DOC AIRBUS | AMM A320F28-42 QUANTITY INDICATING
- PB.001 QUANTITY INDICATING - DESCRIPTION AND OPERATION
- PB.401 QUANTITY INDICATING - DEACTIVATION/REACTIVATION
-
28-42-00-040-002-A
[10]
Check of the Fuel Quantity Indicating Computer Status
-
28-42-00-040-002-A
[10]
- PB.501 FUEL QUANTITY AND TEMPERATURE INDICATING - ADJUSTMENT/TEST
-
28-42-00-710-001-A
[10]
Operational Test of the Fuel Quantity Indicating-System -
28-42-00-740-001-A
[10]
Status Report (BITE) -
28-42-00-740-003-A
[10]
Interrogation of the FQIS Input Parameters Pages -
28-42-00-740-007-A
[10]
Interrogation of the (SMITHS INDUSTRIES) FQIS Troubleshooting Data -
28-42-00-740-009-A
[10]
Interrogation of the (SIMMONDS/GOODRICH) FQIS Trouble Shooting Data -
28-42-00-710-802-A
[10]
Operational Check of Fuel Temperature Indications
-
28-42-00-710-001-A
[10]
- PB.401 PROBE - FUEL QUANTITY - REMOVAL/INSTALLATION
-
28-42-15-000-001-A
[10]
Removal of the Wing Tank Fuel-Quantity-Probes -
28-42-15-000-001-B
[10]
Removal of the Wing-Tank Fuel-Quantity Probes -
28-42-15-400-001-A
[10]
Installation of the Wing Tank Fuel-Quantity-Probes -
28-42-15-400-001-B
[10]
Installation of the Wing-Tank Fuel-Quantity Probes -
28-42-15-000-002-A
[10]
Removal of the Center Tank Fuel-Quantity-Probe -
28-42-15-400-002-A
[10]
Installation of the Center Tank Fuel-Quantity-Probe -
28-42-15-000-005-A
[10]
Removal of the Wing-Tank Fuel-Quantity Probes -
28-42-15-400-005-A
[10]
Installation of the Wing-Tank Fuel-Quantity Probes -
28-42-15-000-004-A
[10]
Removal of the Center (Transfer) Tank Fuel-Quantity Probes -
28-42-15-400-004-A
[10]
Installation of the Center (Transfer) Tank Fuel-Quantity Probe
-
28-42-15-000-001-A
[10]
- PB.401 SENSOR - CADENSICON - REMOVAL/INSTALLATION
-
28-42-16-000-001-A
[10]
Removal of the Cadensicon -
28-42-16-400-001-A
[10]
Installation of the Cadensicon -
28-42-16-000-002-A
[10]
Removal of the Cadensicon -
28-42-16-400-002-A
[10]
Installation of the Cadensicon
-
28-42-16-000-001-A
[10]
- PB.401 PRESELECTOR - FUEL QUANTITY - REMOVAL/INSTALLATION
-
28-42-21-000-001-A
[10]
Removal of the Fuel Quantity Preselector -
28-42-21-400-001-A
[10]
Installation of the Fuel Quantity Preselector -
28-42-21-000-002-A
[9]
Removal of the Fuel Quantity Preselector -
28-42-21-400-002-A
[9]
Installation of the Fuel Quantity Preselector
-
28-42-21-000-001-A
[10]
- PB.401 INDICATOR - FUEL QTY, MULTI TANK - REMOVAL/INSTALLATION
-
28-42-22-000-001-A
[10]
Removal of the Fuel Quantity Indicator -
28-42-22-400-001-A
[10]
Installation of the Fuel Quantity Indicator
-
28-42-22-000-001-A
[10]
- PB.401 PROBE - FUEL QUANTITY, ACT - REMOVAL/INSTALLATION
-
28-42-24-000-001-A
[10]
Removal of the Fuel Quantity Probe of the ACT -
28-42-24-400-001-A
[10]
Installation of the Fuel Quantity Probe of the ACT -
28-42-24-000-003-A
[10]
Removal of the Fuel Quantity Probes of the ACT (AFT Cargo Compartment) -
