENT
Descent path
PF
PNF
0
-
Maintain 3 path whenever possible
-
Check crossing 10,000 FT or FL100 and command “Ldg lts ON, Cont relight “ON or OFF” (As RQD)
10,000 FT or FL100
- Check LAND L and LAND R LIGHTS ON - Check CONT relight ON or OFF and response: - “Checked” Transition level or when cleared to an altitude by ATC
-
Approach checklist (after setting QNH)
- Command “Approach checklist”
Set QNH and cross check and respond “____feet, now”
- Announce “Crossing ten thousand” or “Crossing flight level 100” - Select LAND L and LAND R lights ON - Select CONT relight as RQD(ATR72-200) and announce “Ldg lights ON and Cont relight ON or OFF”
- Announce “Transition level” - Set QNH and cross check. Announce “____feet” (call out deviation)
READ: RESPONSE: - “Landing Lights” (bellow FL 100) - “On” - “Altimeters” -
“QNH____set. Cross checked”
-
“Checked”
-
“Checked on or off”
- “Cabin altitude/ELEVATION” - “Icing angle of attack light” (speed versus)
ATR-72 SOP’s
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 20
FLIGHT PHASE EVENT
PF
Approach checklist (continued)
- “Continuous relight” -
“ON or OFF” (As RQD)
-
“Checked”
Radar vectoring
-
Select assigned altitude(s) and heading(s) on ADU and announce “Altitude____set” and/or “Heading _____set”
PRECISION APPROACH: When clearance for approach, or last heading to intercept final course is received:
-
Select APP mode on ADU and check LOC and GS armed, announce “Approach mode armed”
Both left and right VLF selected: PF on ILS PNF on VOR frequency. ADF’s selected to OM frequency and audio selector panel MKR switch selected ON When radio altimeter displays at 2,500 FT LOC*
GS*
ATR-72 SOP’s
PNF
-
- Announce “Approach checklist complete”
- Confirm ADU settings and respond “Checked”
- Check APP mode on ADU and respond “Checked” -
Crosscheck NAV settings
Crosscheck NAV settings - Announce “Radio altitude alive”
-
Check and respond “Checked”
Check LOC* on ADU and EHSI and respond “Checked” - Select runway heading and announce “Runway heading____set” - Select second VLF on ILS frequency
- Check LOC* on ADU and EHSI and announce “Loc star”
-
Check GS* on ADU and EHSI and respond “Checked” - Select missed approach altitude on ADU and announce “Missed approach ____feet set”
15 Jul 09 - REV 00
- Check runway heading and respond “Checked”
- Check GS* on ADU and EHSI and announce “Glide slope star”
- Check missed approach altitude and respond “Checked”
FINAL COCKPIT PREPARATION-PAGE21
FLIGHT PHASE EVENT
PF
PNF
FAF
Altitude 1,800 FT (AGL) and IAS not above 180 Kt
Speed 170 Kt
-
Cross check altitude and respond “Checked_____feet”
-
PL retard to FI position and command “Flaps 15”
-
Check flap indicator shows 15 and respond “Checked”
0
- Command “Gear down”
- Cross check altitude and announce “Final altitude checked”
- Check IAS not above 180 Kt and announce “Speed checked” 0 - Select flap lever to 15 position and announce “Flaps 15 selected” - Check flap indicator shows 15 0 and announce “Flaps 15 set”
- Check IAS not above 170 Kt and announce “Speed checked” - Select gear lever to the DOWN position and announce “Landing gear down selected” - Set PWR MGT to MCT(3s) then TO - Select TAXI & TO light to ON - Check start rotary selector CONT RELIGHT AS RQD - Check CL 1 and CL 2 to AUTO-100% or MAX RPM-100% - Check landing gear down with three green lights and announce “Landing gear down, three green on”
- Check landing gear down with three green lights and respond “Checked”
ATR-72 SOP’s
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 22
FLIGHT PHASE EVENT
Speed 150 Kt
PF
PNF
- Command “Flaps 30”
0
- Check flap indicator shows 30 and respond “Checked”
- Make PA announcement “Cabin crew be seated for landing”
PA announcement
Before landing checklist
- Check IAS not above 150 Kt and announce “Speed checked” 0 - Select flap lever to 30 position and announce “Flaps 30 selected” 0 - Check flap indicator shows 30 and announce “Flaps 30 set”
-
Adjust PL to maintain Vapp ≥Vapp + 10 Kt
- Command “Before landing checklist” READ: RESPONSE: - “Landing gear” -
“Down three greens”
-
“ON”
-
“30/30”
-
“Takeoff”
-
“Auto-100%” or “MAX RPM-100%”
-
“ON”
- “TLU green light” - “Flaps” - “Power management” - “CL’s” - “External lights”
ATR-72 SOP’s
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 23
FLIGHT PHASE EVENT
PF
PNF
- “PA” -
“Completed”
-
“Checked”
Altitude 1,000 FT AGL In IMC conditions • Rate of descent not greater than 1,000 fpm Speed Vapp -0 to +15 Kt • • No abrupt power changes • Localizer within ONE dot Glide slope within ONE dot •
- Respond “Checked continue” or - “Correcting ______”(name of deviation(s))
- Announce “Before landing checklist completed” - Check 1,000 FT AGL and announce “One thousand stable” or - “One thousand unstable______” (name of deviation(s)) - If deviation continues announce “_____(name of deviation(s)) unstable” - If deviation(s) not corrected after two announcements, announce - “Go-around”
- Respond “Going around”
- Announce “Ground contact” or “Approach lights in sight” or “Runway in sight”
- Respond “Checked continue”
- Announce “Five hundred to minimum”
Final phase During the final phase when visual reference is established it should be announced
500 FT above minimum Expand instrument scan to include outside visual cues
- Respond “Checked”
- Announce “One hundred to minimum”
100 FT above minimum - Respond “Checked” ATR-72 SOP’s
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 24
FLIGHT PHASE EVENT
PF
PNF
- Announce “Minimum”
At DA - Respond “Landing” (if visual contact established) or “Go-around” (no visual contact established) Altitude from 100 FT (AGL)
Touchdown
0
-
Maintain 3 glide slope
-
Visual flare to touchdown. Reduce PL’s to FI position.
-
Select PL’s to GI position
-
PL’s to REV (as required)
Both LO PITCH lights illuminated
- Announce(not RQD if EGPWS calls): “One hundred” “Fifty” “Forty” “Thirty” “Twenty” “Ten”
- Check IDLE GATE - Check both LO PITCH lights ON and announce “Low pitch lights on”
- Announce “Seventy knots” Speed 70 Kt CM2 GROUND PHASE EVENT
ATR-72 SOP’s
CM1
- Command “Hold flight column”
- Hold flight control wheel as required and announce “Flight column hold”
- Respond “I have control”
- Confirm that CM1 takes control of the aircraft and announce “You have control”
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 25
FLIGHT PHASE EVENT NON - PRECISION APPROACH:
Approaching holding over IAF
Clearance for non-precision approach obtained
Over station
PF
-
Set inbound holding course on EHSI Maintain holding speed of 175 Kt Maintain MSA or ATC assigned altitude
-
Set outbound course on EHSI and announce “Outbound course set” Set next step-down altitude on ADU and announce “Pre-set altitude_____feet”
-
- Command “Timing______minutes” - Initiate a descent at 1,000 fpm or a constant 0 descent profile of 3
Outbound procedure (1.000 FT to step-down altitude)
-
Check altitude and respond “Checked”
ALT* (Step-down altitude)
-
Check ALT* on ADU and respond “Checked”
- Check ALT HOLD on ADU and respond “Checked” - Set next step-down altitude or FAF altitude on ADU (after * disappears) and announce “Pre-set altitude_____feet” Inbound turn
ATR-72 SOP’s
-
PNF
- Check selected course and respond “Checked” - Check pre-set altitude and respond “Checked” - Select CHR on the clock and respond “Timing”
- Check altitude alert audio signal and amber light and announce “One thousand to go” - Check ALT* on ADU and announce “ALT star” - Check ALT HOLD on ADU and announce “ALT hold”
- Check pre-set altitude and respond “Checked” - Announce “Time____out” - Select final course and announce “My side_____set”
Select final course and announce “Final course_____set” 15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 26
FLIGHT PHASE EVENT
When radio altimeter displays at 2,500 FT Inbound procedure – Established on final course (IAS 180 Kt)
PF
PNF
- Check and respond “Checked” - PLs retard to FI - Command “Flaps 15”
0
-
Check flap indicator shows 15 and respond “Checked” - Command “Gear down” Speed 170 Kt
- Announce “Radio altimeter alive”
-- Check IAS not above 180 Kt and announce “Speed checked” 0 - Select flap lever to 15 position and announce “Flaps 15 selected” 0 - Check flap indicator shows 15 and announce “Flaps 15 set” - Check IAS not above 170 Kt and announce “Speed checked” - Select gear lever to the DOWN position and announce “Landing gear down selected” - Set PWR MGT to MCT(3s) than TO - Select TAXI & TO light to ON - Check start rotary selector: CONT RELIGHT AS RQD - Check CL1 and CL2 to AUTO or 100%
- Check landing gear down with three green lights and respond “Checked” - Command “Flaps 30” Speed 150 Kt 0
- Check flap indicator shows 30 and respond “Checked”
ATR-72 SOP’s
15 Jul 09 - REV 00
- Check landing gear down with three green lights and announce “Landing gear down, three green on” - Check IAS not above 150 Kt and announce “Speed checked” 0 - Select flap lever to 30 position and announce “Flaps 30 selected” 0 - Check flap indicator shows 30 and announce “Flaps 30 set”
FINAL COCKPIT PREPARATION-PAGE 27
FLIGHT PHASE EVENT
PF
- Make PA announcement “Cabin crew be seated for landing”
PA announcement
-
Before landing checklist
PNF
Adjust PL to maintain Vapp ≥Vapp + 10 Kt
- Command “Before landing checklist” READ: RESPONSE: - “Landing gear” -
“Down three greens”
-
“On”
-
“30/30”
-
“Take off”
-
“Auto-100%” or “MAX RPM”
- “TLU green light” - “Flaps” - “Power management” - “CL’s” - “External lights” - “ON” - “AP” - “Disengaged” - “PA”
ATR-72 SOP’s
-
“Completed”
-
“Checked”
- Announce “Before landing checklist completed”
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 28
FLIGHT PHASE EVENT
PF
- Announce “Final approach fix”
FAF/FAP with MDA pre-selected Confirm FAF and respond “Checked” Command “Timing______minutes” (if required) Initiate a descent at 1,000 fpm or a constant descent 0 profile of 3 - Announce “Rate of descent _____feet per minute set”
-
Altitude 1,000 FT (AGL) In IMC conditions Rate of descent not greater than • 1,000 fpm Speed Vapp -0 to +15 Kt • • No abrupt power changes
PNF
- Respond “Checked continue” or - “Correcting ______”(name of deviation(s))
- Select CHR on the clock and announce “Timing” (if required)
- Check rate of descent on ADU and respond “Checked” - Check 1,000 FT (AGL) and announce “One thousand stable” or - “One thousand unstable______” (name of deviation(s)) - If deviation continues announce “_____(name of deviation(s)) unstable” - If deviation(s) not corrected after two announcements, announce - “Go-around”
- Respond “Going around”
Final phase During the final phase when visual reference is established it should be announced
ATR-72 SOP’s
- Respond “Checked continue”
15 Jul 09 - REV 00
- Announce “Ground contact” or “Approach lights in sight” or “Runway in sight”
FINAL COCKPIT PREPARATION-PAGE 29
FLIGHT PHASE EVENT
PF
PNF
- Announce “Five hundred to MDA”
500 FT above MDA - Respond “Checked” Expand instrument scan to include outside visual cues
- Announce “One hundred to minimum”
100 FT above MDA - Respond “Checked” Minimum MDA -
Check ALT* illuminates on ADU and respond “Checked” - Check ALT HOLD illuminates on ADU and respond “Checked” - Select missed approach altitude on ADU and announce “Missed approach altitude set”
- Check ALT* illuminates on ADU and announce “ALT star. MDA” - Check ALT HOLD illuminates on ADU and announce “Altitude hold”
- Confirm missed approach altitude on ADU and respond “Checked” - Advise PF of distance or time to MAP by announcing “___miles to missed approach point” or “____seconds to missed approach point”
- Respond “Checked” - Announce “Missed approach point”
MAP - Respond “Landing” (if visual contact established) or “Go-around” (no visual contact established) ATR-72 SOP’s
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 30
FLIGHT PHASE EVENT
Altitude from 100 FT (AGL)
Touchdown
PF 0
-
Maintain 3 glide slope
-
Visual flare to touchdown. Reduce PL’s to FI position.
-
Select PL’s to GI position
Both LO PITCH lights illuminated
- Announce(not RQD if EGPWS calls): “One hundred” “Fifty” “Forty” “Thirty” “Twenty” “Ten”
- Check IDLE GATE - Check both LO PITCH lights ON and announce “Low pitch lights on”
-
PL’s to REV (as required) - Announce “Seventy knots”
Speed 70 Kt
GROUND PHASE EVENT
CM1
- Command “Hold flight column”
-
ATR-72 SOP’s
PNF
Respond “I have control”
15 Jul 09 - REV 00
CM2
- Hold flight control wheel as required and announce “Flight column hold” - Confirm that CM1 takes control of the aircraft and announce “You have control”
FINAL COCKPIT PREPARATION-PAGE 31
7FLIGHT PHASE EVENT CIRCLING APPROACH (When ever weather conditions permit always use higher visual circuit pattern)
MAP Any runway environment in sight. For a circling approach the required visual reference are The runway environment • • Runway end/or runway lights • Approach lights In view at all time
PF
-
Check ALT* illuminates on ADU and respond “Checked” - Check ALT HOLD illuminates on ADU and respond “Checked” - Select missed approach altitude on ADU and announce “Missed approach altitude set”
PNF - Check ALT* illuminates on ADU and announce “ALT star. MDA” - Check ALT HOLD illuminates on ADU and announce “Altitude hold”
- Confirm missed approach altitude on ADU and respond “Checked” - Announce “Missed approach point”
-
Respond “Circling” (if visual contact established) or “Go-around” (no visual contact established)
-
Set heading 45 from runway heading and command “Heading____, timing 30 seconds”
-
0
Turn on downwind heading and announce “Downwind heading set” (adjust for wind)
- Start timing and respond “Timing” - At the end of 30 seconds announce “30 seconds time out”
Downwind leg
Abeam threshold
- Command “Timing____seconds” (for reference use three seconds for every 100 FT ± wind component)
-
Keep runway in sight
- Check downwind heading and respond “Checked” Start timing and respond “Timing” - At the end of 30 seconds announce “___seconds time out”
Turning base
ATR-72 SOP’s
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 32
FLIGHT PHASE EVENT
Commencing descent
PF
PNF
- Command “Flaps 30”
0
- Check flap indicator shows 30 and respond “Checked”
- Check IAS not above 150 Kt and announce “Speed checked” 0 - Select flap lever to 30 position and announce “Flaps 30 selected” 0 - Check flap indicator shows 30 and announce “Flaps 30 set” - Make PA announcement “Cabin crew be seated for landing”
PA announcement Adjust PL to maintain Vapp ≥Vapp + 10 Kt
Before landing checklist
- Command “Before landing checklist” READ:
RESPONSE: -
“Down three greens”
-
“ON”
-
“30/30”
-
“Takeoff”
-
“Auto-100%” or “MAX RPM”
-
“ON”
- “TLU green light” - “Flaps” - “Power management” - “CL’s” - “External lights” - “AP”
- ‘Disengaged”
ATR-72 SOP’s
- “Landing gear”
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 33
FLIGHT PHASE EVENT
PF
PNF - “PA”
400 FT (AGL) on final Rate of descent not greater than 1,000 fpm Speed Vapp -0 Kt to +15 Kt No abrupt power lever changes
-
“Completed”
-
“Checked”
- Announce “Before landing checklist completed”
•
-
•
-
Respond “Landing” or “Go-around”
-
Maintain 3 glide slope
•
0
Altitude from 100 FT (AGL)
Touchdown
-
Visual flare to touchdown. Reduce PL’s to FI position. - Select PL’s to GI position
Both LO PITCH lights illuminated
-
Speed 70 Kt GROUND PHASE EVENT
PL’s to REV (as required)
CM1
- Command “Hold flight column”
-
ATR-72 SOP’s
Respond “I have control”
15 Jul 09 - REV 00
- Announce “400 feet stable” or - “400 feet unstable go-around” - Announce(not RQD if EGPWS calls): “One hundred” “Fifty” “Forty” “Thirty” “Twenty” “Ten” - Check IDLE GATE - Check both LO PITCH lights ON and announce “Low pitch lights on”
- Announce “Seventy knots” CM2 - Hold flight control wheel as required and announce “Flight column hold” - Confirm that CM1 takes control of the aircraft and announce “You have control” FINAL COCKPIT PREPARATION-PAGE 34
FLIGHT PHASE EVENT
PF
PNF
VISUAL CIRCUIT PATTERN
Downwind at 1,500 FT (AGL). Speed 180 Kt Upwind end of runway
- PLs retard to FI - Command “Flaps 15”
-
Speed 170 Kt
0
Check flap indicator shows 15 and respond “Checked”
- Command “Gear down” - Adjust PLs to maintain IAS=140Kt
- Check IAS not above 180 Kt and announce “Speed checked” 0 - Select flap lever to 15 position and announce “Flaps 15 selected” 0 - Check flap indicator shows 15 and announce “Flaps 15 set”
- Check IAS not above 170 Kt and announce “Speed checked” - Select gear lever to the DOWN position and announce “Landing gear down selected” - Set PWR MGT to MCT(3s) than TO - Select TAXI & TO light to ON - Check start rotary selector: CONT RELIGHT As RQD - Check CL1 and CL2 to AUTO or 100% - Check landing gear down with three green lights and announce “Landing gear down, three green on”
- Check landing gear down with three green lights and respond “Checked”
ATR-72 SOP’s
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 35
FLIGHT PHASE EVENT
PF
PNF
Abeam threshold. Speed 140 Kt
- Command “Timing____seconds” (for reference use three seconds for every 100 FT ± wind component)
Base leg
-
0
Select HDG to 90 to final, Retard PLs to Vapp commence descent and Command “Flaps 30”
0
- Check flap indicator shows 30 and respond “Checked” - Adjust PLs to maintain Vapp ≥ Vapp+10kt
- Check IAS not above 150 Kt and announce “Speed checked” 0 - Select flap lever to 30 position and announce “Flaps 30 selected” 0 - Check flap indicator shows 30 and announce “Flaps 30 set”
- Make PA announcement “Cabin crew be seated for landing”
PA announcement
Before landing checklist
Start timing and respond “Timing” - At the end of timing announce “___seconds time out”
- Command “Before landing checklist” READ: RESPONSE: - “Landing gear” -
“Down three greens”
-
“On”
-
“30/30”
-
“Takeoff”
-
“Auto-100%” or “MAX RPM”
-
“On”
- “TLU green light” - “Flaps” - “Power management” - “CL’s” - “External lights”
ATR-72 SOP’s
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 36
FLIGHT PHASE EVENT
PF
PNF - “AP”
- “Disengaged” - “PA”
Turning final
500 FT (AGL) on final Rate of descent not greater than 1,000 fpm Speed Vapp -0 Kt to +15 Kt No abrupt power lever changes •
• •
Altitude from 100 FT (AGL)
-
“Completed”
-
“Checked”
-
Set HDG to runway heading
- Announce “Before landing checklist completed”
-
Respond “Landing” or “Go-around”
-
Maintain 3 glide slope
-
Visual flare to touchdown. Reduce PL’s to FI position.
