AIRCRAFT REGN: DATE : STN : FLT No : Page No 1 of 9 1 PRELIMINARY ITEMS 1A WARNING: Make sure that the ground safety-locks are correctly installed on the landing gear. This prevents unwanted movement of the landing gear (Install the nose landing gear, body landing gear and wing landing gear ground lock safety pins as per AMM 32-00-00-481-801). 1B WARNING: Make sure that the safety devices and the warning notices are in position before you start a task on or near: - The flight controls - The flight control surfaces - The landing gear and related doors - Components that move 1C Install wheel chocks. NOTE: If the aircraft is parked and high wind conditions exist of are forecasted, park aircraft i.a.w. AMM. 1D If the aircraft electrical network is not energized, perform a safety check to ensure proper position of controls and switches before energizing the electrical network. Energize the aircraft electrical network. 2 FLIGHT COMPARTMENT AMP 335100-00001-01 2A Perform BITE test of the Emergency Lighting System through the OMS Ref: AMM 33-51-00-740-801 NOTE: During this procedure, if an error message is shown, record this message. Then do the related trouble shooting procedure During the test, obey the instructions shown on the terminal. 2B Ensure at least Qty 10 Inoperative Equipment placards are in the rear pouch of the Technical Log Book. Replenish if less than Qty 10 or raise an ADD. Small Placard (QA/F/0288) P/N XXM000049, Medium Placard (QA/F/0202) P/N XXM000131, Large Placard (QA/F/0201) P/N XXM000132. Check PFR for class 4 messages. rectify or raise add to rectify within time limit stipulated in the PFR 2C NOTE: Refer to Airbus SIL 00-091 for list of spurious messages. (Ref: Email from MCC on 24 Sep 09)
AIRCRAFT REGN: DATE : STN : FLT No : Page No 2 of 9 EXTERNAL WALK AROUND 3 LANDING GEARS AND DOORS (GENERAL) AMP 324200-00002-01 Carry out general visual inspection of brake units for condition and wear (with braking pressure applied) i.a.w AMM 32-42-00-210-802. Replace brake If wear pin indicator is at 01mm and less or if the end of wear indicator pin is level with, or below the face of a guide. Record remaining usable pin length. L/H WLG No.1:... mm No.2:... mm R/H WLG No.3:... mm No.4:...mm 3A No.5:... mm No.6:... mm No.7:... mm No.8:...mm L/H BLG R/H BLG No.9:... mm No.10:... mm No.11... mm No.12... mm No.13:... mm No.14:...mm No.15... mm No.16...mm ( Ref TN 32-019) 4 NOSE LANDING GEAR AND DOORS 4A AMP 200711-00001-01 Do a general visual inspection of the L/HIRF wiring protection installed on the nose landing gear. Make sure that there are no signs of corrosion or damage. Make sure that there are no loose screws or connectors, clamps, fasteners or bonding leads. (Ref: AMM 24-92-71-210-801-A). 4B AMP ZL-711-00001-01 (Zone 711) Do a general visual inspection of the NLG. Do a visual check of the structure, the equipment and the systems. Make sure that there is no damage, corrosion, leaks, cracks or chafing and that the lines are correctly attached. (Ref: AMM 05-27-10-210-801).
AIRCRAFT REGN: DATE : STN : FLT No : Page No 3 of 9 5 WING LANDING GEAR (WLG) WARNING: Make sure that all safety precautions in the cockpit and inspection areas are in place. Make sure that inspection areas are sufficiently clean. Refer to AMM for cleaning procedures. 5A AMP ZL-731-00001-01 (Zone 731) Do a general visual inspection of the wing landing gear and make sure there are no signs of corrosion, damage to the protective finish, distortion, cracks, excessive wear, chafing, scores, dents and burrs. (Ref: AMM 05-27-30-210-801). 5B AMP 200731-00001-01 (Zone 730) Do a detailed inspection of the Brake Temperature Compensation Module (BTCM) L/HIRF Wiring Protection installed. Make sure there are no signs of corrosion or damage. Make sure that there are no signs of loose screws or connectors, clamps, fasteners or bonding leads. (Ref: AMM 24-92-73-220-801-A). 5C AMP ZL-731-00001-01 (Zone 741) Do a general visual inspection of the wing landing gear and make sure there are no signs of corrosion, damage to the protective finish, distortion, cracks, excessive wear, chafing, scores, dents and burrs. (Ref: AMM 05-27-30-210-801). 5D AMP 200731-00001-01 (Zone 740) Do a detailed inspection of the Brake Temperature Compensation Module (BTCM) L/HIRF Wiring Protection installed. Make sure there are no signs of corrosion or damage. Make sure that there are no signs of loose screws or connectors, clamps, fasteners or bonding leads. (Ref: AMM 24-92-73-220-801-A). 6 ENGINE WARNING: Make sure that job set-up configuration and safety precautions are in place. Make sure that inspection areas are sufficiently clean. Refer to AMM for cleaning procedures. 6A AMP 242000-00003-01 Drain and replenish VFG 4 Oil system as per AMM 24-21-00-610-801-A 6B AMP 242000-00007-01 Replace VFG 4 Oil Filter as per AMM 24-21-00-610-802-A Discard old filter.
