Issue no: 01 Rev: 00 Effective from: June 01st, 2015.
Approval no: HQCAA/2210/78/AW
A320-200 WEEKLY CHECK (INCLUDES DAILY) *A/C REGISTRATION : _______________________ *STATION/FLIGHT NO:______________________ *DATE/TIME:______________________________ FH/FC:___________________________________
Notes: 1. ( * ) To be filled by Engineer. 2. Tasks to be accomplished every 7-calendar days (168 hours elapsed time) not exceeding the 8th day.
AIRWORTHINESS MANAGEMENT
A320-200 WEEKLY CHECK REFERENCES Item no. 1.A.8. 1.C.8. 1.C.9. 1.D. 1.E.1. 1.E.2. 1.E.3. 2.A.1. 3.A.1. 3.A.2. 3.A.3. 3.A.4. 4.A.1. 5.A.1.d. 6.A.7. 6.A.8. 6.A.9. 6.A.10. 6.E.3. 6.E.10. 6.E.11.
AMM Reference AMM 27-54-00-210-005 AMM 79-00-00-200-013 AMM 80-13-41-200-010 AMM 24-21-51-200-010 AMM 49-16-00-210-004 AMM 49-42-51-200-005 AMM 49-42-51-700-001 AMM 12-32-28-281-001 AMM 12-14-32-614-801 AMM 32-42-27-210-003 N/A AMM 12-22-32-640-001-A AMM 12-14-29-614-001 AMM 25-50-00-200-002 AMM 24-24-00-710-001 AMM 24-28-00-710-001 AMM 33-51-00-710-001 AMM 27-96-00-710-018 AMM 52-10-00-210-004 AMM 35-30-00-210-006 AMM 38-31-00-100-018
ISSUE 01 REV 00 Effective from June 01, 2015.
Related Document (MPD 275100-06-1) (MPD 792000-I1-1) (MPD 801300-I1-1) (MPD 242100-07-1) (MPD 491600-04-1) (EASA AD 2006-0153) (MPD 494251-01-1) (EASA AD 2006-0153) (MPD 494251-02-1) (EASA AD 2006-0153) (MPD 281100-01-2) (MPD 324100-01-1) (MPD 324227-01-1) (MPD 323105-02-1) (EASA AD 2014-0221) (AOT A32N006-14) (MPD 291000-14-1) (MPD 255000-01-1) (MPD 242400-01-2) (MPD 242400-01-3) (MPD 242800-01-3) (MPD 335100-01-1) (MPD 279000-05-1) (MPD 521000-01-1) (MPD 353000-05-1) (MPD 383100-06-1)
A320-200 WEEKLY CHECK SN
TASK DESCRIPTION
1.
WALKAROUND INSPECTION:
A.
EXTERNAL FUSELAGE :
MECH
AME
Note: Do the walk around inspection of external fuselage as per FIGURE 1 attached with this sheet. 1. Check exterior of fuselage including radome positively latched, avionics equipment vent air inlet valve, Ram air Inlet flap, pack air intake / outlet, ram air turbine doors, flight control surfaces and empennage / APU area exhaust, drain mast and vents (air intake flap closed) as far as visible from ground – for condition, cleanliness and fluid leaks. 2. Do general visual inspections of the lower half of the fuselage from the ground during the aircraft walk-around. 3. Check for presence, condition, clear and cleanliness of Pitot & Static ports, all probes sensors and crew oxygen cylinder over Pressure indicator (Green disc). 4. Inspect belly fairing access panels & wing-to-fuselage fairings for missing fasteners. 5. Do a general visual inspection of the stabilizers and the rear fuselage from the ground during the aircraft walk-around. 6. Make a GVI of the MLG from ground as far as visible & MLG doors. 7. Do a GVI of wing lower surface. This includes the slats and flaps. 8. Check flap attachment bearing no.1 for liner migration. (Only on AP-BLH) 9. Do a general visual inspection of the passenger/crew doors, the emergency exits and the cargo doors as far as visible from the ground during the aircraft walkaround. 10. Check all antennas and static dischargers for their condition & any visible damage. Note: Where applicable, while inspecting the above items makes sure that there is no damage, corrosion, leaks or cracks on all the parts of the components and the structure. B.
NLG/MLG SHOCK STRUTS: 1. Check NLG / MLG shock absorber for Normal extension and cleanliness. 2. Carry out cleaning of shining portion of Main and Nose Landing Gear Shock Strut telescoping member.
C.
ENGINES NACELLES AND PYLONS 1. GVI of power plants, nacelles & pylons of engine 1 & 2 as far as visible from ground. 2. Check visually Engines & Pylons (Cowling closed) for general condition including: Cowling panel, air outlets security of latches, lip skin, intake cowl and engines/pylons drain masts for no obstruction and evidence of leakage. ISSUE 01 REV 00 Effective from June 01, 2015.