-
Select PL’s to GI position
-
0
Touchdown ATR-72 SOP’s
15 Jul 09 - REV 00
- Announce “500 feet stable” or - “500 feet unstable go-around”
- Announce (not RQD if EGPWS calls): “One hundred” “Fifty” “Forty” “Thirty” “Twenty” “Ten”
- Check IDLE GATE
FINAL COCKPIT PREPARATION-PAGE 37
FLIGHT PHASE EVENT
PF
Both LO PITCH lights illuminated
- Check both LO PITCH lights ON and announce “Low pitch lights on” -
PL’s to REV (as required)
- Announce “Seventy knots”
Speed 70 Kt
GROUND PHASE EVENT
CM1
- Command “Hold flight column”
-
ATR-72 SOP’s
PNF
Respond “I have control”
15 Jul 09 - REV 00
CM2
- Hold flight control wheel as required and announce “Flight column hold” - Confirm that CM1 takes control of the aircraft and announce “You have control”
FINAL COCKPIT PREPARATION-PAGE 38
FLIGHT PHASE EVENT
PF
PNF
GO-AROUND
Go-around required
- Command “Go-around” and simultaneously: PL’s advance to the RAMP position Press the GA switch 0 Rotate aircraft to go-around attitude (9 ) Command “Flaps 15” • • • •
Positive climb established on VSI - Command “Gear up”
Established in stable climb
Check flap indicator shows 15 and no lights on LDG GEAR panel and respond “Checked”
-
Command “Taxi light off”
- Command “Heading, low bank IAS”
-
ATR-72 SOP’s
0
-
- Check PL’s at the RAMP position and announce “Go-around power set” 0 - Select flap lever to 15 position and announce “Flap 15 selected”
- Announce “Positive climb” - Select gear lever to the UP position and announce “Gear up selected” 0 - Check flap indicator shows 15 and no lights on LDG GEAR panel and announce “Flaps 15, gear up set” - Select TAXI & TO light to OFF and announce “Taxi light off”
- Select HDG, BANK to low and adjust IAS to VGA on ADU and announce “Heading, low bank and IAS set”
Check settings and respond “Check”
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATIONPAGE 39
FLIGHT PHASE EVENT
PF
PNF
- Command “Speed to white bug” or “Speed to red bug” (icing conditions)
- Announce “Acceleration altitude” - Increase IAS to white or red bug speed (as applicable) and announce “White bug speed set” or “Red bug speed set” (as applicable)
Acceleration altitude
-
Check selected speed on ADU and respond “Checked”
Speed at white or red bug speed
PL’s back to NOTCH position
Climb sequence
ATR-72 SOP’s
-
Check ASI speed and command “Flaps zero”
-
Check flap indicator shows 0 and respond “Checked”
-
- Announce “White bug” or “Red bug” (as applicable) 0 - Select flap lever to 0 and announce “Flaps zero selected” 0 - Check flap indicator shows 0 and announce “Flaps zero set”
0
Retard PL’s to NOTCH position and announce “Power levers back to notch”
- Command “Climb sequence”
15 Jul 09 - REV 00
- Check PL’s at NOTCH position and announce “Notch checked”
- Set PWR MGT to CLB - Retard CL’s to 86% - Select ENG BLEED 1 and ENG BLEED 2 to ON (if not already selected ON prior to takeoff) - Select start rotary selector as required and announce “Climb sequence completed”
FINAL COCKPIT PREPARATION-PAGE 40
GROUND PHASE EVENT
CM 1
CM 2
AFTER LANDING:
Below 70 Kt
-
Maintain direction with nose-wheel steering Use brakes and reverse as required
Vacating runway
- Command “Gust lock engage”
Runway vacated
- Command “After landing checklist”
- Hold control wheel as required
- Engage gust lock (flight controls to neutral) - Select clock to HLD position
- Complete after landing scan as follows: TCAS – Standby Transponder, ADF 1 and 2 and Com 2 – Off 0 Flaps – 0 Trims – Reset EHSI 1 and 2, EADI 1 and 2, RA, radar contrast – Off TQ Bug – Set 90% ADU – Standby ALT pre-select – 0 VOR 1 and 2 – Off LAND L, LAND R and STROBE lights – Off Cont relight Off Anti-icing level 1 – Off • •
• • •
• • • • •
• •
ATR-72 SOP’s
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 41
GROUND PHASE EVENT
Engine cool down time (PL between FI and GI for one to two minutes
CM 1
-- Command “CL number 1 to feather”
CM 2
- Select CL 1 to FTR position (timing 20 seconds for oil check), - Select ENG 1 BLEED to OFF and announce “CL number one to feather”
- Respond “Checked” Engine 1 fuel shut off
- Command “CL number 1 to shut off” (After 1-2min with PL between FI and GI)
- Respond “Checked”
-
Select CL 1 to FUEL SO position, Check hydraulic crossfeed-open Reset fuel used(FU) Select PUMP ENG 1 to OFF Announce “CL number one to shut off”
- Silently read and cross check After Landing Checklist and when complete announce “After landing checklist completed” - Respond “Checked” Marshall in sight
-
Follow marshaller’s instructions
-
Select TAXI & TO light to OFF Set parking brake to ON Select CL 2 to FTR position Open communication hatch
PARKING:
At the final parking position
ATR-72 SOP’s
15 Jul 09 - REV 00
FINAL COCKPIT PREPARATION-PAGE 42
GROUND PHASE EVENT
Propeller brake on
CM 1
-
Engine 2 fuel shut off (On night flights wait for GPU to be connected before shutting down engine 2)
-
Check green READY light illuminates and NP stable (20 seconds timing) Select PROP BRAKE switch ON and check PROP BRK light illuminated Select BEACON to OFF Select SEAT BELTS to OFF Select EMERG EXIT LT to DISARM Select ENG 2 BLEED to OFF Select CL 2 to FUEL SO position and announce “CL number 2 to shut off”
CM 2
- Check right hand side engine 2 and announce “Prop brake on”
- Select COM 1 to OFF, cockpit door main switch to OFF and oxygen MAIN SUPPLY to OFF.
Parking checklist -Command ”Parking checklist” READ: RESPONSE: - “Parking brake” -
“On”
-
“Fuel shut off”
-
“Off”
-
“On, locked”
-
“Off”
- “CL 2” - “COM 1” - “Prop brake” - “Bleed valves” - “Emergency exit lights/ Seat belts” - “Disarmed/Off” - “Beacon” -
ATR-72 SOP’s
“Off”
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FINAL COCKPIT PREPARATION-PAGE 43
GROUND PHASE EVENT
CM 1
Parking checklist (continued)
- “Fuel pumps” -
“Off”
-
“Off”
-
“Checked”
Contact ground crew and confirm chocks set
-
Release parking brake
Complete flight documentation
-
Complete Technical Log entries
-
Select BAT to OFF and announce “Battery switch off” Select NAV to OFF
-
Command “Leaving the aircraft checklist”
LEAVING THE AIRCRAFT:
Leaving the aircraft checklist
ATR-72 SOP’s
CM 2
- “Cockpit door main switch” - “Parking checklist completed”
- Complete required post flight documentation
READ:
RESPONSE:
- “Parking brake”
-
“Released”
- “NAV light”
-
“Off”
- “EXT lights”
-
“Off”
- “Battery”
- “Off”
- “Documentation”
-
“Completed”
- “Leaving the aircraft checklist completed”
-
“Checked”
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FINAL COCKPIT PREPARATION-PAGE 44
ATR – 72 STANDARD OPERATING PROCEDURES APPENDIX
ATR – 72 INTERNAL INSPECTION
PRELIMINARY COCKPIT PREPARATION
GROUND PHASE EVENT
CM 1
INTERNAL INSPECTION (Prior to the powering the aircraft with GPU)
CM 2 Lateral and overhead panel C/Bs -Check that all C/Bs are set (IN) Emergency equipment check -Exit hatch: closed handle locked & secured Escape rope stowed -L/G emergency handle: stowed and cover closed -Axe stowed -Portable fire extinguisher: secured and pressure within the green area -Check 3 gear pins stowed behind F/O seat -Protective gloves -Oxygen masks stowed (both side) -Flash lights stowed (both side) -Smoke goggles stowed (both side) -Life jackets stowed (bellow both seat) Documentation -Check on board
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GROUND PHASE EVENT
CM 1
INTERNAL INSPECTION (con’t)
CM 2 Batteries -Set BAT toggle switch to ON -Check: MFC1A and MFC2A flashes then extinguish -Check: MFC1B and MFC2B flashes then extinguish -Check EMER BUS and ESS BUS supply indication arrows illuminate -Check UNDV light extinguished PROP BRAKE(hotel mode only) -Check ON light illuminate -Check PROP BRK light illuminate on MEMO panel Landing gear -Check control lever DOWN Engine -Both EEC selected ON -Both PEC selected ON(ATR72-500) -Both PL on GI -Both CL on fuel SO
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GROUND PHASE EVENT
CM 1
INTERNAL INSPECTION (con’t)
CM 2 Parking brake -Check ACCUM. pressure(3000psi) -Use HYD AUX PUMP if necessary -Set Parking handle to PARKING-ON
Flight Controls -Check GUST LOCK engaged -Check/Set Flaps control lever to agree with actual flaps position
GPU connected (green AVAIL on)
GPU AVAIL -Push GPU AVAIL green light P/B and check that only DC GEN 1 & DC GEN 2 amber FAULT lights illuminates. Lights -NAV light ON -NO SMKG light ON -Seat Belts signs ON
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GROUND PHASE EVENT
CM 1
PRELIMINARY COCKPIT PREPARATION (Con’t)
CM 2
OVERHEAD PANEL
Annunciator light -Annunciator light switch select to TEST and check ALL lights (except Fuel LO LEVEL) illuminate. F/O wiper -Check wiper rotary selector as OFF Bleed & Air condition panel -Extinguish any white light except BLEED 1 & BLEED 2 -Select TEMP selectors to 12 o’clock Avionics ventilation -Check OVBD VALVE in AUTO position and no amber or white light
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GROUND PHASE EVENT
CM 1
PRELIMINARY COCKPIT PREPARATION (con’t)
CM 2 Oxygen panel -Check oxygen high pressure sufficient for the scheduled flight -Check PAX supply OFF -Select MAN supply ON COMP SMK Depress SMK TEST p/b to check Smoke detectors. When the test is Over, reset AVIONIX VENT EXH.MODE p/b to restart extract fan. ENG 2 FIRE Protection-test -Check FIRE HANDLE 2 IN latched -Extinguish any white light -Depress SQUIB TEST pb and check both AGENT SQUID light illuminate -Select TEST switch on FIRE , and check: ENG FIRE red lt illuminates into associated fire handle; -CCAS is activated:(CRC+MW+ENG 2 FIRE on CAP+ Red light in CL-out off S/O position) -Select TEST switch on FAULT and check both LOOP A&LOOP B light illuminate (MC+SC+LOOP light on CAP)
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GROUND PHASE EVENT
CM 1
PRELIMINARY COCKPIT PREPARATION (con’t)
CM 2 Signs panel -Check NO SMKG is to ON -Check SEAT BELTS is to ON De-icing/Anti-icing panel -Check all lights extinguished PROBS/Windshield htg panel -Check all white lights illuminated ACW electric panel -Check all white lights extinguished HYD panel -Check all white light extinguished -BLUE & GREEN PUMP LO PR lt illuminates EMER LOC XMTR -Check switch AUTO, guarded External lights -Check NAV light ON -WING & LOGO lights ON (night flights only)
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GROUND PHASE EVENT
CM 1
PRELIMINARY COCKPIT PREPARATION (con’t)
CM 2 PROP BRK (engaged ON) -Check ON lt illuminate(MEMO panel also) -UNLK lt extinguished DC/AC electric panel -Check no amber light except both GEN FAULT lights CVR-TEST -With GPU can be performed only by pressing the RCDR p/b on the pedestal -Check ON blue lgt illuminates in p/b -Depress the TEST ,check needle in green arc -Stop the CVR by depressing RESET on the pedestal CAPT. Wiper -Check wiper at OFF position STORM light -As RQD STDBY Compass light -Check light is OFF
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GROUND PHASE EVENT
CM 1
PRELIMINARY COCKPIT PREPARATION (con’t)
CM 2 DOME light -As RQD MIN CAB light -Check switch is in OFF FUEL panel -ENG 1 PUMP ON=FEED LO PR1 extinguish -FUEL X-FEED on line=FEED LO PR2 extinguished -FUEL X-FEED closed = FEED LO PR 2 illuminated -ENG 2 PUMP ON=FEED LO PR2 extinguish -Both ENG FUEL PUMP select OFF DOORS Test: Depress TEST sw -Check CAB OK & SVCE OK lights illuminates (provided doors are open) Spoiler lights -Check lights OFF LDG indicators -Check LDG lever down and 3 green lights
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GROUND PHASE EVENT
CM 1
PRELIMINARY COCKPIT PREPARATION (con’t)
CM 2 TLU -Check TLU in AUTO position no amber light
ENG 1 FIRE Protection-test -Check FIRE HANDLE 1 IN latched -Extinguish any white light -Depress SQUIB TEST pb and check both AGENT SQUID light illuminate -Select TEST switch on FIRE , and check: ENG FIRE red light illuminates into associated fire handle; -CCAS is activated:(CRC+MW+ENG 1 FIRE on CAP+Red light in CL-out off S/O position) -Select TEST switch on FAULT and check Both LOOP A & LOOP B light illuminates (MC+ SC+ LOOP light on CAP)
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GROUND PHASE EVENT
CM 1
PRELIMINARY COCKPIT PREPARATION (con’t)
CM 2 PEDASTAL
Lights -Adjust lights as RQD ATPCS-test -Set ATPCS selector (Left)to ARM check ATPCS green light illuminate -Set ATPCS selector to ENG 1 check ENG 2 UPTRIM illuminate, after 2.15s ARM light extinguishes extinguish es -Do the same for ENG 2 (Right) TCAS -Test: Select ATC to STBY Select TCAS to STBY Press “TEST” button on TCAS Check aural message and visual Display on VSI. -TCAS selector stays at STBY FDEP - Enter flight number on data panel
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GROUND PHASE EVENT
CM 1
PRELIMINARY COCKPIT PREPARATION (con’t)
CM 2 TRIMS First flight of the day: -Check PITCH, ROLL and YAW trim Operation in both direction to full deflections. -Check STBY PITCH trim operation, operation , check SW guarded in OFF position Before each flight: -Check PITCH,ROLL and YAW trim -Check STBY PITCH operation, SW check guarded in OFF position. VHFs, -ON than TEST ADFs, -ON than TEST ATC -STBY than TEST IDLE GATE -Check amber band visible on the lever, and IDLE GATE FAIL amber light extinguished.