AIRCRAFT REGN: DATE : STN : FLT No : Page No 4 of 9 AMP 242100-00001-01-E NOTE: Only VFG 1 and VFG 4 needs to be serviced in this service check 6C Carryout VFG 1 Oil Top up to the maximum level as per AMM Task 24-21-00-612-801. Record in the aircraft technical logbook the qty of oil uplifted to reach the maximum level: Carryout VFG 4 Oil Top up to the maximum level as per AMM Task 24-21-00-612-801. Record in the aircraft technical logbook the qty of oil uplifted to reach the maximum level: 7 BODY LANDING GEAR (BLG) AND DOORS WARNING: Make sure that all safety precautions in the cockpit and inspection areas are in place. Make sure that inspection areas are sufficiently clean. Refer to AMM for cleaning procedures. 7A AMP ZL-751-00001-01 (Zone 751) Do a general visual inspection of the body landing gear and make sure there are no signs of corrosion, damage to the protective finish, distortion, cracks, excessive wear, chafing, scores, dents and burrs. (Ref: AMM 05-27-50-210-801). 7B AMP 200751-00001-01 (Zone 750) Do a detailed inspection of the Brake Temperature Compensation Module (BTCM) L/HIRF Wiring Protection installed. Make sure there are no signs of corrosion or damage. Make sure that there are no signs of loose screws or connectors, clamps, fasteners or bonding leads. (Ref: AMM 05-27-50-220-801). 7C AMP ZL-751-00001-01 (Zone 761) Do a general visual inspection of the body landing gear and make sure there are no signs of corrosion, damage to the protective finish, distortion, cracks, excessive wear, chafing, scores, dents and burrs. (Ref: AMM 05-27-50-210-801). 7D AMP 200751-00001-01 (Zone 760) Do a detailed inspection of the Brake Temperature Compensation Module (BTCM) L/HIRF Wiring Protection installed. Make sure there are no signs of corrosion or damage. Make sure that there are no signs of loose screws or connectors, clamps, fasteners or bonding leads. (Ref: AMM 05-27-50-220-801).
AIRCRAFT REGN: DATE : STN : FLT No : Page No 5 of 9 8 FWD CARGO COMPARTMENT 8A 8B 8C AMP ZL-131-00001-01 (Zone 130) Do a general visual inspection of the lower deck forward cargo compartment which includes the cargo door profile on the fuselage side. Use a FLASHLIGHT. (Ref: AMM 05-21-30-210-801) AMP 501300-00001-01 (Zone 130) Examine the ceiling panels, the partition wall panels and the sidewall panels for cracks and other damages. Make sure the panels are correctly attached. Missing fasteners are not permitted. Ref: 50-13-00-210-801. Make sure that the self-adhesive tapes, installed at the joints of the panels are in the correct condition. If necessary, replace the damaged self-adhesive tape. Make sure the seal of each panel is in the correct condition. Examine floor panels for cracks or other damages. Make sure that the seal of each floor panel is in the correct condition. Examine the access doors installed in the partition wall and make sure that the door locking mechanism(s) operate correctly. AMP 256800-00005-01 (Zone 130) Do a visual check of the cargo lining decompression panels. (Ref: AMM 25-68-00-210-805) 9 AFT CARGO COMPARTMENT AMP ZL-151-00001-01 (Zone 150) Do a general visual inspection of the lower deck aft cargo compartment. Use a 9A FLASHLIGHT. (Ref: AMM 05-21-50-210-801) 9B 9C AMP 501400-00001-01 (Zone 150) Examine