_ AMM TASK 28-21-45-400-003).
NOTE : Sequence valves are not fitted to the center tank pumps
____ but the fuel pump pressure can be tested using the same procedure. The fuel output pressure of the center tank fuel pumps is more than that of the wing tank fuel pumps.
2 Do Para. 4.D. (Preparation for Test) thru Para. 4.G. (Test of
_ the Sequence Valve) on the center tank fuel pump, No. 1(2).
3 Make sure that the fuel pressure for the center tank pumps is
_ more than approximately 2.76 bar (40.0 psi).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞28-21-00∞∞∞∞∞∞∞∞∞∞Page A272
201-299, 401-499, Aug 01/05 CES
NOTE : The fuel pressure given here for this test is without a____
fuel transfer.
4_ If the fuel pressure is less than that specified:
- replace the PUMP-FUEL NO 1, CTR TK (37QA) (PUMP-FUEL NO 2,
CTR TK (38QA)) (Ref. AMM TASK 28-21-51-000-002) and (Ref.
AMM TASK 28-21-51-400-002).
5_ If the fault continues, investigate the reason for the low
pressure and make sure that:
- the fuel pick up strainer and pump input pipe is clear
- the fuel pump/canister outlet pipe work is not damaged and
leaking.
6_ Replace all the unserviceable fuel pipes and strainers.
(9) Do the test given in Para. 3.A.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞28-21-00∞∞∞∞∞∞∞∞∞∞Page A273
201-299, 401-499, Aug 01/05 CES
R **ON A/C ALL
TASK 28-21-00-810-824 Fuel Pumps - Right Wing Tank Pumps 1 And 2 System Failure WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
1. Possible Causes
_______________
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 28-21-00-710-001 Operational Test of the Wing-Tank Fuel Control
3. Fault Confirmation
__________________
A. Do the Operational Test of the Wing-Tanks Fuel Control (Ref. AMM TASK 28-21-00-710-001).
4. Fault Isolation
_______________
A. If a fuel low pressure indication is given for both the Right Wing Fuel Pumps.
(1) Identify the fault symptoms for each of the pumps.
(2) Refer to the List of Faults in P. Block 101 for the applicable task reference.
「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 ∞∞28-21-00∞∞∞∞∞∞∞∞∞∞Page A274
May 01/04 CES
TASK 28-21-00-810-825
Internal Fuel Leak Which Causes a Fuel Imbalance or a Discharge From a NACA Vent During Taxi or Flight
WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
1. Possible Causes
_______________
- VALVE-AIR RELEASE, L WING TK (86QM)
- VALVE-AIR RELEASE, R WING TK (87QM)
- L(R) FULL SENSOR 23QJ1(2)
- L(R) UNFULL SENSOR 24QJ1(2)
- L(R) UNFULL SENSOR 25QJ1(2)
- L(R) UNFULL SENSOR 26QJ1(2)
- L(R) FULL SENSOR 27QJ1(2)
- L(R) SURGE SENSOR 28QJ1(2)
- FLSCU1(2) 7(9)QJ
- L (R) engine LP fuel supply line VALVE ASSY-SUCTION, FUEL PUMP
- OUTLET (CHECK) VALVE, Part of CANISTER-FUEL PUMP, L(R) WING TK OUTER 1QM(4QM)
- OUTLET (CHECK) VALVE, Part of CANISTER-FUEL PUMP, L(R) WING TK INNER 2QM(3QM)
- engine LP fuel feed pipes and connections between the wing front spar tank wall and the wing Rib 1 tank wall
2. Job Set-up Information
______________________
A. Referenced Information
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 FUEL 燃油1(143)