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A320-200 WEEKLY CHECK SN
TASK DESCRIPTION
MECH
AME
3. Check fan blades and spinner for FOD and free rotation. 4. Check visually using flash light turbine exhaust 5th stage LPT blades nozzle and exhaust/cone for damage and metal deposit. 5. Check visually using flash light fan exhaust: acoustic lining exit vanes and struts, thrust reverser blocker door. 6. Check fan thrust reverser doors are properly latched (red indicator not protruding). 7. Check Engine intake/ exhaust and Pylon area for sign of damage and leaks. 8. Check Master Magnetic Chip Detector for evidence of metallic debris. 9. Inspection of Starter Magnetic Chip Detector. 10. Replenish Engine starting oil system. 11. Engine fuel & control - Correct faults of the engine Scheduled Maintenance Report (SMR). D.
INTEGRATED DRIVE GENERATOR 1. Check oil level of integrated drive generator (green range) and replenish if necessary. 2. Check filter differential pressure indicator (pop out not protruding).
E.
APU SYSTEM Note: Following tasks are only applicable on AP-BLH (MSN 0542). 1. GVI of APU air inlet plenum & air intake. 2. Check wear indicator of starter motor brush. 3. Test of clutch of APU starter motor.
2.
FUEL TANK:
A.
1. Drain water contents from each fuel tank.
3.
TIRE PRESSURE:
A.
1. Check tire pressure, if incorrect inflate the tire with nitrogen and then record the following values. NLG Wheel 1 _________ PSI Wheel 2 _________ PSI LH MLG : Wheel 1 ________ PSI Wheel 2 _________ PSI RH MLG : Wheel 3 ________ PSI Wheel 4 _________ PSI ISSUE 01 REV 00 Effective from June 01, 2015.
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A320-200 WEEKLY CHECK SN
TASK DESCRIPTION
MECH
AME
2. For MLG brakes, measure Heat Pack Wear Indicators with parking brake on. Brake Assy 1
Brake Assy 2
Brake Assy 3
Brake Assy 4
Fwd Pin
mm
mm
mm
mm
Aft Pin
mm
mm
mm
mm
3. For MLG Door Actuator PN 114122011 or 114122010: Open MLG doors. a. The movement of door actuator must be smooth & continuous. The door should open from fully closed position to the point at which the actuator is vertical in 30 seconds. b. Move the MLG Door with your hand away from the fully open position, through approximately 30 degrees & back to the fully open position, make sure that the resistance to motion is smooth. There must be hydraulic resistance only. c. With the door fully open, measure the dimension ’DIM’ as shown in FIGURE 2. Dimension ’DIM’ must be greater than or equal to 385 mm (15.157 in). If the door actuator fails any of the above three inspection checks, it must be replaced before next flight. 4. For MLG Door Actuator PN 114122014: Perform LH and RH MLG door actuator PN 114122014 greasing as per AMM Task 12-22-32-640-001-A. Note: Ensure greasing of both eye end bearings is accomplished (Refer to FIGURE 3 for grease nipples location). 4.
HYDRAULIC POWER:
A.
1. Check nitrogen charge pressure on Hydraulic Power Accumulators. Adjust the Accumulator Pressure as necessary.
5.
CARGO COMPARTMENT:
A.
1. Carry out visual inspection of following items in cargo compartment. a. Door nets and divider nets. b. Net attachment joints. c. Floor panels for obvious damage and serviceability of rollers. d. Cargo door surround, side walls, ceiling, decompression panels, lining, floor panels and pressure compensation valve. e. Check cargo compartment for obvious damage and cleanliness. f. Check Serviceability of Cargo Compartment lights.
ISSUE 01 REV 00 Effective from June 01, 2015.
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A320-200 WEEKLY CHECK SN
TASK DESCRIPTION
6.
INTERNAL FUSELAGE:
A.
COCKPIT
MECH
AME
1. Check instrument & all panels for cleanliness, condition & security of installation. 2. Check cockpit interior, flooring pedestal; upholstery, cover windows/windshields for cleanliness. 3. Check crew seats, belts & shoulder harness for condition. 4. Check windows & windshields for cracks, delamination & hot spots. Check sliding window for general condition & operation. 5. Check crew oxygen pressure. 6. Perform CVR Test. 7. Operational check of Emergency Generating System. 8. Operational check of Static Inverter. 9. Operational check of Cabin Emergency Lights. 10. Operational Check Of Electrical Flight Control System (EFCS) - The logics activating ELAC 1, ELAC 2 and SEC1 standby power supplies - to confirm ability of SEC.1 and SEC.2 to achieve pitch control - to confirm ability of side stick priority function. 11. Check CFDS (PFR) for slow door opening/closing messages of MLG doors. 12. Print and attach PFR with the Weekly Check. B.