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GROUND PHASE EVENT
CM 1
PRELIMINARY COCKPIT PREPARATION (con’t)
CM 2 EMER AUDIO CANCEL -Check SW guarded and lock wired PLs -Check in GI position CLs -Check in S/O position -Engines oil press LOW warning test (First flight of the day): -Select both CLs out of S/O position -After 30s timing check: Both local alert oil LOW press CCAS OIL LOW PRESS Master warning light with CRC -Select both CLs to S/O position GUST LOCK -Check engaged ON AIL LOCK light -Check extinguished
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INTERNAL INSPECTION & PRELIMINARY COCKPIT PREPARATION PAGE 12
GROUND PHASE EVENT
CM 1
PRELIMINARY COCKPIT PREPARATION (con’t)
CM 2 F/O- EFIS control panel -TEST /SET: *Select EADI to ON (Check composite mode), *Select EADI to OFF *Select EHSI to ON (Check comp mode), *Select EADI to ON -Test DH by depressing DH TEST p/b, check RA increasing to 100ft, and three boxes on bottom right of EADI displaying O, M, I side by side -EHSI inner knob select to max radar brightness ( recommended),check WX amber light on EHSI -Select one of ADF/VOR/LNAV EHSI pointer SECURITY DOOR panel -Check FAULT lgt lit (if main SW is OFF) GPS -Select ON (if installed) CAPT- EFIS control panel -Same as for F/O side
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GROUND PHASE EVENT
CM 1
PRELIMINARY COCKPIT PREPARATION (con’t)
CM 2 F/O LATERAL CONSOLE MAINTENANCE panel -Check that rotary selector is in “NORM FLT” position before flight. EXTRACT AIR FLOW --Check forward and guarded OXIGEN MASK /Test First flight of the day : -Set audio control panel to INT -Depress and hold “PRESS TO TEST AND RESET” pb, (observe blinker momentarily turns yellow and must turn dark (if no leak ) -HOLD the ‘PRESS TO TEST AND RESET” pb, and press the red grips on each side of the hose (oxygen press inflates the harness), observe blinker momentarily turns yellow and must turn dark if there is no leak. -HOLD the “PRESS TO TEST AND RESET” pb, and select the EMERG knob(test flow) observe blinker turns yellow during the oxygen flow and must turn dark when the knob is released.
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INTERNAL INSPECTION & PRELIMINARY COCKPIT PREPARATION PAGE 14
GROUND PHASE EVENT
CM 1
PRELIMINARY COCKPIT PREPARATION (con’t)
CM 2
-Check that oxygen flow sounds through loudspeakers. -Check OXY LO PR light not lit -Set N/100% rocker lever to 100% AHRS -Check AHRS 2 light extinguished F/O SWITCHING -Check ATT/HDG, VOR/ILS, and EFIS/SG: depress then reset -Check lights extinguished AUDIO -Check AUDIO 2 light extinguished F/O INSTRUMENT PANEL VSI -Check no flags and pointer indicates zero. -Set 12nm TCAS distance and above ALTIMETER -Check no flag-Set QNH
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INTERNAL INSPECTION & PRELIMINARY COCKPIT PREPARATION PAGE 15
GROUND PHASE EVENT
CM 1
PRELIMINARY COCKPIT PREPARATION (con’t)
CM 2 E/GPWS -Push GPWS/GS pushbutton for TEST EHSI/RMI -Crosscheck heading information -Select RMI on VORs or ADFs pointers. EADI -Check no flags ASI -Check no flags, pointer indicates zero , VMO pointer indicates 250kt CLOCK -Check time, adjust if necessary CENTRAL PANEL CAB PRESS panel -Check no light illuminated -Check rotary selector facing to green mark AUTO PRESS panel TEST: Depress TEST pb, and check: -MC+SC+AIR on CAP
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GROUND PHASE EVENT
CM 1
PRELIMINARY COCKPIT PREPARATION (con’t)
CM 2
-FAUL amber light lit in MODE selector pb, -display cycling between -8800 and 18800 CAB PRESS indicators -Check : DIFF = 0 RATE= 0 ALT = pressure altitude HYDRAULIC gauges -BLUE and GREEN pressure = 0 -ACCUMULATOR pressure=3000psi ANTI-SKID -Check no light illuminated LANDING GEAR -Check lever DOWN 3 green ON BRK TEMP -Check no light illuminated FLAPS indicator -Check position according to flaps lever position and external inspection.
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INTERNAL INSPECTION & PRELIMINARY COCKPIT PREPARATION PAGE 17
GROUND PHASE EVENT
CM 1
PRELIMINARY COCKPIT PREPARATION (con’t)
CM 2 TLU -Green light lit ON STICK PUSHER -Check no light illuminated TRIM indicator -Check neutral setting for YAW and ROLL axis. MEMO panel -“NO SMOKE - SEAT BELTS” ON -“PROP BRAKE ON” (If engaged) FUEL USED -Pull knob to reset fuel used value ENG 1 & 2 instruments -Oil press = 0 -Oil temp = realistic indication -FF/FU = 0 -NH = 0 -ITT = realistic indication -NP = 0 -TQ = 0
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INTERNAL INSPECTION & PRELIMINARY COCKPIT PREPARATION PAGE 18
GROUND PHASE EVENT
CM 1
PRELIMINARY COCKPIT PREPARATION (con’t)
CM 2 ENG panel -ECU 1 & 2 ,and ATPCS pb’s depress IN STBY instruments -Check no flags -Pull knob to erect STBY horizon if necessary. -Set QNH on STBY ALT PWR MGT -Check rotary selector in TO position SYNPHR -Check synphr off white lt extinguished. PEC 1 & 2 (ENG 127F) -Check no amber light illuminated CAP -Check amber light extinguished ICE DETECT panel -Check no any white light illuminate
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INTERNAL INSPECTION & PRELIMINARY COCKPIT PREPARATION PAGE 19
GROUND PHASE EVENT
CM 1
PRELIMINARY COCKPIT PREPARATION (con’t)
CM 2 FUEL QTY panel Depress TEST pb, and check: - MC+SC+FUEL on CAP -All lights and displays -Both LO LVL lights illuminated -Both RUN green lights illuminated in fuel pumps pb
CAPT. INSTRUMENT PANEL ADC -odd days :ADC 1 -even days : ADC 2 -FAULT light extinguished TAT/SAT/TAS -Check TAT value with weather information VSI -Check no flags and pointer indicates zero. -Set 12nm TCAS distance and above
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INTERNAL INSPECTION & PRELIMINARY COCKPIT PREPARATION PAGE 20
GROUND PHASE EVENT
CM 1
PRELIMINARY COCKPIT PREPARATION (con’t)
CM 2 ALTIMETER -Check no flag-Set QNH EHSI/RMI -Crosscheck heading information -Select VORs or ADFs pointers (RMI) EADI -Check no flags ASI -Check no flags, pointer indicates zero , VMO pointer indicates 250kt CLOCK -Check time, adjust if necessary
CAPT. LATERAL CONSOLE
(E)GPWS switch -Check switch guarded in normal position -TERR amber lgt lit (when radar in OFF)
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INTERNAL INSPECTION & PRELIMINARY COCKPIT PREPARATION PAGE 21
GROUND PHASE EVENT
CM 1
PRELIMINARY COCKPIT PREPARATION (con’t)
CM 2
CAPT SWITCHING -Check ATT/HDG, VOR/ILS, EFIS SG lights extinguished AHRS -Check AHRS 1 light extinguished AUDIO -Check AUDIO 1 SEL light not lit MKR -Set MKR sw to LO OXYGEN MASK -Test (once a day), same like F/O side N/W STEERING -Check N/W steering sw. guarded on normal position.
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INTERNAL INSPECTION & PRELIMINARY COCKPIT PREPARATION PAGE 22
GROUND PHASE EVENT
CM 1
PRELIMINARY COCKPIT PREPARATION (con’t)
CM 2
GLARESHIELD FD bars -Check FD bars switches (CAPT/FO) in ON position. NAV 1 & 2 -Set ON and TEST ADU -Select HDG, LO BANK, IAS and check FD bars appearing on both EADI -Select first altitude on ALT PRESEL -Select COUPLING to PF side
ATR-72 SOP’s
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ATR-72 STANDARD OPERATING PROCEDURES
SECTION 3 ABNORMAL PROCEDURES
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
ABNORMAL PROCEDURES
TOC/P1
TABLE OF CONTENTS
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
3.1
ABNORMAL PROCEDURES
3.1/P1
3.1.1
General
3.1/P1
3.1.2
Procedures
3.1/P1
3.1.3
Notification and Verification of Condition
3.1/P3
3.1.4
Initiation of Procedure
3.1/P3
3.1.5
Reading of Checklist
3.1/P3
3.1.6
Acceleration Height
3.1/P4
3.1.7
Engine Shutdown Procedure
3.1/P4
3.1.8
Flight with an Engine Inoperative
3.1/P4
3.1.9
Emergency Airports
3.1/P5
3.1.10
Depressurisation
3.1/P5
3.1.11
Cabin Fire Procedures
3.1/P7
3.1.12
Interception Procedures
3.1/P7
3.1.13
Ground Proximity Warning System (GPWS)
3.1/P8
3.1.14
TCAS
3.1/P8
ABNORMAL/EMERGENCY PROCEDURES APPENDIX
ABNORMAL PROCEDURES
TOC/P2
TABLE OF CONTENTS
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
ABNORMAL PROCEDURES ATR-72 STANDARD OPERATING PROCEDURES
3.1
ABNORMAL PROCEDURES
3.1.1
General
3.1/P1 Rev 00 15 Jul 09
Refer ATR-72 Flight Crew Operating Manual, Section 2.04.00, Introduction, for non-normal procedures. Pilots must be sufficiently familiar with the QRH to ensure that they can, if necessary, expeditiously and accurately locate any required non-normal procedure. Selection of transponder codes for emergency situations (7700) and the making of emergency radio calls to ATC is a normal crew function and should be actioned by crew members in appropriate circumstances. It is Company policy that on all aircraft fire detector warnings are treated as genuine and the appropriate emergency procedure is completed. Abnormal or/and emergency procedures describe actions to be taken that are necessary to deal with a pending or already effective failure of any of the aircraft systems or its components. These actions are required to protect the occupant’s or/and the aircraft from impending or even critical harm. The main objective of the flight crew must be to: MAINTAIN POSITIVE CONTROL OF THE AIRCRAFT The conduct of any emergency procedures or the analysis of any technical problems should not normally take place until:
3.1.2
(a)
The vertical and lateral flight path is under positive control;
(b)
Possible ground contact is no longer a threat; and
(c)
Altitude is above 400 FT (AGL)
Procedures The presentation of the emergency procedures assumes a standard cockpit composition in which CM 1 is PIC and PF, and the CM 2 is PNF. Under some circumstances a different task distribution may be more appropriate in applying these procedures. Therefore, it is essential that the PIC assesses the situation and clearly determines the task distribution for the different phases of flight.
3.1/P2
ABNORMAL PROCEDURES
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
Since abnormal and/or emergency operation is non-routine, all actions in abnormal and/or emergency procedures have to be announced before they are performed. The actions prescribed in abnormal and/or emergency procedures are classified according to their mode of application, as follows: (a)
Memory Actions Some specific actions during the application of abnormal and/or emergency procedures must be carried out as soon as the situation permits. It is not acceptable to refer to any document due to the inherent time delay. In these cases crewmembers must be able to act by memory. After completion of memory actions the complete applicable abnormal/emergency checklist must be completed including the memory items.
(b)
Monitored Actions Some abnormal and/or emergency procedures contain non-reversible actions, which may lead to imminent danger if they are incorrectly executed. Such actions have to be monitored and shall only be executed when monitoring is confirmed by the other crewmember. These actions include:
(c)
(i)
Power lever reduction of a failed engine;
(ii)
Selection of the condition lever to FTR/FUEL SO position;
(iii)
Activation of the fire handle and extinguisher switch.
Read-and-Do Actions With the exception of the memory items most of the abnormal and/or emergency actions shall only be executed after being read from the appropriate documentation. Some of the procedures contain configuration changes of the aircraft. Therefore, proper crew coordination must be carried out before executing such action(s).
(d)
Review Actions For flight phases where the read-and-do concept is not possible to follow, review actions are presented for the flight crew to read in advance of what has to be done, thus enabling the flight crews to memorize these items when they are needed.
3.1/P3
ABNORMAL PROCEDURES ATR-72 STANDARD OPERATING PROCEDURES
3.1.3
Rev 00 15 Jul 09
Notification and Verification Verification of Condition Any crewmember detecting an abnormal and/or emergency shall immediately inform the other crewmember.
3.1.4
(a)
Aural warnings shall be silenced by pressing Warning/Caution light;
(b)
The affected system shall be recognized on the CAP;
(c)
The system’s local fault shall be identified on the overhead panel;
(d)
The PF must call for the appropriate checklist which must be confirmed by the PNF as the checklist applicable for the particular abnormal/emergency situation.
(e)
The PIC will designate the PF.
Initiation of Procedure After the PF is ready he shall initiate application by using the wording “Start Procedure”.
3.1.5
(a)
Memory actions are then performed by the PNF on commands from the PF;
(b)
Upon completion of the memory items the PF will call for the complete checklist on a Read-And-Do basis including previously completed memory items.
Reading of Checklist Abnormal and/ or emergency procedures are read by PNF starting with the procedure title and shall be read once the PF is ready to follow the execution of the procedures. Memory actions must be read a nd confirmed. Except for memory items and irreversible actions (e.g. engine shut down) the required action must be read first, then execute d and reported to PF, who shall cross check whenever feasible. Any abnormal or emergency has to be continued to its end and upon reaching the end of the checklist the PNF must announce that the applicable checklist is “COMPLETED”.
ABNORMAL PROCEDURES
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
Note:
3.1.6
3.1/P4
There may be special situations in which it is of benefit to stop an abnormal and/or emergency procedure. The decision to do so rests solely with the PIC and such decision should be based upon sound analysis of the situation.
CAUTION 1:
The main goal is to maintain positive aircraft control. All action shall be done as soon as possible but never in a hurry. Strict adherence to the checklists is mandatory.
CAUTION 2:
According to CCAR’s regulations and Company policy the Cockpit Voice Recorder (CVR) circuit breaker should be pulled after landing on any flight where a significant abnormal/emergency situation has occurred.
Acceleration Height A standard acceleration height (AGL) of 800 FT should be used or such height as published in the pre-computed takeoff charts whichever is the higher, in the event of an engine failure on takeoff.
3.1.7
Engine Shutdown Procedure Refer ATR – 72 Abnormal/Emergency Procedures Appendix at the end of this Section.
3.1.8
Flight with an Engine Inoperative Following an engine shutdown in flight it is the commander's responsibility to decide whether: (a)
The flight should be continued to destination;
(b)
The flight should return to the departure airport; or
(c)
A landing should be made at the nearest suitable airport.
Factors that need to be considered for flight with an inoperative engine include the following: (a)
Nature of the malfunction which preceded the engine shutdown and any further mechanical difficulties which may arise from the shutdown;
(b)
Availability of the inoperative engine for use;
(c)
Altitude, aircraft weight and useable fuel at the time of engine shutdown;
Deleted:
ABNORMAL PROCEDURES ATR-72 STANDARD OPERATING PROCEDURES
3.1/P5 Rev 00 15 Jul 09
(d)
Distance to be flown;
(e)
Relative characteristics of suitable airports available for landing;
(f)
Weather conditions en route and at suitable airports available for landing;
(g)
Air traffic congestion;
(h)
Type of terrain; and
(i)
Familiarity of pilot with airport to be used.