the ceiling panels, the partition wall panels and the sidewall panels for cracks and other damages. Make sure the panels are correctly attached. Missing fasteners are not permitted. Ref: 50-13-00-210-801. Make sure that the self-adhesive tapes, installed at the joints of the panels are in the correct condition. If necessary, replace the damaged self-adhesive tape. Make sure the seal of each panel is in the correct condition. Examine floor panels for cracks or other damages. Make sure that the seal of each floor panel is in the correct condition. Examine the access doors installed in the partition wall and make sure that the door locking mechanism(s) operate correctly. AMP 256800-00005-01 (Zone 150) Do a visual check of the cargo lining decompression panels. (Ref: AMM 25-68-00-210-805) 10 BULK CARGO COMPARTMENT AMP ZL-161-00001-01 (Zone 160) Do a general visual inspection of the lower deck bulk cargo compartment. Use a 10A flashlight. (Ref: AMM 05-21-60-210-801)
AIRCRAFT REGN: DATE : STN : FLT No : Page No 6 of 9 10B 10C AMP 501500-00001-01 (Zone 160) Examine the ceiling panels, the partition wall panels and the sidewall panels for cracks and other damages. Make sure the panels are correctly attached. Missing fasteners are not permitted. Ref: 50-15-00-210-801. Make sure that the self-adhesive tapes, installed at the joints of the panels are in the correct condition. If necessary, replace the damaged self-adhesive tape. Make sure the seal of each panel is in the correct condition. Examine floor panels for cracks or other damages. Make sure that the seal of each floor panel is in the correct condition. Examine the access doors installed in the partition wall and make sure that the door locking mechanism(s) operate correctly. AMP 256800-00005-01 (Zone 160) Do a visual check of the cargo lining decompression panels. (Ref: AMM 25-68-00-210-805) SYSTEMS 11 ATA 21 - AIR CONDITIONING AMP 212100-00005-01 Discard galley extraction filter elements iaw AMM 25-30-00-920-801. 11A Install new galley extraction filter elements. 12 ATA 25 - EQUIPMENT/FURNISHINGS 12A Check Emergency Equipment for condition and where applicable, ensure sufficient life remaining to the next Service Check, except for Life Vest*. Ref A380 Safety Equipment Check List QA/F/0640. *Note: For life vest only presence and condition needs to be confirmed, life for life vest will be checked every A-check. 12B Check emergency equipment location placards for presence and condition where applicable. Provide/ Replace emergency equipment location placards if required. 12C Carry out the following on Telemedicine Unit Tempus IC (located in Main Deck Galley GSM ft of door M5L): 1) Check the capacity/condition of the battery installed in the unit. 2) Check the capacity/condition of the spare Tempus Battery (P/N 01-1001) placed with the unit. 3) Check the availability of the RJ 45 White Cable (P/N 01-1021) stored with the Tempus IC unit. Note: Battery capacity check can be carried out by pressing the both batteries or on the unit for main battery. button on If there is no green light illuminating on the main unit or main battery then replace the unit. If there is no green light illuminating on the spare battery replace the spare battery. (Technical Notice 44-006).
