AMM 28-11-42-000-002
AMM 28-11-42-400-002
AMM 28-12-00-200-001
AMM 28-12-41-200-002
AMM 28-12-41-200-003
AMM 28-12-47-200-001
AMM 28-21-41-000-001
AMM 28-21-41-400-001
AMM 28-21-43-000-003
AMM 28-21-43-400-003
AMM 28-21-53-000-001
AMM 28-21-53-000-003
AMM 28-21-53-400-001
AMM 28-21-53-400-003
AMM 28-23-00-720-001
AMM 28-25-00-710-002
AMM 28-25-00-710-003
AMM 28-25-00-869-001
AMM 28-25-43-000-001
AMM 28-25-43-400-001
AMM 28-25-51-000-001
AMM 28-25-51-000-002
AMM 28-25-51-400-001
AMM 28-25-51-400-002
AMM 28-46-00-710-001
AMM 28-46-00-740-001
TSM (CFDS) PB 101
TSM (OBS) PB 101
3. Fault Confirmation
__________________
Removal of the Clack Valve 214QM(216QM), 215QM(217QM)
Installation of the Clack Valve 214QM(216QM),
215QM(217QM)
Inspection of the Tank Venting System
Inspection of the Overpressure Protector 96QM
Inspection of the Overpressure Protector 46QM (47QM)
Visual Check of NACA Intake for Signs of Blockage
Removal of the Low Pressure (LP) Air-Release-Valve
86QM(87QM)
Installation of the Low Pressure (LP)
Air-Release-Valve 86QM(87QM)
Removal of the Fuel-Pump Check-Valve 37QM(38QM)
Installation of the Fuel-Pump Check-Valve 37QM(38QM)
Removal of the Jet Pump 66QM(69QM), 67QM(68QM)
Removal of the Jet Adaptor Assembly
Installation of the Jet Pump 66QM(69QM), 67QM(68QM)
Installation of the Jet Adaptor Assembly
Operational Test of Crossfeed Valve Using Individual
Motors: ...
Operational Test of the Defuel System
Operational Test of the Refuel System
Fuel Transfer
Removal of the Defuel/Transfer Valve (11QM)
Installation of the Defuel/Transfer Valve (11QM)
Removal of the Refuel Valve 7QU, (8QU)
Removal of the Refuel Valve 10QU
Installation of the Refuel Valve 7QU, (8QU)
Installation of the Refuel Valve 10QU
Test of the Tank High Level Sensing System
Functional (BITE) Test
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
A. General (synopsis of refuel system description and operation)
There are four different types of refuel procedures, these are as follows:
- Automatic Pressure
- Manual Pressure (with electric power)
- Manual Pressure (without electric power)
- Manual Overwing, (gravity and without electric power).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞28-25-00∞∞∞∞∞∞∞∞∞∞Page 250
Aug 01/05 CES Refueling is usually automatic, the required fuel load is set on the preselector at the refuel panel (800VU).
A fuel gallery connects the refuel coupling to the refuel valve of each tank. The refuel valves are used to control the fuel flow into the tanks in three types of refuel (procedures) and are as follows:
- Automatic Pressure
- Manual Pressure (with electric power)
- Manual Pressure (without electric power).
The fuel flow in the Overwing method is controlled by the delivery system (fuel tanker or pump unit).
During an automatic refuel, when all the refuel valve control switches are set to NORMAL, the Fuel Quantity Indicating Computer (FQIC) controls the refuel valves. Each refuel valve is closed when the actual fuel load for its related tank equals an amount, computed by the FQIC, that is related to the preselected fuel quantity. Fuel is supplied to all tanks at the same time. This is to keep the refuel time to a minimum. The fuel is loaded in the order that follows: Left and right wing tank outer cells, which when full, overflow into the related inner cell through a spill pipe. Center tank (if the preselected fuel load is more than the two wing tank capacities).
During a Manual Pressure Refuel each refuel valve is closed, by one of the ground (refuel) crew, when its refuel valve control switch is set to SHUT.
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) FUEL 燃油2(81)