It is expected that the commander will, at all times, operate the aircraft with full regard to safety. No undue emphasis should be placed on the continuation of a flight to the destination unless the commander is satisfied that this is a desirable and safe course of action. Following an engine shutdown a two engine aircraft should normally proceed to the nearest suitable airport, although there is no objection to the aircraft proceeding to the destination provided the increased flying time is not significant. When runway approach slope guidance is not available the aircraft should carry out a normal circuit unless circumstances or terrain make this unadvisable. 3.1.9
Emergency Airports Pilots must maintain an adequate knowledge of airports, suitable for an emergency landing, which are on, or adjacent to, the aircraft's flight path. The appropriateness of a particular airport is related to the urgency of the situation. However, in general, an airport should be considered suitable, depending upon the nature of the emergency, even if it does not meet normal operational standards and if it can reasonably assumed that a safe landing can be made.
3.1.10
Depressurisation
3.1.10.1
General
In the event of a depressurisation the requirement for the donning of oxygen masks is immediate. The following table of Times of Useful Consciousness are representative of a person in normal health in a seating position.
ABNORMAL PROCEDURES
3.1/P6 Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
ALTITUDE (FT)
TIME
22,000
5 minutes
25,000
2 minutes
28,000
1 minute
30,000
45 seconds
35,000
30 seconds
40,000
18 seconds
The above times can be reduced by approximately 50% with moderate activity and by approximately 33% in a rapid depressurization. If oxygen is applied expeditiously the debilitating effects of oxygen deprivation are removed within 20 seconds. 3.1.10.2
Emergency Descent Procedures
If an emergency descent is required the procedures as detailed in the Flight Crew Operating Manual should be followed. Following completion of the applicable nonnormal procedure(s), the First Officer should select transponder code 7700 and advise ATC through the use of a PAN call. The commander should make the following PA announcement: “COCKPIT SPEAKING, CABIN CREW SEATED AND FASTENED” Flight deck crews must be aware of the height of the terrain in the vicinity of the descent and must limit the descent to the MSA (or grid MORA) for the sector or 10,000 FT whichever is the higher. During the descent, the First Officer should call each 5,000 FT, 2,000 FT and 1,000 FT prior to the nominated level off altitude. When the aircraft attains the required level off altitude, the commander should make a PA announcement indicating that the use of oxygen masks (if used by the passengers) is no longer required and/or explain the reason for the emergency descent. Based upon this PA announcement the purser shall enter the flight deck to report on the condition of passengers and cabin crew.
3.1/P7
ABNORMAL PROCEDURES ATR-72 STANDARD OPERATING PROCEDURES
Rev 00 15 Jul 09
The flight deck crew should assess the situation with respect to:
3.1.11
(a)
The state of any structural damage (if required);
(b)
Distance to and weather conditions at suitable diversion airport(s);
(c)
Any intervening terrain between the aircraft’s position and suitable diversion airport(s); and
(d)
Diversion fuel requirements.
Cabin Fire Procedures In the case of a fire in the cabin, a cabin crew member will contact the flight deck either personally or via the interphone providing the following information: (a)
What is actually on fire and its location;
(b)
If the fire is in the galley area, request that galley power be removed;
(c)
The amount and the colour of the smoke and the effect it is having on the passengers; and
(d)
The ferocity of the fire and whether it can be contained.
The purser should keep the commander updated as to the progress in containing the fire and if at any time the situation appears out of control an immediate face to face report will be made. In this case a landing at the nearest adequate airport should be considered. 3.1.12
Interception Procedures ICAO standard procedures are to be followed in the event of in-flight interception. These procedures, including the State variations are detailed in the Jeppesen Airway Manual together with an appropriate NOTAM for any variations from standard procedures. In the event of an in-flight interception proceed as follows; (a)
Do not perform any manoeuvre that may be construed as hostile. Maintain straight and level flight;
ABNORMAL PROCEDURES ATR-72 STANDARD OPERATING PROCEDURES
3.1/P8 Rev 00 15 Jul 09
(b)
Select transponder to 7700 and where possible notify the appropriate ATC centre;
(c)
Attempt to establish communication with the interceptor or with the appropriate intercept control unit by making a general call on 121.5 MHZ giving the identity and position of the aircraft and the nature of the flight; and
(d)
Follow instructions from intercepting aircraft responding as appropriate to instructions.
If any instructions received by radio from any source conflict with those given by the intercepting aircraft request immediate clarification whilst complying with the instructions given by the intercepting aircraft. 3.1.13
Ground Proximity Warning System (GPWS) Refer Flight Crew Operating Manual, Page 2.02.16.
3.1.14
TCAS Refer Flight Crew Operating Manual, Page 2.02.15
ATR – 72 ABNORMAL/EMERGENCY PROCEDURES APPENDIX
GROUND PHASE EVENT
CM 1
CM 2
ENGINE FIRE BEFORE V1
Takeoff run
- Receive takeoff clearance and announce “Cleared for takeoff. Wind 0 _____ /______knots” -
Announce “Takeoff, timing, flight control left or right”
-
Advance PL’s to notch position and announce “Notch”
- Select clock to RUN and CHR - Hold control column forward and into wind - Check ATPCS ARM light illuminates and announce “ATPCS arm” - Check FDAU bars on RTO value - Check engine parameters TQ, NP, ITT, NH oil and announce “Power set” - Continue to scan airspeed and engine instruments throughout takeoff and announce “Engine instruments checked normal”
- Announce “Seventy knots” At 70 knots -
ATR-72 ABNORMAL/EMERGENCY PROC
Release nose wheel steering and announce “I have control” or “You have control” (CM2 as PF)
15 JUL 09 – REV 00
- Confirm “You have control” or “I have control” (CM2 as PF)
PAGE 1
GROUND PHASE EVENT
CM 1
- “Engine Fire”
Fire warning occurs
Aircraft stopped
Memory Items
-
“STOP”
-
Rejected takeoff: Retard PL’s to FI then GI Reverse as required Full braking 0 Stop aircraft with good engine into the wind (0 to 0 90 )
-
-
- “Engine 1 fire, wind from (left or right)
Command: “Both condition levers to feather, then shut off”
“Agent 1 discharge” “Timing 30 seconds”
-
or
-
“Engine 2 fire, wind from (left or right) Cancel fire warning Hold control column Notify ATC
Parking brake ON
“Fire handle (1 or 2) pull”
ATR-72 ABNORMAL/EMERGENCY PROC
CM 2
- Retard both CL’s to FTH then SO and announce “Both condition levers to feather and shut off” - Pull fire handle (1 or 2) and announce “Fire handle (1 or 2) pulled” - Activate AGENT 1 push button and announce “Agent 1 discharged” - Commence timing and announce “Timing started”
Make PA announcement “Cockpit speaking, cabin crew to your stations”
15 JUL 09 – REV 00
PAGE 2
GROUND PHASE EVENT
CM 1
CM 2
Command “On ground engine fire checklist”
On Ground Engine Fire checklist
Read On Ground Engine Fire checklist After 30 seconds and fire warning continues
- Announce “30 seconds – fire continues” - Command “Agent 2 discharge”
- If fire warning continues announce “Fire continues”
If fire warning continues or there is external evidence of fire - Command “Fire handle (1 or 2) pull”
Evacuation
- Pull second fire handle and announce “Fire handle (1 or 2) pulled”
Make PA announcement “Evacuate left/right, evacuate left/right, evacuate left/right”
- Command “Emergency evacuation checklist” Emergency evacuation checklist
ATR-72 ABNORMAL/EMERGENCY PROC
- Activate AGENT 2 push button and announce “Agent 2 discharged”
15 JUL 09 – REV 00
- Read and do Emergency Evacuation checklist - When complete announce “Emergency evacuation checklist completed”
PAGE 3
FLIGHT PHASE EVENT
PF
ENGINE FIRE AFTER V1 Note: No any action relating to the engine fire are to be made until the landing gear has been selected UP V1
VR
-
Check speed Release hand from PL’s
ENGINE FIRE
-
Check speed Rotate aircraft
PNF
- Announce: “V1”
- Announce: “Rotate”
- Announce: “ENGINE FIRE” -
Respond: “Continue”
-
Command: “Gear up”
-
Check no lights on LAND GEAR panel and respond: “Checked”
Positive climb established on VSI
Identify engine
- Identify engine: “Confirm (1 or 2)”
Notify ATC
(Immediately after fire warning sounds, cancel CRC by pressing the MW or EMER AUDIO CANCEL) - Announce: “Positive climb” - Select gear lever to the UP position and announce: “Gear up selected” - Check no lights on LAND GEAR panel and announce: “Gear up set” - Confirm: “Engine fire (1 or 2)”
- Notify ATC
400Ft AGL
- Announce: “400 Feet” - Check altitude and order: “Memory items”
Memory items PLs
ATR-72 ABNORMAL/EMERGENCY PROC
-
Hold non-affected engine PL Command: “Power lever (1 or 2) to flight idle” 15 JUL 09 – REV 00
- Confirm correct engine and retard affected PL to FI position and announce: “Power lever (1 or 2) to flight idle” PAGE 4
FLIGHT PHASE EVENT
PF
PNF
Memory items(con’t) CLs
-
Hold non-affected engine CL Command: “Condition lever (1 or 2) to feather, then shut off”
- Confirm correct engine and retard affected CL to FTH then SO and announce: “Condition lever (1 or 2) to feather(wait one second) and shut off”
Fire handle
-
Command: “Fire handle (1 or 2) pull”
- Place hand on applicable fire handle - When confirmed pull fire handle (1 or 2) and announce: “Fire handle (1 or 2) pulled”
Timing 10 seconds
-
Command: “Timing 10 seconds”
Agent discharge
-
Command: “Agent 1 discharge”
-
Monitor Fire handle red light If Fire continue
30 seconds
- Command: “Agent 2 discharge”
-
Monitor Fire handle red light
- Respond: “Timing” - After 10 seconds announce: “10 seconds time out” - Activate AGENT 1 push button and announce: “Agent 1 discharged” Note: Light comes ON when bottle is Empty. - After 30 seconds announce: “30 seconds time out” - Activate AGENT 2 push button and announce: “Agent 2 discharged” - Announce: “Memory items completed”
- Respond: “Checked” - Announce: “Acceleration altitude”
Acceleration altitude - Command: “Altitude Hold”
ATR-72 ABNORMAL/EMERGENCY PROC
15 JUL 09 – REV 00
- Select ALT HOLD on ADU and announce: “Altitude hold”
PAGE 5
FLIGHT PHASE EVENT
In-Flight engine fire check list
PF
PNF
- Command: “In-flight engine fire checklist”
- Read and do In-Flight Engine Fire checklist
- Monitor and confirm items
- When complete announce: “In-flight engine fire checklist competed”
Speed at white or red bug speed
After Takeoff checklist
Single Engine Operation checklist
ATR-72 ABNORMAL/EMERGENCY PROC
-
Check ASI speed and command: “IAS, flaps zero (fifteen – icing), MCT”
-
Check IAS, flap indicator shows 0 (or 15 ) and PWR MGT to MCT and respond: “Checked”
0
0)
- Announce: “White bug” or Red bug” (as applicable) - Select IAS and announce: “IAS set” 0 - Select flap lever to 0 and announce: “Flaps zero ( fifteen) selected” - Set PWR MGT to MCT and announce: “MCT set” 0 0 - Check flap indicator shows 0 (15 – icing) and announce: “Flaps zero (fifteen) set” - Adjust IAS to white/red bug speed
- Command: “After takeoff checklist” - Monitor and confirm items
- Read and do After Takeoff checklist
- Command: “Single engine operation checklist” - Monitor and confirm items
- Read and do Single Engine Operation checklist - When complete announce: “Single engine operation checklist completed”
15 JUL 09 – REV 00
- When complete announce: “After takeoff checklist completed”
PAGE 6
FLIGHT PHASE EVENT
PF
PNF
- Command: “Clear CAP” - Push CLR on CAP Decision – Land ASAP
- Announce intentions and diversion airport.
PA announcement
- Make PA announcement to passengers
ATR-72 ABNORMAL/EMERGENCY PROC
15 JUL 09 – REV 00
PAGE 7
FLIGHT PHASE EVENT
PF
PNF
ENGINE FLAMEOUT AFTER V1 Note: No any action relating to the engine flame-out are to be made until the landing gear has been selected UP
V1
-
Check speed Release hand from PL’s
- Announce: “V1”
VR
-
Check speed Rotate aircraft
- Announce: “Rotate”
ENGINE FLAME OUT AT TAKE-OFF
Positive climb established on VSI
CONT RELIGHT (ATR72 -200 only)
- Announce: “ENGINE FLAME OUT” - Respond: “CONTINUE”
-
Command: “Gear up” Check no lights on LAND GEAR panel and respond: “Checked”
UP TRIM
- Check CONT Relight ON and respond: “Checked” - If no UP trim , both PLs advance to RAMP
AUTO FEATHER
- If no AUTO FTHR command: “CL (1 or 2) to Feather”
-
ATR-72 ABNORMAL/EMERGENCY PROC
Check TQ=100% on live engine and NP=0% on failed engine Respond: “Checked”
15 JUL 09 – REV 00
- Announce: “Positive climb” - Select gear lever to the UP position and announce “Gear up selected” - Announce: “CONT RELIGHT ON” (select if not) (ATR72-200 only) - Check UP trim on live engine and announce: “ UP TRIM” or “NO UP TRIM”
- Check NP=0% on failed engine and announce: “ AUTO Feather” , if not “NO AUTO Feather” - Retard CL (1 or 2) to feather position and announce: “CL (1 or 2) Feather”
PAGE 8
FLIGHT PHASE EVENT
PF
LAND GEAR -
Check no lights on LAND GEAR panel and respond: “Checked”
Notify ATC
- Command: “Altitude hold”
Announce: “Engine flame out (1 or 2)”
Identify engine
-
Memory items
- Announce: “Memory Items”
PL
-
Hold non-affected engine PL Command: “Power lever (1 or 2) to flight idle” (Retard PL to NOTCH on good engine if it was on RAMP) - Hold non-affected engine CL - Command: “Condition lever (1 or 2) to feather, then shut off” - Respond: “Checked”
Speed at white or red bug speed -
ATR-72 ABNORMAL/EMERGENCY PROC
- Check no lights on LAND GEAR panel and announce: “Gear up set” - Notify ATC
Acceleration altitude
CL
PNF
Check ASI speed and command: “IAS, flaps zero (fifteen – icing), MCT”
15 JUL 09 – REV 00
- Announce :“Acceleration altitude” - Select ALT mode on ADU and announce: “Altitude hold” - Respond: “Confirm engine ( 1 or2)”, if identification incorrect.