AIRCRAFT REGN: DATE : STN : FLT No : Page No 7 of 9 13 ATA 28 - FUEL AMP 281100-00005-01 Perform operation of trim tank water drain valves to remove accumulated water. Ref: AMM 28-11-00-281-804. 13A Note: - Ensure Aircraft was parked for more than one hour and none of the fuel systems components were operational for more than one hour before carrying out the task. - If possible, carry out the water drain procedure before refuelling. If refuelling was carried out on the aircraft before carrying out the task, wait for 1 hour for the separation of fuel and water to ensure ideal water drainage is achieved. - Ensure fuel temperature is above 5 deg. - There must be more than 10% content of fuel in each tank in order to ensure effective water drainage is completed. If less than 10% content of fuel is found, then the indirect water drain valves will have a decreased flow - After drainage, ensure drain valves are properly seated and not leaking. - Make a technical log entry that water drainage has been performed and record amount of water found in each tank. 14 ATA 32 LANDING GEAR AMP 320000-00001-01-E (MPD Task 325400-00002-01) 14A Lubricate all the following Body Wheel Steering Mechanism as per AMM 320000-600-803 of Fig. : 32-00-00-991-03500-A sheet 5/6 and 6/6. 1. Item 93 - Steering Unlock Mechanism 2. Item 94 - Bogie Beam Locking Wedge 3. Item 95 - Locking Wedge 4. Item 96 - Aft Axle 5. Item 97 - Lock Spring (LH) 6. Item 98 - Steering Actuator 7. Item 99 - Aft Axle 8. Item 100 - Steering Unlock Actuator 9. Item 101 - Lock Spring (RH) 10. Item 104 - Steering Actuator 11. Item 105 - Steering Actuator Note 1: Item 96 & 99 (AFT AXLE) also require lubricating with raising the BLG aft axle until the wheels are off the ground (Ref. AMM TASK 07-12-00-582-803). Note 2: Ensure that good quantity of new grease comes out from all related joints. Note 3: After Lowering the BLG aft axle and removing the jacks, clean and remove the unwanted grease. (Zone 750) Left BLG (Zone 760) Right BLG
AIRCRAFT REGN: DATE : STN : FLT No : Page No 8 of 9 15 ATA 34 - NAVIGATION AMP 341000-00101-01 15A Note: Only one MFP need to be cleaned at a time every 3 rd service check. Clean Multifunction Probe # 3 as per AMM 34-10-00-100-803 16 ATA 35 - OXYGEN AMP 353000-00001-01 Perform visual check of portable oxygen equipment. (Ref: AMM 35-30-00-210-801) NOTE: 16A For Aircraft fitted with new Protective Breathing Equipment P/N: MR10022N only, carry out the following tasks (Ref. TN 35-007). Do a Check to ensure that the 'Replace By' date has not been exceeded. Do a Check to ensure that the tamper-evident seals have not been damaged/torn and that metal latch is engaged to its locked position Do a Check to ensure that the humidity indicator (round dot seen through viewing window of the PBE assembly) is blue in color. If it has turned pink, replace the PBE assembly 17 ATA 38 - WASTE/WATER SERVICING AMP 383000-00001-01 Clean Vacuum Waste lines with chemical cleaning agent and crushed ice. 17A (Ref: AMM 38-31-00-100-801). 17B 17C AMP 383000-00003-01 Clean Filter Element of washbasin drain assembly. (Ref: AMM 38-32-00-100-801). AMP 380000-00005-01 Discard water filter of drinking fountain as per AMM 381600-920-801. Install new water filter. 18 ATA 44 CABIN SYSTEMS AMP 442000-00001-01 (Applicable to airplane with Crew Rest Compartment only) 18A Discard IFE CWS / RCC air filter IAW AMM 442100-920-814. Install new IFE CWS / RCC air filter. 19 ATA 45 ON BOARD MAINTENANCE SYSTEM AMP 452000-00101-01 19A Up And Down Data Loading System - Check Of Discrepancies Between Repository Content and Aircraft Configuration as per AMM 452000-860-809.
AIRCRAFT REGN: DATE : STN : FLT No : Page No 9 of 9 20 ATA 46 INFORMATION SYSTEM AMP 463000-00101-01 20A Carryout System Test of NSS (flight operation domain) as per AMM 463000-730-801-A 20B Carry out Functional End-to-End Test for Internet IAW: TASK 46-41-00-720- 846-A 20C Click on the data loading page and ensure that all the correct Software PNs are installed and the State is Identical (Green). Note: Refer to Technical Notice 46-021 and IPC 46-41-37. 21 ATA 49 AUXILIARY POWER UNIT AMP 499100-0000-01-E 21A Carryout APU oil level check and replenishment as required i.a.w. AMM 49-91- 00-612-802-A 22 FINAL ITEMS 22A Put the aircraft back to its initial configuration. 22B 22C 22D 22E 22F Make sure that the work area is clean and clear of tools and other items. De-energize the ground service network. Ensure all cabin doors, cargo compartment doors and service panels are properly closed and secured. Ensure no damage has been caused by ground equipment or during baggage loading. Ensure towing lever is in normal (spring loaded) position after tow bar removal. On completion of SERVICE CHECK, ensure Line Maintenance CRS (Form QA/F/0122) is duly completed and certified by authorized person [issued as a single copy and not required to be placed on board the aircraft].