28-42-24-400-003-A
[10]
Installation of the Fuel Quantity Probes of the ACT (AFT Cargo Compartment)
-
28-42-24-000-001-A
[10]
- PB.401 COMPUTER - FUEL QUANTITY INDICATING (FQIC) - REMOVAL/INSTALLATION
-
28-42-34-000-001-A
[10]
Removal of the Fuel Quantity-Indicating Computer (FQIC) -
28-42-34-400-001-A
[10]
Installation of the Fuel Quantity-Indicating Computer (FQIC) -
28-42-34-000-002-A
[10]
Removal of the Fuel Quantity-Indicating Computer (FQIC) On Board Removable Memory -
28-42-34-400-002-A
[10]
Installation of the Fuel Quantity-Indicating Computer (FQIC) On Board Removable Memory
-
28-42-34-000-001-A
[10]
- PB.401 HARNESS - WING TANK - REMOVAL/INSTALLATION
-
28-42-43-000-006-A
[10]
Removal of the Wing-Tank Inner-Cell Group A Harness -
28-42-43-400-006-A
[10]
Installation of the Wing-Tank Inner-Cell Group A Harness -
28-42-43-000-007-A
[10]
Removal of the Wing-Tank-Inner-Cell Group B Harness -
28-42-43-400-007-A
[10]
Installation of the Wing-Tank-Inner-Cell Group B Harness -
28-42-43-000-003-A
[10]
Removal of the Wing-Tank Outer-Cell Group A Harness -
28-42-43-400-003-A
[10]
Installation of the Wing Tank Outer-Cell Group A Harness -
28-42-43-000-004-A
[10]
Removal of the Wing-Tank Outer-Cell Group B Harness -
28-42-43-400-004-A
[10]
Installation of the Wing-Tank Outer-Cell Group B Harness -
28-42-43-000-005-A
[10]
Removal of the Wing Tank Harness -
28-42-43-400-005-A
[10]
Installation of the Wing Tank Harness -
28-42-43-000-008-A
[10]
Removal of the Wing Tank Fuel Quantity Indicating Probe Fused/Shorting Plug Connectors -
28-42-43-400-008-A
[10]
Installation of the Wing Tank Fuel Quantity Indicating Probe Fused/Shorting Plug Connectors
-
28-42-43-000-006-A
[10]
- PB.401 HARNESS - CENTER TANK - REMOVAL/INSTALLATION
-
28-42-44-000-001-A
[10]
Removal of the Center Tank Harness -
28-42-44-400-001-A
[10]
Installation of the Center Tank Harness -
28-42-44-000-002-A
[10]
Removal of the Center Tank Harness -
28-42-44-400-002-A
[10]
Installation of the Center Tank Harness -
28-42-44-000-003-A
[10]
Removal of the Center Tank Fuel Quantity Indicating Probe Fused Adapters -
28-42-44-400-003-A
[10]
Installation of the Center Tank Fuel Quantity Indicating Probe Fused Adapters
-
28-42-44-000-001-A
[10]
- PB.401 DUALCOMP - LEFT WING TANK - REMOVAL/INSTALLATION
-
28-42-46-000-001-A
[10]
Removal of the Dualcomp -
28-42-46-400-001-A
[10]
Installation of the Dualcomp
-
28-42-46-000-001-A
[10]
- PB.401 ULTRACOMP - CENTER TANK - REMOVAL/INSTALLATION
-
28-42-47-000-001-A
[10]
Removal of the Ultracomp -
28-42-47-400-001-A
[10]
Installation of the Ultracomp
-
28-42-47-000-001-A
[10]
- PB.401 ULTRACOMP - RIGHT WING TANK - REMOVAL/INSTALLATION
-
28-42-48-000-001-A
[10]
Removal of the Ultracomp -
28-42-48-400-001-A
[10]
Installation of the Ultracomp
-
28-42-48-000-001-A
[10]