- Confirm correct engine and retard affected PL to FI position and announce: “Confirm power lever (1 or 2) to flight idle” - Confirm correct engine and retard affected CL to FTH (wait one second) then SO and announce: “Condition lever (1 or 2) to feather and shut off” - Announce: “Memory items completed” - Announce: “White bug” or Red bug” (as applicable) - Select IAS and announce: “IAS set” 0 - Select flap lever to 0 and announce “Flaps zero ( fifteen) selected” - Set PWR MGT to MCT and announce: “MCT set” PAGE 9
FLIGHT PHASE EVENT
PF
PNF 0
-
0
0)
Check IAS, flap indicator shows 0 (or 15 ) and PWR MGT to MCT and respond: “Checked”
Command “Engine flameout at takeoff checklist” - Monitor and confirm items
0
- Check flap indicator shows 0 (15 – icing) and announce: “Flaps zero (fifteen) set” - Adjust IAS to white/red bug speed
Engine Flame Out At Takeoff checklist
After Takeoff checklist
- Command “After takeoff checklist” - Monitor and confirm items
- Read and do Engine Flame Out At Takeoff checklist - When complete announce “Engine flame out at takeoff checklist completed”
- Read and do After Takeoff checklist - When complete announce “After takeoff checklist completed”
Single Engine Operation checklist
- Command “Single engine operation checklist” - Monitor and confirm items
- Read and do Single Engine Operation checklist - When complete announce “Single engine operation checklist completed”
- Command “Clear CAP” - Push CLR on CAP
Decision – Land ASAP - Announce intentions and diversion airport. PA announcement - Make PA announcement to passengers
ATR-72 ABNORMAL/EMERGENCY PROC
15 JUL 09 – REV 00
PAGE 10
FLIGHT PHASE EVENT SINGLE ENGINE GO-AROUND Go-around
PF
PNF
-- Command “Go-around” and simultaneously: PL’s advance to the RAMP position Press the GA switch 0 Rotate aircraft to go-around attitude (8 ) Command “Flaps 15” • • • •
Positive climb established on VSI - Command “Gear up”
-
Established in stable climb
0
Check flap indicator shows 15 and no lights on LDG GEAR panel and respond “Checked”
- Select TAXI light to OFF and announce “Taxi light off”
- Command “Heading, low bank IAS”
- Select HDG, BANK to low and adjust IAS to VGA on ADU and announce “Heading, low bank and IAS set”
Check settings and respond “Check”
Notify ATC
- Notify ATC
Acceleration altitude - Command “Altitude hold”
ATR-72 ABNORMAL/EMERGENCY PROC
- Announce “Positive climb” - Select gear lever to the UP position and announce “Gear up selected” 0 - Check flap indicator shows 15 and no lights on LDG GEAR panel and announce “Flaps 15, gear up set”
- Command “Taxi light off”
-
PL’s back to NOTCH position
- Check PL’s at the RAMP position and announce “Go-around power set” 0 - Select flap lever to 15 position and announce “Flap 15 selected”
-Retard PL’s to NOTCH position and announce -“Power levers back to notch”
15 JUL 09 – REV 00
- Announce “Acceleration altitude” - Select ALT mode on ADU and announce “Altitude hold” -Check PL’s at notch position, announce -“Notch checked” PAGE 11
FLIGHT PHASE EVENT
PF
PNF
- Announce “White bug” or Red bug” (as applicable)
Speed at white or red bug speed -
-
Check ASI speed and command “IAS, flaps zero (fifteen – icing), MCT”
0
0)
Check IAS, flap indicator shows 0 (or 15 ) and PWR MGT to MCT and respond “Checked”
- Select IAS and announce “IAS set” 0 - Select flap lever to 0 and announce “Flaps zero ( fifteen) selected” - Set PWR MGT to MCT and announce “MCT set” 0 0 - Check flap indicator shows 0 (15 – icing) and announce “Flaps zero (fifteen) set” - Adjust IAS to white/red bug speed
-
Command “After takeoff checklist”
After Takeoff Checklist
- Read and do After Takeoff checklist - When complete announce “After takeoff checklist completed” -
Make PA announcement to passengers
PA announcement
ATR-72 ABNORMAL/EMERGENCY PROC
15 JUL 09 – REV 00
PAGE 12
FLIGHT PHASE EVENT
PF
PNF
EMERGENCY DESCENT
According to flight event
Autopilot remains engaged
-Order: “Emergency descent” “Memo items” :Do - Mask/Crew communication(as RQD) - Select minimum altitude on ALT SEL - Select IAS mode and set 245kts - Turn with HDG knob ±45º - PLs to FI - Cont relight on (ATR72-200 only) - CLs to 100 OVRD or MAX RPM (ATR72-200 only)
-Order: “Emergency descent checklist” - Emergency checklist response
:Do - Emergency checklist read
- Order: “Masks off” :Do - Oxygen mask remove - Oxygen hatch close - Oxygen test P/B depress
ATR-72 ABNORMAL/EMERGENCY PROC
“Memo items completed”
“Emergency descent checklist completed”
- Monitor R/D Approaching FL 100
:Do - Mask/Crew communication(as RQD) - Seat belts on - PA: - XPDR 7700 set - ATC: Mayday, mayday, mayday - Oxygen pax supply on - Oxygen pressure check
15 JUL 09 – REV 00
:Do - Oxygen mask remove - Oxygen hatch close - Oxygen test P/B depress
PAGE 13
ATR-72 STANDARD OPERATING PROCEDURES
SECTION 4 PERFORMANCE
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
PERFORMANCE
TOC/P1
TABLE OF CONTENTS
Rev 00
ATR-72 STANDARD
15 Jul 09
OPERATING PROCEDURES
4.1
COMPUTER TAKEOFF CHARTS
4.1/P1
4.1.1
General
4.1/P1
4.1.2
Takeoff Chart Format
4.1/P2
4.1.3
De-Code of Takeoff Chart
4.1/P3
PERFORMANCE
TOC/P2
TABLE OF CONTENTS
Rev 00
ATR-72 STANDARD
15 Jul 09
OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
PERFORMANCE ATR-72 STANDARD OPERATING PROCEDURES
4.1
COMPUTER TAKEOFF CHARTS
4.1.1
General
4.1/P1 Rev 00 15 Jul 09
The Company produces computer generated runway takeoff and landing charts for the ATR-72 aircraft. Airport analyses facilitate the determination of the maximum allowable takeoff for specific airport conditions and aircraft configurations with the failure of the most critical engine. The limitations observed are those specified in the approved Airplane Flight Manual (AFM). The maximum allowable takeoff weight is determined by the most limiting of the following:
4.1.2
(a)
Maximum Certified Takeoff Weight: The structural limit weight;
(b)
Climb Limit Weight: The maximum weight at which the required minimum climb gradients are available in the second and final segment based on the airport elevation and temperature;
(c)
Runway Limit Weight: The maximum weight at which the aircraft complies with the certification requirements under the rules governing required runway length. The runway limited weight is a function of runway length, slope, airport elevation, temperature and wind;
(d)
Obstacle Limited Weight: The maximum weight at which obstacle clearance required by ICAO can be demonstrated. The obstacle limited weight is a function of obstacle height and distance, temperature, airport elevation, runway slope and wind. Unless otherwise specified on the airport analysis, a straight flight out path along the extended runway center line is assumed;
Takeoff Chart Format
Set out below is a facsimile of the Company standard computer generated takeoff chart for ATR-72 aircraft.
4.1/P2
PERFORMANCE
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
F15
1.
13/07/2004
TANSONNHAT
VVTS 25R
2.
ELEVATION= 33.0 (FT)
3.
T.O.R.A = 10000.0 (FT)
0-DRY CHECK
5-TYRE SPEED
4.
A.S.D.A = 11017.0 (FT)
1-STRUCTURE
6-BRAKE ENERGY
5.
T.O.D.A = 11017.0 (FT)
2-2ND SEGMENT
7-RWY 2 ENGINE
AIR COND. ON
6.
SLOPE =
3-RUNWAY
8-FINAL TO
NORMAL CONDITIONS
7.
LARGE WIDTH ASSUME 4-OBSTACLE
9-VMC
WITHOUT REVERSE
8.
NO OBSTACLE AVAILABLE
9.
- WIND
TOW (KG)
10.
O – KT
V1 VR V2 (IAS KT)
11.
A
12.
T
13.
(DC) 5.0
14. 15.
10.0 15.0 20.0 22.0 24.0
LIMITATION CODES
-0.08 (%)
CODES
ATR72-500
QNH = 1013.2 (HPA)
JAR-DGAC
V2/VS OPTIMIZED V1/VR OPTIMIZED
DRY RUNWAY SCREEN HEIGHT 35 FT
-10
-5
0
5
10
22500 1-1
22500 1-1
22500 1-1
22500 1-1
22500 1-1
98 110 114
100 110 114
100 110 114
100 110 114
100 110 114
22500 1-1
22500 1-1
22500 1-1
22500 1-1
22500 1-1
98 110 114
100 110 114
100 110 114
100 110 114
100 110 114
22500 1-1
22500 1-1
22500 1-1
22500 1-1
22500 1-1
97 110 114
101 110 114
101 110 114
101 110 114
101 110 114
22500 1-1
22500 1-1
22500 1-1
22500 1-1
22500 1-1
97 110 114
101 110 114
101 110 114
101 110 114
101 110 114
22500 0-0
22500 1-1
22500 1-1
22500 1-1
22500 1-1
96 110 114
101 110 114
101 110 114
101 110 114
101 110 114
22500 1-1
22500 1-1
22500 1-1
22500 1-1
22500 1-1
96 110 114
101 110 114
101 110 114
101 110 114
101 110 114
DATA INTENTIONALLY NOT DISPLAYED (EXAMPLE ONLY) 44.0 46.0 48.0 50.0
21866 2-4
22257 2-4
22231 2-2
22231 2-2
22231 2-2
98 113 117
107 122 125
115 129 132
115 129 132
115 129 132
21582 2-4
21922 2-4
21965 2-2
21965 2-2
21965 2-2
98 113 117
107 122 125
115 127 131
115 127 131
115 127 131
21285 2-4
21574 2-4
21596 2-2
21596 2-2
21596 2-2
99 114 117
109 123 126
114 126 129
115 126 129
115 126 129
20991 2-4
21220 2-4
21228 2-2
21228 2-2
21228 2-2
100 114 117
110 123 126
114 125 128
115 125 128
115 125 128
16.
/NO OBSTACLE
17.
/MINI. ACCELERATION HEIGHT:
800. (FT)
QNH ALT:
833 (FT)
18.
/MAXI. ACCELERATION HEIGHT:
2184.(FT)
QNH ALT:
2217 (FT)
PERFORMANCE
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
4.1.3
1.
2.
3.
4.
5.
6.
4.1/P3
De-Code of Takeoff Chart
F15……………………......
Flap setting
13/07/2004………………. TANSONNHAT.…………
Date chart prepared Name of airport
VVTS 25R……………….
IATA code and runway direction
ELEVATION = 33.0 (FT).
Airport elevation
LIMITATION CODES….
Title
ATR72-500………………
Aircraft type and model
JAR-DGAC………………
Certifying authority
T.O.R.A = 10000.0 (FT)
Takeoff run available
0-DRY CHECK………….
Program checks both dry and wet conditions and if a dry limit shows this limit code
5-TYRE SPEED…………
Tyre speed limit code
V2/VS OPTIMIZED……..
Basis of chart calculation
A.S.D.A = 11017.0 (FT) 1-STRUCTURE…………
Accelerate stop distance available Structural limit code
6-BRAKE ENERGY…….
Brake energy limit code
VI/VR OPTIMIZED………
Basis of chart calculation
T.O.D.A = 11017.0 (FT)
Takeoff distance available
2-2ND SEGMENT………
Second segment limit code
7-RWY 2 ENGINE………
Two engine runway lengthy limit code
AIR COND. ON………….
Air conditioning on
SLOPE = -0.08%.............
Runway slope
3-RUNWAY………………
Runway limit code
8-FINAL TO……………...
Program checks fourth segment and if a limit shows this limit code
NORMAL CONDITIONS.
Statement on conditions
PERFORMANCE
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
7.
4.1/P4
LARGE WIDTH ASSUMED……………….
Program has the capability to enter runway width. If not entered displays this text meaning a default width of 30 m
4-OBSTACLE……………
Obstacle limit code
9-VMC………………….... WITH OUT REVERSE….
VMC (G) limit code Operation with out reverser assumed for dry runway. With reverser for wet runway
8.
NO OBSTACLE AVAILABLE………………
Obstacle data is presented in this field
9.
WIND……………………. TOW (KG)……………….
Title Title
CODES………………….
Title
QNH=1013.2 (HPA)…….
QNH pressure used for chart
DRY RUNWAY………….
Runway condition
O – KT……………………
Title
V1 VR V2 (IAS KT)……..
Title
SCREEN HEIGHT………
Text on dry runway screen height
11.
A…………………………..
Title
12.
T…………………………..
Title
13
DC………………………... -10, -5, 0, 5, 10…………..
Degrees C Wind speed
14.
5.0………………………… 22500 1-1……………….
OAT Maximum takeoff weight and limitation code
15.
98 110 114…………….
V1, VR and V2 speeds
16.
/NO OBSTACLE…………
Statement on obstacle
10.
PERFORMANCE
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
17.
18.
4.1/P5
MINI. ACCELERATION HEIGHT………………….
Title
800. (FT)…………………
Minimum acceleration height (AGL)
QNH ALT: 833 (FT)……..
Minimum acceleration height (QNH)
MAXI. ACCELERATION HEIGHT………………….
Title
2184. (FT)………………..
Minimum acceleration height (AGL)
QNH ALT: 2217 (FT)……
Minimum acceleration height (QNH)
PERFORMANCE
4.1/P6 Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
ATR-72 STANDARD OPERATING PROCEDURES
SECTION 5 FLIGHT PLANNING
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
FLIGHT PLANNING
TOC/P1
TABLE OF CONTENTS
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
5.1
FLIGHT PLANNING
5.1/P1
5.1.1
Sample Computer Flight Plan
5.1/P1
5.1.2
De-Code of Computer Flight Plan
5.1/P4
5.1.3
Fuel Calculations
5.1/P11
FLIGHT PLANNING
TOC/P2
TABLE OF CONTENTS
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
5.1/P1
FLIGHT PLANNING ATR-72 STANDARD OPERATING PROCEDURES
5.1
FLIGHT PLANNING
5.1.1
Sample Computer Flight Plan
1 2
PLAN 1660 K6XXX/PNHSGN VDSR TO VVTS AT72 HSC/F IFR 15/07/09 NONSTOP COMPUTED 0258Z FOR ETD 0800Z PROGS 0000ADF VNB212 KGS
3 4 5
ATTN CAPT FLT RELEASE XXXXXX VDSR /REP 1500L/0800Z/. . . . BLOFF . . . . VVTS /SGN 1608L/0908Z/. . . . BLON . . . .
6
GCD 0228 G/D 0279 A/D 0285 W/C M007 TEMP M13 TDV/P18 MAXS 4/POPET
7 8 9 10 11 13 14 15 16
23
E.FL A.FUEL E.TIME TRIP 702 . . . . 1.08 ROUTE RES 5PCT 50 . . . . 0.05 FUEL BURN ADJUSTMENT FOR ALTERNATE VDPP 392 . . . . 0.35 FINAL RES 250 . . . . 0.30 1000 KGS INCR/DECR EXTRA 0 . . . . 0.00 IN TOW +/- 10 KGS TAKE OFF 1394 . . . . 2.18 TAXI 40 . . . . BLOCK 1434 . . . . 2.18 BLOCK FUEL . . . . ------------------ --------------E.WT CORR. OP.LIMIT STRUC. REASONS FOR OP.LIMIT DOW 013640 ... .. EPLD 004000 ... .. EZFW 013640 ... .. MZFW ... .. 020300 / . . . . . . . . . ETOW 015034 ... .. MTOW ... .. 022500 / . . . . . . . . . ELAW 014332 ... .. MLAW ... .. 022350 / . . . . . . . . . ------------------ --------------FUEL CONSUMPTION - 0.0 PCT/HR/ENG
24 25
COMPANY ROUTE R01 FL230 VDSR W15 PNH R468 TSN..VVTS
17 18 19 20 21 22
------------------ --------------26
CAPT. . . . . . . . . . FO . . . . . . . . DISP. . . . . . . . . . ------------------ ---------------
27 28
29 30 31
32 33 34 35 36
DEST ALTERNATE MSA TTK GDIST ADIST FL W/C TIME FUEL ALTN - 1 VDPP /PNH 073 292 138 139 180 P001 00.35 392 TIME TO DIST W/C CFR FOB XFR ETP / ALT ETP1 VDSR / VDPP 0066/0066 P003/M003 0 001160 00000 00.19/00.16 N12378E104366 ETP2 VDPP / VVTS 0059/0056 P004/M017 0 000875 00000 00.49/00.14 N11108E105468 ------------------ --------------VDSR ELEV 00059FT REMAINING AWY FIX OAT FL TAS GS MCSE ZDIST ZTIME ETA ECBO TIME EFOB FREQ MSA WIND ITCS RDIST CTIME ATA ACBO AFOB ---------------------------------W15 SATON P00 15 239 241 123 0057 00/14 .... 000.2 00/54 001.2 082 053/003 122 0222 00/14 .... ..... ..... ----------------------------------
Rev 00 15 Jul 09
5.1/P2
FLIGHT PLANNING ATR-72 STANDARD OPERATING PROCEDURES
37
38
W15 ETP1 M13 23 269 263 169 0020 00/05 .... 000.2 00/49 001.2 082 114/011 169 0202 00/19 .... ..... ..... ---------------------------------W15 TOC M13 23 269 263 169 0028 00/07 .... 000.3 00/42 001.1 082 114/011 169 0174 00/26 .... ..... ..... ---------------------------------W15 PNH M13 23 269 263 169 0038 00/09 .... 000.4 00/33 001.0 114.3 082 114/011 169 0136 00/35 .... ..... ..... ---------------------------------R468 ETP2 M13 23 269 258 113 0060 00/13 .... 000.5 00/20 000.9 073 116/011 112 0076 00/48 .... ..... ..... ---------------------------------R468 TOD M13 23 269 258 113 0007 00/02 .... 000.5 00/18 000.9 073 116/011 112 0069 00/50 .... ..... ..... ---------------------------------R468 POPET M11 22 346 336 113 0003 00/01 .... 000.5 00/17 000.9 073 141/011 112 0066 00/51 .... ..... ..... ---------------------------------R468 SAPEN M04 17 322 319 110 0015 00/03 .... 000.6 00/14 000.8 046 053/005 109 0051 00/54 .... ..... ..... ---------------------------------R468 CUCHI P06 11 293 292 114 0017 00/04 .... 000.6 00/10 000.8 046 082/000 114 0034 00/58 .... ..... ..... ---------------------------------R468 TSN P15 07 272 275 114 0013 00/04 .... 000.6 00/06 000.8 116.7 016 264/004 114 0021 01/02 .... ..... ..... ---------------------------------.. VVTS P18 00 269 258 079 0021 00/06 .... 000.7 00/00 000.7 .../... 0000 01/08 .... ..... ..... ---------------------------------VVTS ELEV 00033FT
VDSR N13247E103487 SATON N12570E104336 ETP1 N12378E104366 PNH N11326E104506 ETP2 N11108E105468 POPET N11060E105570 SAPEN N11012E106110 CUCHI N10542E106269 TSN N10490E106387 VVTS N10492E106397
------------------ --------------FIRS VVTS /0054 ------------------ --------------39 40
ALTERNATE DATA -N0272F180 SAP1C SAPEN R468
41 42
CPT LAT LONG MCS DIST D249D N10474 E106348 251 0005 SAPEN N11012 E106108 300 0028 POPET N11060 E105570 290 0015 VDPP N11330 E104516 293 0090
43 44 45
(FPL-XXXXXX-IS -AT72/M-SGDH/S -VDSR0800
Rev 00 15 Jul 09
5.1/P3
FLIGHT PLANNING ATR-72 STANDARD OPERATING PROCEDURES
46 47 48 49 50 51 52
-N0269F230 W15 PNH R468 TSN DCT -VVTS0108 VDPP -EET/ VVTS0054 REG/VN-B212 SEL/CFMR -E/0218 P/TBN R/UV S/MJ J/L D/0 0 C N/A A/BLUE) C/......)