HYDRAULIC & ENGINE OIL QUANTITY & SQUIB TEST 1. Check hydraulic quantity on ECAM. Make an entry in Tech Log if any replenishment is performed. 2. Check engine oil quantity within 5 to 30 min after engine shut down: if indication is below minimum, check engine oil level at tank sight glass top-up oil as required. 3. Perform ENG/APU Fire/Squib Test.
C.
APU OIL LEVEL & HOURS RECORD 1. Perform APU oil level test and record APU hours and cycles via MCDU. Hours: __________________
Cycles : ____________________
2. Check APU cowling for security. D.
AIRCRAFT DOCUMENTATION 1. Check the following onboard documents a. Certificate of Registration b. Certificate of Airworthiness (C of A) c. Insurance ISSUE 01 REV 00 Effective from June 01, 2015.
g. Noise Certificate h. Emergency Equipment Chart i. Technical Log Book Page 4 of 8
A320-200 WEEKLY CHECK SN
TASK DESCRIPTION d. Weight Schedule e. Radio License f. Radio Installation Certificate
E.
MECH
AME
j. AOC k. Certificate of MR l. Certificate of Maintenance Release
PASSENGER CABIN 1. Ensure A/C interior cleanliness. 2. Check PVC floor covering near entry door and galley areas for obvious damage and cleanliness. 3. For passenger door, check emergency cylinder/accumulator pressure. 4. Passenger seats for obvious damage and seat covers for condition and stain. 5. Sidewall- and ceiling panels, bins, partitions and curtains for obvious damages and cleanliness. 6. Ceiling panels for proper installation. 7. Carry out a visual inspection of fwd and aft lavatories extinguisher bottles for evidence of leakage and/or discharge and check temperature indicators for any color change. 8. Check all portable Oxygen units for minimum dispatch pressure. 9. Check for serviceability of cabin reading, external lights. Operational test of cabin emergency lights by “Test Emergency Light Sys” pushbutton & emergency escape path marking. 10. Visual check of the tamper seal/serviceability indication of the protective breathing equipment.(CKPT & CABIN) 11. Cleaning of vacuum waste lines with chemical cleaning agent and crushed ice.
F.
EMERGENCY EQUIPMENT Check all the emergency equipment for condition quantity & validity. Check that all installation/ fixtures / brackets etc required to secure the emergency equipment to their proper location are installed and in serviceable condition. Note: Refer Emergency Equipment Chart in aircraft for location of equipments.
ISSUE 01 REV 00 Effective from June 01, 2015.
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A320-200 WEEKLY CHECK NOTE: THIS TABLE IS TO BE FILLED ON THE FIRST WEEKLY CHECK OF EVERY MONTH i.e. WEEKLY CHECK PERFORMED ON ANY OF THE DATES BETWEEN 01st – 07th OF THE MONTH. SN
1 2 3 4 5 6 7 8 9
DESCRIPTION
PART No
SERIAL No
HST EXPIRY DATE
If New Bottle Installed SN:
New Expiry Date
Crew Oxygen Bottle Cabin Oxygen Bottle Cabin Oxygen Bottle Cabin Oxygen Bottle Cabin Oxygen Bottle Cabin Oxygen Bottle Cabin Oxygen Bottle Cabin Oxygen Bottle Cabin Oxygen Bottle
Note: An item must be replaced if it has an expiry of less than 30 days starting from the date of compliance of this particular task.
Certificate of Release to Service (CRS) I hereby certify that the overhaul / repair(s) / replacement(s) / scheduled maintenance task(s) / modification(s) / mandatory inspection(s) have been carried out in accordance with the instructions of the manufacturer and requirements of the Airworthiness Directorate. It is further certified that work has been performed in accordance with updated manuals, drawing using proper tools, calibrated test equipments, etc. The aircraft is fully airworthy and meets all the safety / Airworthiness standards. I am fully conversant with relevant Rules given in CAR 94, ANO's and Airworthiness Notices. Signature: _____________________ Name: ________________________ AME No. ______________________ Date: _________________________
Note: The person signing CRS is responsible to ensure that each and every task is signed. ISSUE 01 REV 00 Effective from June 01, 2015.
Page 6 of 8
A320-200 WEEKLY CHECK EXTERNAL WALKAROUND DIAGRAM (FIGURE 1)
ISSUE 01 REV 00 Effective from June 01, 2015.
Page 7 of 8
A320-200 WEEKLY CHECK FIGURE 3
ISSUE 01 REV 00 Effective from June 01, 2015.
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