DOC AIRBUS | FIN A320FFIN: (6QM) STRAINER-PUMP INLET, L WING TK INR
Zone: 540
AMM TASK
- STRAINER - PUMP INLET, WING TANK
-
28-21-54-000-001-A
Removal of the Fuel Pump Strainer -
28-21-54-400-001-A
Installation of the Fuel Pump Strainer -
28-21-54-000-002-A
Removal of the Fuel Pump Strainers -
28-21-54-400-002-A
Installation of the Fuel Pump Strainers
-
28-21-54-000-001-A
IPC FIGURE
SIMILAR FINs
- 26QM - VALVE-WATER DRAIN, R WING TK INR
- 216QM - CLACK VALVE
- 226QM1 - VALVE-WATER DRAIN, ACT1
- 226QM2 - VALVE-WATER DRAIN, ACT2
- 16QM - VALVE-FLOAT VENT, L WING TK INR
- 46QM - PROTECTOR-OVERPRESSURE, L VENT SURGE TK
- 96QM - PROTECTOR-OVERPRESSURE, CTR TK
- 256QM - PROTECTOR-OVERPRESSURE, AFTACT
- 76QM - V BAND CLAMP-TRANSFER ACTR, L FWD SPAR
- 6QM - STRAINER-PUMP INLET, L WING TK INR
- 86QM - VALVE-AIR RELEASE, L WING TK
- 36QM - CHECK VALVE-FUEL PUMP, R WING TK OUTR
- 66QM - JET PUMP-WATER SCAVENGE, L VENT SURGE TK
- 116QM - SHROUD-REFUEL/DEFUEL CPLG, R
- 156QM - CLAMP-V BAND
- 166QM1 - VALVE-FUEL INLET, ACT1
- 166QM2 - VALVE-FUEL INLET, ACT2
- 176QM - CHECK VALVE-ACT TRANSFER
- 236QM - VALVE-ISOLATION, FWD ACT
- 56QM - HOUSING-MLI, L WING TK INR 1
- 106QM - MLI-L WING TK INR 2
- 206QM - MLI-NO 7 LEFT
- 186QM - CLAMP-V BAND