53
END OF JEPPESEN DATAPLAN REQUEST NO. 1660 END OF PLAN 1660
Rev 00 15 Jul 09
5.1/P4
FLIGHT PLANNING Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
5.1.2
1.
Decode of Computer Flight Plan
PLAN 1660………………...
Flight plan with reference number.
K6XXX/PNHSGN VDSR...………………........
Title (Flight number/sector) Departure airport (ICAO).
VVTS…………………........ ATR72………….……........
Arrival airport (ICAO). Data plan aircraft type.
HSC/F………………….......
Primary cruise mode/fuel conservation.
IFR……………………........
Instrument Flight Rules.
15/07/09……………………
Day/month/year flight plan computed
NONSTOP……………….... COMPUTED 0258Z….......
Non stop flight plan. Time flight plan was computed.
FOR ETD 0800Z……........ PROGS………………........
Estimated Time of Departure. Bracknell winds prognostics.
0000ADF...........................
Date time collection weather data, ADF – Aviation Digital Format
VNB-212..…………….......
Customer aircraft data base file.
KGS………………………..
Kilos (Flight plan in kilos).
3.
ATTN CAPT…………........
Send to responsible person
4.
XXXXXX.………………….
Call sign
VDSR/REP……………….. 1500L/0800z………….......
Departure airport (ICAO/IATA). Estimated Time of Departure - Local/Zulu time
BLOFF.………………........
Block off time
VVTS/SGN
Arrival airport (ICAO/IATA).
1608L/0908Z ..………........
Estimated Time of Arrive – Local/Zulu time
BLON……..………………..
Block on time
2.
5.
5.1/P5
FLIGHT PLANNING Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
6.
7.
8.
9.
GCD 0228…………….......
Great Circle Distance.
G/D 0279..…………….......
Ground Distance.
A/D 0285….………………..
Air Distance.
W/C M007….………...........
Average Wind Component.
TDV/P18…….……………..
Average Temperature Deviation.
MAXS 4/POPET.……........
Maximum wind shear at waypoint.
E.FL….……….………........
Estimated fuel burn values.
A.FUEL
Actual fuel burn values.
E.TIME………….……….....
Estimated time values.
TRIP……...……………....... 702………...….………......
Estimated trip fuel burn.
1.08…………...….…….......
Estimated time en-route.
ROUTE RES 5PCT
Variable reserve = 0.05 x (TRIP+ALTERNATE).
10.
11.
12
50….…………………….....
Reserve fuel value.
0.05…………………….......
Estimated time value of reserve fuel.
ALTN
Alternate (ICAO)
VDPP…..………...
392..……………………......
Estimated fuel burn to alternate.
0.35……..…………........
Estimated time to alternate.
FINAL RES…………........
Holding fuel and time values.
250…………………….......
Hold fuel
0.30…………………........
30 minutes holding at alternate (1500 FT AGL).
FUEL BURN ADJUSTMENT FOR 1000 KGS INCR/DECR
Fuel burn for each 1000 kg increase or decrease in take-off weight.
IN TOW +/– 9 KGS.……...
5.1/P6
FLIGHT PLANNING Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
13.
EXTRA……………………..
Extra fuel and time values.
14.
TAKE OFF.………………..
Take-off fuel and time values.
1394………………….........
Estimated take-off fuel.
2.18.………………….........
Estimated total time.
TAXI………………………..
Taxi fuel
40…………………….........
Taxi fuel quantity
BLOCK……………..…...... 1434..………………….......
Ramp fuel and time values. Estimated ramp fuel.
2.18………………….......... BLOCK FUEL……………..
Estimated total time. Actual ramp fuel – fill in area
E.WT…………………........
Estimated weight
CORR…………………......
Correct
OP.LIMIT…………………..
Operations limit
STRUC……………….........
Structure limit
REASONS FOR OP.LIMIT…………………..
Reasons for operations limit
18.
DOW
013640
Dry operating weight
19.
EPLD
4000
20.
EZFW
013640
Estimated zero fuel weight
MZFW
020300
Maximum zero fuel weight
21.
ETOW MTOW
015034 022500
Estimated takeoff weight Maximum takeoff weight
22.
ELAW
014332
Estimated landing weight
MLAW
022350
Maximum landing weight
15.
16.
17.
Estimated payload
5.1/P7
FLIGHT PLANNING Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
23.
FUEL CONSUMPTION – 0.0 PCT/HR/ENG..……..…
Primary cruise mode fuel degradation
24.
COMPANY ROUTE R01……………..………….
Name of company route in route database file
25.
VDSR W15 PNH..............
Route summary waypoint
26.
CAPT…………………….....
Signature of Captain
FO………………………….. DISP....…………………….
Signature of First Officer Signature of Dispatcher
DEST ALTERN……….......
Destination alternate.
MSA……………………….. TTK……………………......
Minimum Safe Altitude (grid MORA data). True track to alternate
GDIST…………………......
Ground distance to alternate
ADIST….………………….. FL…………………………..
Air distance to alternate. Flight Level.
W/C……………………......
Wind component.
TIME…………………........
Estimated time en-route.
FUEL…………………........
Estimated fuel burn en-route.
ALTN - 1…..…………....
Primary alternate (up to 4 permitted)
VDPP/PNH......…………….
Alternate airport (ICAO/IATA)
MSA 073 ………………….
Minimum safe altitude (grid MORA data).
TTK 292……..………….....
True track to alternate
GDIST 138…….………......
Ground distance to alternate.
ADIST 139.........................
Air distance to alternate.
FL 180……….……….......
Flight level to alternate.
W/C P001……………........
Average wind speed to alternate
TIME 00.35……………….. FUEL 392……………........
Time to alternate. Fuel to alternate.
27.
28.
with
airway
and
significant
5.1/P8
FLIGHT PLANNING Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
29.
DIST………………………..
Distance to en-route alternate from ETP.
W/C……………………......
Wind component to en-route alternates.
CFR……………………......
Critical fuel required.
FOB……………………......
Fuel on board.
XFR……………………......
Extra fuel required.
ETP1…………………........ VDSR/VDPP………….......
Equal time point 1. En-route alternate airports.
0066/0066…………….......
Distance from ETP’s to en-route alternates.
P003/M003………………..
Average wind component from ETP’s to en-route alternates.
00000…………………....... 001160…………………….
Fuel required from ETP’s to en-route alternates. Fuel on board at ETP’s.
00000…………………......
Extra fuel required.
31.
N12378E104366…….......
Lat/long coordinates of ETP.
32.
VDSR ELEV 00059FT......
VVNB elevation (departure elevation).
33.
AWY……………………….. FIX…..……………………...
Airway identifier. Waypoint identifier.
OAT………………………..
Outside air temperature
FL…………………………..
Flight level.
TAS……………………......
True airspeed.
GS..……………………….. MCSE..…………………….
Ground speed. Magnetic course.
ZDIST…………………......
Zone distance – Between check points
ZTIME...............................
Zone time
ETA……………………...... ECBO................................
Estimated Time of Arrival – fill in area. Estimate cumulative burn off fuel
TIME..…………………...... EFOB………………….......
Remaining time. Estimated fuel remaining on board
30.
5.1/P9
FLIGHT PLANNING Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
34.
FREQ………………….......
Navaid frequency.
MSA………………………..
Minimum Safe Altitude (grid MORA data).
WIND………………….......
Wind direction and speed.
ITCS………………………..
Indicated true course
RDIST…………………......
Remaining distance
CTIME……………………..
Cumulative time
ATA……………………...... ACBO…………………......
Actual Time of Arrival – fill in area. Actual cumulative burn off fuel – fill in area.
AFOB……………………..
Actual fuel remaining on board – fill in area.
35.
Body of flight plan……......
Includes all relevant data.
36.
Body of flight plan……......
Includes all relevant data.
37.
VVDN ELEV 00033FT......
VVDN elevation (arrive elevation).
38.
VVNB N21133E105483…..
Name and coordinates of flight plan waypoints.
39.
ALTERNATE DATA….......
Header line for alternate data.
40.
-N0245F080 W2…….........
Route summary from arrival airport to alternate airport.
41.
CPT…………………………
Checkpoint.
LAT……………………....... LONG………………….......
Latitude. Longitude.
MCS………………………..
Route segment magnetic course.
DIST………………………..
Route segment distance.
42.
Body of alternate plan……
Includes all relevant data.
43.
FPL-XXXXXX-IS……........
Flight Plan – Call Sign – IFR Scheduled.
5.1/P10
FLIGHT PLANNING Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
44.
AT72/M- SGDH/S..............
Type of aircraft/wake turbulence Equipment and transponder code.
45.
VDSR0800…………….......
Departure airport and ETD.
46.
N0269F230 W15 PNH.......
Speed, Flight Level and route of flight.
47.
VVTS0108 VDPP………...
Arrival airport, trip time and alternate airport.
48.
EET/VVTS0054………......
Estimated Elapsed Time to FIR boundaries.
49.
REG/VN-B212 SEL/LSCF……………........
Aircraft registration and SELCAL code.
E/0218……………………..
Endurance – time.
P/TBN…………………......
Persons on Board.
R/UV….…..…………........
Radio.
S/MJ……………………......
Survival equipment.
J/L..…………………........
Life jackets.
D/ C ..................................
Dinghies, number, capacity and colour.
51.
A/BLUE..…………
Aircraft colours.
52.
C/………………………......
Name of pilot in command.
53.
END OF JEPPESEN DATAPLAN………………..
Jeppesen end statement.
50.
category
–
5.1/P11
FLIGHT PLANNING ATR-72 STANDARD OPERATING PROCEDURES
5.1.3
Rev 00 15 Jul 09
Fuel Calculations
Refer Company Policy & Administration Manual, Chapter 8.1.7 for Company fuel policy.
5.1/P12
FLIGHT PLANNING Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
ATR-72 STANDARD OPERATING PROCEDURES
SECTION 6 MASS AND BALANCE
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
MASS AND BALANCE
TABLE OF CONTENTS ATR-72 STANDARD
TOC/P1 Rev 00 15 Jul 09
OPERATING PROCEDURES
6.1
MASS AND BALANCE
6.1/P1
6.1.1
General
6.1/P1
6.1.2
Departure Control System (DCS)
6.1/P1
6.1.3
Load Sheet and Balance Chart
6.1/P1
MASS AND BALANCE
TABLE OF CONTENTS ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
TOC/P2 Rev 00 15 Jul 09
MASS AND BALANCE
6.1/P1 Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
6.1
MASS AND BALANCE
6.1.1
General
Aircraft mass and balance information including Dry Operating Weight(s) and Dry Operating Indices for each particular ATR-72 aircraft is included in the aircraft’s library. 6.1.2
Departure Control System (D.C.S)
Aside from the Company standard format DCS generated load and balance sheet there are also a number of different formats of Departure Control Systems in use by ground handling companies. These systems are self evident in the presentation of the weight and balance data necessary for the calculation of takeoff performance. 6.1.3
Load Sheet and Balance Chart
The ATR-72 aircraft utilises a combined Load Sheet and Balance Chart that is compiled as follows: (a)
Enter the DOW (Dry Operating Weight) in the DOW field, make any appropriate adjustments and determine the ADJ DOW;
(b)
Enter the fuel load in the TAKEOFF FUEL field and sum to ADJ DOW to determine the OPERATING WEIGHT;
(c)
Complete the fields MAX-ZFW, MAX-TOW and MAX LW to determine ALLOWED TFC LOAD;
(d)
Calculate the TOTAL TRAFFIC LOAD and enter the DRY OPER WEIGHT to determine ZERO FUEL WEIGHT;
(e)
Enter TAKEOFF FUEL and sum to ZERO FUEL WEIGHT to determine TAKEOFF WEIGHT;
(f)
Enter TRIP FUEL and deduct from TAKEOFF WEIGHT to determine LANDING WEIGHT;
(g)
Make any appropriate adjustments to the DOI (Dry Operating Index) in the field designed for this purpose then enter the balance grid with the ADJ DOI and draw down through the index scale (in the direction of the slope) to account for: (i)
Passengers in compartments A, B and C;
(ii)
Baggage and cargo in the forward and aft cargo compartments.
MASS AND BALANCE ATR-72 STANDARD OPERATING PROCEDURES
6.1/P2 Rev 00 15 Jul 09
(h)
From the last obtained point draw a vertical line to intercept the horizontal line corresponding to the actual zero fuel weight and check that the intersection point is within the zero fuel weight operation limits (dotted lines) and not above the maximum zero fuel weight for the aircraft without fuel;
(i)
From the point after passengers and baggage have been accounted for, enter the fuel grid and account for the planned fuel load;
(j)
From this point draw a vertical line to intercept the horizontal line corresponding to the actual takeoff weight and check that the intersection point is within the takeoff and landing certified limits and not above the maximum takeoff weight;
(k)
Determine the takeoff weight centre of gravity in percentage MAC and continue down to the determine the stabilizer setting at the takeoff weight;
(l)
Following the vertical line associated with the takeoff condition return upwards to the fuel zone, subtract the trip fuel quantity then return back to the centre of gravity grid to ensure that the landing weight is within the takeoff/landing certified limits and not above the maximum landing weight.
MASS AND BALANCE ATR-72 STANDARD OPERATING PROCEDURES
6.1.4
6.1/P3 Rev 00 15 Jul 09
LAST MINUTE CHANGE PROCEDURE Last minute change means any change concerning passengers, baggage, cargo, mail, fuel occurring after the using of the load sheet. This LMC must immediately be communicated as soon as noticed by traffic agent if take- off weigh variation exceeds ± 300 kg. The following must be checked: No weight limitation is exeeded. MACTON and MACZFW remain within the limit. If the LMC exeed 300kg , the new Loadsheet and Balance sheet have to be issued. -
MASS AND BALANCE
6.1/P4 Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
ATR-72 STANDARD OPERATING PROCEDURES
SECTION 7 LOADING
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
LOADING ATR-72 STANDARD OPERATING PROCEDURES
7.1
LOADING
Refer Company ATR-72 Weight and Balance Manual.
7.1/P1 Rev 00 15 Jul 09
LOADING
7.1/P2 Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
ATR-72 STANDARD OPERATING PROCEDURES
SECTION 8 CONFIGURATION DEVIATION LIST
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
CONFIGURATION DEVIATION LIST ATR-72 STANDARD OPERATING PROCEDURES
8.1
8.1/P1 Rev 00 15 Jul 09
CONFIGURATION DEVIATION LIST
Refer Company Policy and Administration Manual, Chapter 8.6. SSCA approved ATR-72 Configuration Deviation List is included in the flight deck documentation library.
CONFIGURATION DEVIATION LIST
8.1/P2 Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
ATR-72 STANDARD OPERATING PROCEDURES
SECTION 9 MINIMUM EQUIPMENT LIST
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
MINIMUM EQUIPMENT LIST ATR-72 STANDARD OPERATING PROCEDURES
9.1
9.1/P1 Rev 00 15 Jul 09
MINIMUM EQUIPMENT LIST
Refer Company Flight Operations Manual, Chapter 8.6. SSCA approved ATR-72 Minimum Equipment List is included in the flight deck documentation library.
MINIMUM EQUIPMENT LIST
9.1/P2 Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
ATR-72 STANDARD OPERATING PROCEDURES
SECTION 10 EMERGENCY EQUIPMENT
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
EMERGENCY EQUIPMENT
TOC/P1
TABLE OF CONTENTS
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
10.1
EMERGENCY EQUIPMENT
10.1/P1
10.1.1
General
10.1/P1
10.1.2
Emergency Equipment Location
10.1/P1
10.1.3
Portable Oxygen
10.1/P3
10.1.4
Water (H20) Extinguisher
10.1/P6
10.1.5
HALON Fire Extinguisher (Type 1)
10.1/P8
10.1.6
HALON Fire Extinguisher (Type 2)
10.1/P10
10.1.7
Protective Breathing Equipment (PBE)
10.1/P12
10.1.8
Life Vests
10.1/P21
10.1.9
Miscellaneous Safety Equipment
10.1/P25
EMERGENCY EQUIPMENT
TOC/P2
TABLE OF CONTENTS
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
10.1/P 1
EMERGENCY EQUIPMENT ATR-72 STANDARD OPERATING PROCEDURES
10.1
EMERGENCY EQUIPMENT
10.1.1
General
Rev 00 15 Jul 09
Cabin crew is responsible for the serviceability checking of all cabin emergency equipment in accordance with procedures detailed in the Cabin Crew Manual. The Purser shall report to the Commander prior to departure that this check has been satisfactorily completed. The flight deck crew is responsible for the serviceability checking the flight deck emergency equipment. 10.1.2
Emergency Equipment Location
Portable emergency equipment is stowed at strategic locations throughout the aircraft. This may include: (a)
Life vests;
(b)
Portable breathing equipment;
(c)
Emergency locator transmitter(s) (ELT’s);
(d)
Halon fire extinguishers;
(e)
Water fire extinguishers;
(f)
First aid kits;
(g)
Megaphone(s);
(h)
Flashlights;
(i)
Crash axe(s)/crow bar(s);
(j)
Flight deck escape ropes;
(k)
Life rafts.
Refer the following flight deck and passenger cabin emergency equipment layout diagrams specific for locations.
10.1/P 2
EMERGENCY EQUIPMENT Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
EMERGENCY EQUIPMENT LAYOUT VN-B227, B231
FWD ATTENDANT SEAT STW 01 Water Fire extinguisher bottle
Flight desk 03 Crew lifevests 03 Crew oxygen masks 03 Smoke goggles 02 Flash lights 01 Crash Axe 01 Emer Escape rope 01 Fire flighting gloves 01 Fire extinguisher BCF (halon 1211) FWD PARTITION SAFETY STW 01 Protective breathing equip(PBE) FWD ATTENDANT 01 First aid kit stowage) (underseat
01 Oxygen bottle with first aid mask 01 Flash lights 01 ATTENDANT Crew life vest FWD (underseat stowage) 01 Oxygen bottle with first aid mask 01 Flash lights 01 Crew life vest 02 Oxygenmask keys
AFT LEFT STOWAGE 01 First kit STOWAGE LHaid AFT 01 Fire BCF bag 01extinguisher First aid oxygen (Halon 1211) containing 4 oxygen masks 01 Protective Breathing equipment(PBE) 01 Megaphone 01 Emer medical kit (EMK)
C/A SEAT AFT AFT PARTITION SAFETY STW 01 Fire BCF(4.25 cuft) with 01extinguisher Oxygen bottle (halonfirst 1211) aid mask 01 Protective 01 Flashbreathing lights equip(PBE) 01 Crew life vest 01 Fire extinguisher BCF (halon 1211)
10.1/P 3
EMERGENCY EQUIPMENT Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
10.1.3
Portable Oxygen
10.1.3.1
General
Portable oxygen bottles are installed with oxygen masks that include a moulded face-piece, re-breather bag and elastic restraining strap that are individually wrapped for hygienic reasons. A supply tube is also provided. Portable oxygen bottles can be used by passengers with breathing difficulties or by cabin crew as a walk around bottle following a depressurisation and an emergency descent. Portable oxygen bottles are not suitable for use during the fighting of an in-flight fire because the masks have holes in the sides that allow cabin air to enter the mask. The portable oxygen cylinder is fitted with a HI outlet and a LO outlet, a quantity/contents gauge and a yellow ON-OFF control knob. The following table details flow rate and duration based upon oxygen bottle 100% full: Bottle Size
10.1.3.2
Flow Rate (litres/min)
Duration (minutes)
HI
LO
HI
LO
310 litre (passenger)
4
2
77
155
120 litre (crew)
4
2
30
60
Pre-Flight Check
During the pre-flight inspection of oxygen bottles the following should be observed: (a)
The bottle quantity/contents gauge indicates 3/4 full or 1500 psi;
(b)
The bottle is secured in its brackets;
(c)
The dust caps are in position;
(d)
There is no oil or grease on the fittings;
(e)
There is a mask taped to each bottle; and
(f)
There is a serviceable shoulder strap.
10.1/P 4
EMERGENCY EQUIPMENT Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
10.1.3.3
Operation
(a)
Push aside or remove dust cover and insert metal connector of mask tube into the HI outlet ensuring that it “clicks” into position;
(b)
Turn yellow control knob ON; Note: With the yellow control knob ON, inserting the mask connector into one of the two outlets starts the oxygen flowing. Removal of the mask connector stops the oxygen flow.
(c)
After using oxygen turn yellow control knob OFF (finger tight) and remove the mask connector. SCOTT PORTABLE OXYGEN BOTTLE
10.1/P 5
EMERGENCY EQUIPMENT ATR-72 STANDARD OPERATING PROCEDURES
10.1.3.4
Rev 00 15 Jul 09
Precautions When Using Oxygen
When using a portable oxygen bottle the following precautions should be taken: (a)
As oxygen promotes combustion there is to be no smoking within a 3 metres radius of the passenger using oxygen (approximately 3 passenger rows either side);
(b)
Ensure that the oxygen bottle fittings are free from any oil or grease as such contaminants can cause combustion;
(c)
Turn the ON/OFF valve slowly and do not over tighten when closing;
(d)
Before putting on the mask wipe away any heavy lipstick or grease from the mouth area;
(e)
Ensure tubing is not kinked and that oxygen is flowing (filling of rebreather bag) before fitting the mask with an efficient seal to the passenger's face. Some oxygen masks are fitted with a ‘green indicator flow valve’. When oxygen is flowing to the mask, the indicator (normally clear or sometimes red) will turn green;
(f)
If it is necessary to use a portable oxygen mask on an infant, reverse the mask (nose part under the chin) and hold gently against the face. The rebreather bag should be held vertically to ensure the free flow of oxygen;
(g)
Oxygen therapy is rarely detrimental to a patient and its value far outweighs the very rare problems caused by its use. The passenger will normally be able to advise the position in which he/she breathes easiest. If required and available, cabin crew should seek assistance from a medically qualified passenger(s); and
(h)
When the pressure gauge indicates less than 200 psi the valve should be turned off and the bottle considered empty.
10.1/P 6
EMERGENCY EQUIPMENT ATR-72 STANDARD OPERATING PROCEDURES
10.1.4
Water (H2O) Fire Extinguisher
10.1.4.1
General
Rev 00 15 Jul 09
Water (H2O) extinguishers are designed for extinguishing smouldering fabric or waste fires and should NEVER be used on a fire originating from an electrical source. Accordingly, water (H2O) extinguishers should never be used for a fire in the galley area. 10.1.4.2
10.1.4.3
10.1.4.4
Pre-Flight Check
(a)
Ensure that the extinguisher is secured in its brackets;
(b)
The lock-wire seal is intact; and
(c)
That the CO2 cartridge is visible though the hole in the handgrip.
Note:
If the locking wire is broken unscrew the handgrip by turning it anticlockwise and check the cartridge for puncture.
Operation
(a)
Remove from bracket;
(b)
Hold extinguisher upright;
(c)
Turn handle clockwise rapidly to the limit of its travel, breaking the locking wire; and
(d)
Holding the extinguisher upright aim at the base of the fire and depress the trigger with the thumb.
Precautions
(a)
Do not discharge directly at a person;
(b)
Do not use to fight a fire in the flight deck;
(c)
Do not drink contents in a survival situation.
10.1/P 7
EMERGENCY EQUIPMENT Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
WATER (H2O) FIRE EXTINGUISHER
10.1/P 8
EMERGENCY EQUIPMENT ATR-72 STANDARD OPERATING PROCEDURES
10.1.5
HALON Fire Extinguisher (Type 1)
10.1.5.1
General
Rev 00 15 Jul 09
This type of fire extinguisher is designed for extinguishing electrical and flammable liquid fires and is suitable for ALL types of fires in an aircraft. The extinguishing agent is a vaporising liquid that interrupts the chemical reaction taking place in the flames thereby extinguishing the fire. It is a colourless, noncorrosive liquefied gas that can give off an acrid odour that can cause running of the eyes and nose. 10.1.5.2
Pre-Flight Check
(a)
Check that the pressure indicator is positioned in the green range indicating acceptable pressure charge; and
(b)
That the ring pin is in place with the seal intact. Note: The extinguisher is serviceable even if the plastic seal of the ring pin is broken, provided that the pressure gauge is in the green band.
10.1.5.3
10.1.5.4
Operation
(a)
Remove from bracket;
(b)
Remove ringed safety pin from the lever and handle;
(c)
Hold the extinguisher upright with the fingers of one hand under the handle and the thumb on the top of the lever. The other hand should be placed on the bottom of the bottle to steady it if necessary; and
(d)
Aim the extinguisher at the base of the fire and press the lever down with the thumb.
Note:
Duration of discharge from the small size bottle is approximately six (6) seconds and twelve (12) seconds from the large size bottle.
Precautions
(a)
Do not discharge directly at a person;
(b)
Discharge distance should be between 1.5 and 2 metres with an open fire in the cabin. In the case of a fire in a confined space the extinguisher should be held as close as possible.
10.1/P 9
EMERGENCY EQUIPMENT ATR-72 STANDARD OPERATING PROCEDURES
HALON FIRE EXTINGUISHER (TYPE 1)
Rev 00 15 Jul 09
10.1/P 10
EMERGENCY EQUIPMENT Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
10.1.6
HALON Fire Extinguisher (Type 2)
10.1.6.1
General
The extinguishing agent has the same properties as the HALON fire extinguisher (Type 1) above. 10.1.6.2
Pre-Flight Check
Check the red indicator disc is in place and that the sealing wire is intact. Note: If the red disc or sealing wire are missing the weight of the extinguisher should be compared with a serviceable bottle to determine if the contents are still intact. If not, the extinguisher must be replaced. 10.1.6.3
10.1.6.4
Operation
(a)
Remove from bracket;
(b)
Raise safety catch on the back of the operating head by pushing up with the thumb;
(c)
Grasp the operating handle and put the forefinger through the loop provided at the same time firmly pressing the trigger at the back of the handle with the heel of the hand;
(d)
Initial depression of the trigger will cause the red disc to fall out and a little additional effort is required to break the sealing disc of the extinguisher;
(e)
Hold extinguisher at an angle within 60 of vertical position;
(f)
Firmly squeeze the actuation trigger; and
(g)
Ensure that the discharge nozzle head is pointing toward the fire before operating.
Note:
Duration of discharge is approximately thirteen (13) seconds.
0
Precautions
(a)
Do not discharge directly at a person;
(b)
Discharge distance should be between 1.5 and 2 metres with an open fire in the cabin. In the case of a fire in a confined space the extinguisher should be held as close as possible.
10.1/P 11
EMERGENCY EQUIPMENT ATR-72 STANDARD OPERATING PROCEDURES
HALON FIRE EXTINGUISHER (TYPE 2)
Rev 00 15 Jul 09
10.1/P 12
EMERGENCY EQUIPMENT ATR-72 STANDARD OPERATING PROCEDURES
10.1.7
Protective Breathing Equipment (PBE)
10.1.7.1
General
Rev 00 15 Jul 09
Protective breathing equipment (PBE) is a breathing apparatus designed to protect the wearer's eyes and respiratory tract from the effects of smoke and toxic fumes while fighting an in-flight fire. The following general features apply to all types of PBE’s installed on Company aircraft: (a)
They are designed to enclose the head within an elastic neck seal and provide for a minimum of 15 – 20 minutes (depending upon the manufacturer) of breathable air from a chemical generator;
(b)
They can be worn by persons with glasses, jewellery, a beard or a hair bun;
(c)
They are installed with a neck shield (of varying length depending upon manufacturer) that extends downward from the hood to protect the collar and upper shoulder area; and
(d)
They have features that permit the wearer’s voice to be heard outside the PBE.
Note:
Excess make-up should be removed before donning a PBE as contact between grease and oxygen can cause burns.
Wearer’s should be aware that although the head area is protected, the rest of the body is not and the wearer should guard against a feeling of invincibility. Company aircraft are installed with one of three types of protective breathing equipment as detailed below.
10.1/P 13
EMERGENCY EQUIPMENT Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
10.1.7.2
Puritan Bennett PBE
This PBE is a demand device which means that more strenuous the work the more oxygen will be produced. (a)
(b)
Pre-Flight Check: (i)
Inspect that the PBE unit is visible through access door;
(ii)
Confirm that the white tamper proof seals located at the top and bottom of the access door are intact; and
(iii)
Ensure that the foil pouch is in place and is not obviously expanded.
Operation: (i)
Open the container by pulling the red handle. Pull the red tag to open the foil pouch and pull out on the blue aural/nasal cone and remove the hood;
(ii)
Place both hands inside the neck seals, palms facing each other and visor facing downward. Guide the hood over the head and down over the face using the hands to shield the face and glasses from the blue cone ensuring that hair clothing and jewellery is clear of the neck seal;
(iii)
Using both hands pull the neck shield down over the collar and shoulders; and
(iv)
Grasp both adjustment straps at the lower corner of the visor and pull forward simultaneously to activate the oxygen canister, then backward to seal the cone over the nose and mouth. Oxygen will inflate the hood.
(v)
If required, adjust glasses through the fabric, not through the neck seal. Note: The blue cone must be positioned high on the nose with a firm seal otherwise fogging may occur. If the hood begins to deflate and becomes hot and moist the oxygen supply is depleted and the PBE must be removed.
10.1/P 14
EMERGENCY EQUIPMENT Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
(c)
Abnormal Operation (i)
Failure of Starter Candle If the starter candle fails to activate when the adjustment strap is pulled an additional sharp pull on the strap may be adequate to actuate the device. If the device still fails the hood will continue to function. Placing fingers into the neck seal may be required to enable sufficient breathing volume until the chemical generator begins supplying oxygen.
(ii)
Loss of Neck Seal The continued presence of strong irritating odours inside the hood that results in eye and respiratory tract discomfort is an indication of an ineffective neck seal. Ensure that the neck seal is in contact with the skin and that the seal is not disrupted by hair or jewellery. If the condition persists or there is evidence of a tear in the neck seal, the wearer should quickly go to a safe area and remove the hood and don an alternative unit.
(d)
Removal (i)
Move away from fire and/or toxic fumes area;
(ii)
Push adjustment buckles forward with thumbs to release straps;
(iii)
Place both hands under neck seal and ease up over face;
(iv)
Stow PBE in a safe dry place and allow it to cool; and
(v)
Brush hair with hands to break down any oxygen build up.
10.1/P 15
EMERGENCY EQUIPMENT Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
PURITAN – BENNETT PBE
10.1/P 16
EMERGENCY EQUIPMENT Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
10.1.7.3
Drager PBE
The oxygen canister can be activated by just breathing into the oral-nasal mask but to start the chemical reaction by this method takes a few seconds, therefore pulling the black quick-start toggle is the more immediate method of activation. (a)
(b)
(c)
Pre-Flight Check: (i)
Check container seal is intact and the yellow serviceability serviceability indicator is not broken; and
(ii)
The container is not broken.
Operation: (i)
Open container and remove foil bag containing the hood;
(ii)
Pull red tear strip at top of foil bag and remove hood;
(iii)
Place hood over head ensuring that the breathing bag cover is to the front over the chest;
(iv)
Ensure that the neck seal is free of obstruction (e.g. hair, clothes collar, etc) and that the head harness is pulled down for a secure fit;
(v)
Fit oral-nasal mask securely to the nose and mouth and pull black quick start toggle to activate; and
(vi)
Fit tie strap around the waist.
Abnormal Operations: If the hood collapses onto the head during inhalation or there is an increased breathing resistance check the fitting of the oral-nasal mask as the cause may be an incomplete respiration back to the breathing back due to leakage or an empty oxygen source. After correcting the fitment of the oral-mask check the equipment by making five (5) deep breaths. If the collapsing of the hood or increased resistance occurs again either the oxygen reserve has been used up or the hood is defective and should be removed.
10.1/P 17
EMERGENCY EQUIPMENT Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
(d)
Removal: (i)
Move away from fire and/or toxic fumes area;
(ii)
Release the tie strap;
(iii)
Place both hands under neck seal and ease up over face;
(iv)
Stow PBE in a safe dry place and allow it to cool; and
(v)
Brush hair with hands to break down any oxygen build up. DRAGER PBE
10.1/P 18
EMERGENCY EQUIPMENT Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
10.1.7.4
Scott PBE
(a)
Pre-Flight Check: (i)
A date/month/year date/month/year stamp should be visible, but set back through the round inspection window. Note: If the date/month/year stamp appears to be firmly pressed against the inspection window, as if the inside of the container is pressurised, the PBE should be further checked for serviceability.
(ii)
(b)
If the vacuum sealed bag is soft and not tightly formed around the hood, or if the humidity indicator inside the bag has changed colour from blue to pink, the unit is unserviceable.
Operation: (i)
Open the storage case by lifting the latch marked “LIFT” and remove sealed unit from the storage case;
(ii)
Grasp the red strip and tear open the sealed bag and remove the PBE from bag;
(iii)
Hold the hood and pack firmly against the body with one hand and with the other hand pull the ring marked “PULL TO ACTUATE” in the direction indicated. The unit will be actuated when the ring and the pin pull free; Note: unit.
A flow of oxygen should be audible, if not discard the
(iv)
Grip the hood around the neck seal edge with the oxygen pack away from the body, bend forward from the waist and pull hood over the chin, across the face and over the head. Stand upright and pull hood down until the headband engages the forehead; and
(v)
Ensuring that hair, jewellery or clothing is clear of the neck seal in order to make a tight seal around the neck pull the skirt of the hood fully down over the chest and shoulders.
10.1/P 19
EMERGENCY EQUIPMENT Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
Note: It is normal to hear the sound of oxygen rushing into the hood, indicating that the oxygen generator is operating correctly. Once the noise ceases move to a safe area and immediately remove the hood. Heat is produced by the generator and may cause minor discomfort inside the hood, but it is no cause for alarm. The generator pack should not be touched during and after operation due to heat build-up. (c)
Removal: (i)
Move away from the fire or toxic area; and
(ii)
Pull the hood from the back forwards and over the head.
(iii)
Stow PBE in a safe dry place and allow it to cool; and
(iv)
Brush hair with hands to break down any oxygen build up.
10.1/P 20
EMERGENCY EQUIPMENT Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
SCOTT PBE
10.1/P 21
EMERGENCY EQUIPMENT ATR-72 STANDARD OPERATING PROCEDURES
10.1.8
Life Vests
10.1.8.1
General
Rev 00 15 Jul 09
Life vests are carried on all Company aircraft and are normally stowed in a container attached to the underside of the passenger seats. The following section contains information on life vests from various manufacturers that may be installed on Company aircraft. Life vests installed on Company aircraft consist of the following components: (a)
Pressurised cylinder(s) as the primary means of inflation, activated by pulling on one or two (depending upon the number if chambers) red toggles that hangs from the bottom of the vest;
(b)
A mouth inflation valve for secondary inflation that can be used to inflate the life jacket by blowing into one or two (depending upon the number of chambers) mouthpieces. The life jacket can be deflated by depressing the pin in the centre of the mouthpiece(s);
(c)
A whistle for attracting attention; and
(d)
A light, with a continuous life of approximately 20 hours that is connected to a water sensitive battery and activated automatically immediately on contact with water.
Life vests are designed to ensure that an unconscious or injured person will automatically roll face upward in the water. 10.1.8.2
Double Chamber Life Vest Operation
(a)
Remove vest from its stowage, tear off the plastic container and un-roll the vest;
(b)
Put the vest over the head with the larger portion of it in the front over the chest;
(c)
Secure the tapes around the waist by the clip(s) provided;
(d)
To inflate the vest, pull down firmly on both red toggles.
10.1/P 22
EMERGENCY EQUIPMENT Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
Note: Life vests worn by adults must not be inflated in the aircraft cabin. It may be impossible for an adult wearing an inflated life jacket to evacuate through a window exit. If a passenger is evacuating through a door exit the jacket may be inflated just prior to leaving the aircraft. Life vests worn by small children and persons incapable of inflating the life jacket may be inflated at the exit area, just prior to leaving the aircraft. DOUBLE CHAMBER LIFE VEST
10.1/P 23
EMERGENCY EQUIPMENT Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
10.1.8.3
Single Chamber Life Vest Operation
(a)
Adult: (i)
Remove vest from its stowage, tear off the plastic container and unroll the vest;
(ii)
Put the vest over the head with the larger portion of it in the front over the chest;
(iii)
Secure the tapes around the waist and tie them in the front towards the side of the body with double knots;
(iv)
To inflate the vest, pull down firmly on the red toggle. Note: Life vests worn by adults must not be inflated in the aircraft cabin. It may be impossible for an adult wearing an inflated life jacket to evacuate through a window exit. If a passenger is evacuating through a door exit the jacket may be inflated just prior to leaving the aircraft. Life vests worn by small children and persons incapable of inflating the life jacket may be inflated at the exit area, just prior to leaving the aircraft.
(b)
Use on a Child (i)
Remove vest from its stowage, tear off the plastic container and unroll the vest;
(ii)
Inflate the vest by pulling the red toggle;
(iii)
Place vest over child’s head (partially deflate, if necessary);
(iv)
Cross tapes at the back and tie in a single knot over the inflated life vest and a double knot at the back.
10.1/P 24
EMERGENCY EQUIPMENT ATR-72 STANDARD OPERATING PROCEDURES
SINGLE CHAMBER LIFE VEST (ADULT AND CHILD USE)
Rev 00 15 Jul 09
10.1/P 25
EMERGENCY EQUIPMENT Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
10.1.9
Miscellaneous Safety Equipment
10.1.9.1
Megaphone
Portable battery operated megaphones (loud hailers) are carried on board Company aircraft to provide the means for cabin crew (and flight deck crew, if necessary) to control passengers during evacuation when the PA system is inoperative or to control passengers when outside the aircraft following an evacuation. The megaphone may be used in the cabin only in emergency situations when the PA system has failed. It is not to be used for normal passenger briefing or for making non safety related announcements. The megaphone consists of a microphone, amplifier, battery, trumpet shaped loud speaker and a carrying strap. The following general rules apply to megaphone use:
10.1.9.2
(a)
When used inside the aircraft the megaphone should be pointed down the central length of the cabin;
(b)
When used outside the aircraft announcements should be made and repeated a number of times in different directions as the sound is emitted in a narrow beam which is not easily audible on either side;
(c)
Speak slowly, calmly and do not shout as this can distort the speech.
Emergency Torch
All Company aircraft are fitted with emergency torches (flashlights) that are located near cabin crew seats and in the flight deck. These torches are for emergency use only. The torch is waterproof, but will not float and has a wrist strap attached to the base. When activated, the torch will operate for approximately six hours. (a)
Pre-Flight Check (i)
Ensure torch correctly positioned in stowage with the plastic guard in place and with the lead seal intact; and
(ii)
That the red light is flashing in 3 to 10 seconds intervals.
Note:
If the interval is longer than 10 seconds, the battery power is low and they should be replaced.
10.1/P 26
EMERGENCY EQUIPMENT Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
(b)
Operation (i)
Pull the torch out from its stowage mount. This action turns the light on;
(ii)
Wear the wrist-strap over the wrist to prevent from loss during evacuation.
Note 1:
In survival situations (when a torch needs to be carried unilluminated), unscrew the bottom cap of the torch, disconnect the plug inside and replace the cap. Reverse this procedure to reactivate the torch when required.
Note 2:
On some aircraft, the torch is fitted with an ON/OFF switch. During the pre-flight check the switch should be turned on to ensure the torch operates correctly. EMERGENCY TORCH
10.1.9.3
Heat Resistant Gloves
One set of heat resistant gloves are stowed in the flight deck and are to be used for protection in the case of an in-flight fire.
10.1/P 27
EMERGENCY EQUIPMENT ATR-72 STANDARD OPERATING PROCEDURES
10.1.9.4
Rev 00 15 Jul 09
Crash Axe
Company aircraft have a crash axe installed in the flight deck that can be used to open panels in the case of an in-flight fire. The handle is insulated to prevent electric shock if a cable is cut during fire fighting. 10.1.9.5
First Aid Kit
There are first aid kits of varying sizes containing at least the following basic first aid supplies that can be used in the case of a medical emergency: (i)
Compressed Wound Dressings;
(ii)
Bandages and splints;
(iii)
Triangular bandages;
(iv)
Adhesive strapping;
(v)
Tablets and medicines for head ache and other common ailments;
(vi)
A pair of scissors, burn ointment and antiseptic swabs;
(vii)
Latex gloves.
If an emergency first aid kit is opened, the purser must submit a report to the Cabin Crew Unit outlining the circumstances requiring its use. Additionally, an entry should be made in the Cabin Technical Log for the supply of a replacement emergency first aid kit.
10.1/P 28
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ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
ATR-72 STANDARD OPERATING PROCEDURES
SECTION 11 EMERGENCY EVACUATION PROCEDURES
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
EMERGENCY EVACUATION PROCEDURES
TOC/P1
TABLE OF CONTENTS
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
11.1
EMERGENCY EVACUATION PROCEDURES
11.1/P1
11.1.1
Categorisation of Emergency Landings
11.1/P1
11.1.2
Flight Deck Procedures
11.1/P2
11.1.3
Evacuation Responsibility
11.1/P3
11.1.4
Evacuation PA Announcements
11.1/P4
11.1.5
Evacuation
11.1/P4
EMERGENCY EVACUATION PROCEDURES
TOC/P2
TABLE OF CONTENTS
Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
INTENTIONAL BLANK PAGE
EMERGENCY EVACUATION PROCEDURES ATR-72 STANDARD OPERATING PROCEDURES
11.1
EMERGENCY EVACUATION PROCEDURES
11.1.1
Categorisation of Emergency Landings:
11.1/P1 Rev 00 15 Jul 09
Emergency landings are categorised as follows: (a)
Prepared Emergency Landing An emergency landing where there is sufficient time for cabin and passenger preparation.
(b)
Unprepared Emergency Landing Is an emergency landing where it is necessary to land the aircraft as soon as possible.
An emergency landing is further defined as follows: (a)
Forced landing Is a landing, on land away from an airport
(b)
Ditching Is a landing on water
(c)
Abnormal Landing An abnormal landing is a landing at an airport in which some aircraft damage is anticipated. An abnormal landing is to be considered if the landing gear cannot be locked fully down or some other malfunction exists and it is known or considered possible that the aircraft will be damaged during landing. In an abnormal landing, preparation for rapid evacuation should be as for either a forced landing or ditching, with the exception that it is not necessary to have passengers remove and stow certain items or loosen tight clothing. If landing gear standby indicators indicate that the landing gear is down and locked then normal procedures will apply. A tower fly past should only be conducted if there is reason to doubt that the landing gear is not fully down or there is known damage to the landing gear.
EMERGENCY EVACUATION PROCEDURES ATR-72 STANDARD OPERATING PROCEDURES
11.1.2
Flight Deck Procedures
11.1.2.1
Prepared Emergency Landing
11.1/P2 Rev 00 15 Jul 09
In all emergency situations it is important that the cabin crew are given adequate time in which to complete their passenger cabin preparation duties. As soon as it is expected that an emergency landing will be required, the SEAT BELT and NO SMOKING signs should be selected ON and the Purser summoned to the flight deck by the following PA announcement: “COCKPIT SPEAKING, PURSER REQUIRED IN COCKPIT”
The Purser is to be informed of the emergency in the following format: (a)
Nature of the emergency;
(b)
Approximate flight time available;
(c)
Type of emergency landing (forced landing, ditching or abnormal landing); and
(d)
Any other relevant information such as whether the Commander intends to make a PA announcement prior to cabin preparation or if a “BRACE” command will be given.
The Purser will repeat the Commander’s instructions to ensure that everything is completely understood prior to returning to the cabin to commence the cabin preparation. As the flight deck crew will be occupied dealing with the emergency situation the Purser is responsible for the PA announcement to the passengers detailing the nature of the emergency, the time available and the steps required in cabin preparation. If time and/or duties permit the Commander (or First Officer) should make a PA announcement providing additional appropriate information on the emergency and the anticipated landing. It is essential that this PA announcement does not over-ride the cabin preparation PA announcement being made by the Purser.
EMERGENCY EVACUATION PROCEDURES ATR-72 STANDARD OPERATING PROCEDURES
11.1/P3 Rev 00 15 Jul 09
In the case of a forced landing or ditching both pilots should loosen their collar, tie and shoe laces, remove sharp objects from pockets and, in the case of a ditching, fit a life jacket (do not inflate). The Purser must advise, or the Commander must confirm, that passenger cabin preparation has been completed prior to the commencement of final approach. All appropriate checklists must be completed. 11.1.2.2
Unprepared Emergency Landing
In the case of an unprepared emergency landing the degree of cabin preparation will depend upon the time available. As a situation requiring an unprepared landing is most likely to occur shortly after takeoff or during approach and landing the cabin should be secure with respect to cabin service items, cabin crew and passengers seated with seat belts fastened. If possible, the Commander should communicate the situation to the Purser by summoning him/her to the flight deck in accordance. If there is insufficient time the Commander (or First Officer) should make an appropriate PA announcement which will alert the cabin crew and the passengers to the emergency situation. 11.2.2.3
“Brace” Instructions
At approximately 1,500 FT the First Officer should make the following PA announcement: “CABIN CREW TAKE YOUR SEATS FOR LANDING”
At 30 seconds or approximately 300 FT before landing the First Officer should make the following PA announcement: “BRACE FOR IMPACT, BRACE FOR IMPACT” Whenever there is a possibility of a runway overrun on a rejected takeoff or of an unanticipated abnormal landing involving abnormal decelerations cabin crew should be alerted by a PA announcement: ‘BRACE FOR IMPACT, BRACE FOR IMPACT’ 11.1.3
Evacuation Responsibility
The Commander is responsible for the evacuation PA announcement. Cabin crew will only initiate evacuation when it is obvious that the aircraft must be immediately evacuated due to catastrophic circumstances.
EMERGENCY EVACUATION PROCEDURES
11.1/P4 Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
Following a rejected takeoff or a landing that does not appear normal and there are visible signs inside or outside of the cabin of an emergency situation, that may not be apparent to the flight deck crew (e.g. smoke and/or fire) the Purser shall make the following PA announcement: “PASSENGERS REMAIN INSTRUCTIONS”
SEATED
AND
AWAIT
FURTHER
The Purser will then enter the flight deck and advise the Commander of the emergency situation. The Commander will assess the situation and be responsible for the evacuation PA announcement. 11.1.4
Evacuation PA Announcements
Immediately the aircraft comes to a stop the Commander (or First Officer) shall make the following PA announcement: “COCKPIT SPEAKING, CABIN CREW TO YOUR STATIONS”
Once the Passenger Evacuation checklist is completed and evacuation is required the Commander (or First Officer) will make the following PA announcement: “EVACUATE, EVACUATE!” 11.1.5
Evacuation
If possible, pilots should proceed to the passenger cabin to assist in the emergency evacuation as follows: (a)
Assist in the opening of any suitable doors and exits.
(b)
Assist in the evacuation by directing passengers to the most suitable exit avoiding congestion and by calling in a loud, clear voice urge passengers to: “HURRY, COME THIS WAY”
(c)
In the case of a ditching instruct passengers to inflate life jackets when outside the aircraft;
(d)
If possible, the Commander or the Purser should check that all passengers have evacuated the aircraft.
EMERGENCY EVACUATION PROCEDURES ATR-72 STANDARD OPERATING PROCEDURES
11.1/P5 Rev 00 15 Jul 09
When no significant aircraft damage has occurred and cabin crew have prepared the passenger cabin for evacuation the speed of the evacuation should be a consideration. Passenger safety is the prime consideration in any emergency evacuation. The flight deck crew and cabin crew will usually be able to determine whether or not the evacuation requires utmost speed at the increased risk of injuries to individual passengers.
EMERGENCY EVACUATION PROCEDURES
11.1/P6 Rev 00 15 Jul 09
ATR-72 STANDARD OPERATING PROCEDURES
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ATR-72 STANDARD OPERATING PROCEDURES
SECTION 12 AIRCRAFT SYSTEMS
ATR-72 STANDARD OPERATING PROCEDURES
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AIRCRAFT SYSTEMS ATR-72 STANDARD OPERATING PROCEDURES
12.1
AIRCRAFT SYSTEMS
Refer FCOM, Volume 1 for information on aircraft systems.
12.1/P1 Rev 00 15 Jul 09
