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时间:2011-03-28 13:49来源:蓝天飞行翻译 作者:航空
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 - troubleshoot the LRU(s) before you start more Steps. Refer to P. Block 101, CFDS for the related Page/Task number.

 (6) Do the:


 - Operational Test of the Main Fuel Pump System with Fuel Flow by Transfer (Ref. AMM TASK 28-21-00-710-007)

 - Functional Test of the Center Tank Fuel Control (Ref. AMM TASK 28-21-00-720-001).

 

 (7) If any Manual Mode fuel pump failures are detected in Step (6):

 - troubleshoot those pump failures before you start more steps. Refer to P. Block 101 for the related Page/Task number.

 (8) If an ECAM warning or FAULT legend failure is found:

 - do the Fuel Pumps - Center Tank Autofeed Warning and/or FAULT Legend Failure (Ref. TASK 28-21-00-810-816).

 (9) If the Fuel Pump Auto Feed system operates as specified:


 - no maintenance steps are necessary.
 4. Fault Isolation
_______________
 A. If the FUEL - AUTO FEED FAULT warning/FAULT legend is given or the system fails to operate as specified:
 (1) Make sure that the slats are fully retracted:

 - retract if necessary (Ref. AMM TASK 27-80-00-866-005).

 (2) Refuel (Ref. AMM TASK 12-11-28-650-003), defuel (Ref. AMM TASK 28-25-00-650-001) or transfer fuel (Ref. AMM TASK 28-25-00-869-001) to obtain these fuel levels:

 - left wing tank 5100 kg (11244 lb)

 - right wing tank 5100 kg (11244 lb)

 - center tank more than 250 kg (550 lb).

 


 「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 A268
 201-299, 401-499, Aug 01/05 CES

 

 (3) Set the Electronic Centralized Aircraft Monitoring (ECAM) system to on (Ref. AMM TASK 31-60-00-860-001), then: - on the ECAM control panel, push (in) the FUEL P/BSW

 - make sure that the FUEL page shows on the ECAM lower Display Unit (DU).

 (4) Push (in) the P/BSW-CTR TK/MODE SEL/AUTO (48QA) (set to auto).

 (5) Push (in) all the fuel pump P/BSWs (set to on).

 (6) Examine the FUEL page on the ECAM lower DU.

 (7) If the following occurs:


 (a) Both the center tank pumps 1 and 2 are shown off.
 1 Remove the SFCC No 1 (21CV) and 2 (22CV) in turn from their
_ racks (Ref. AMM TASK 27-51-34-000-001).
 2 Examine the FUEL page on the ECAM lower DU.
_

 3 If the center tank pumps 1 and 2 operate correctly:
_

 - replace the SFCC-1 (21CV) or SFCC-2 (22CV) (Ref. AMM TASK 27-51-34-000-001) and (Ref. AMM TASK 27-51-34-400-001).
 4 If the fault continues:
_

 a Do a check of (Ref. ASM 28-21/04), and replace if
_
 necessary:

 - the RELAY REFUEL/DEFUEL CTL PNL DOOR (14QU).
 b Do a check of (Ref. ASM 28-21/04), the:
_

 - aircraft wiring ( 16 degrees signal(ground) line) between the SFCC No 1 (21CV) rack connector AA, pin 10H and the RELAY-CTR TK PUMP 1 CTL (51QA), terminal A3

 - aircraft wiring ( 16 degrees signal(ground) line) between the SFCC No 1 (21CV) rack connector AA, pin 10H and the RELAY-CTR TK PUMP 2 CTL (52QA), terminal A3

 - aircraft wiring ( 16 degrees signal(ground) line) between the SFCC No 2 (22CV) rack connector AA, pin 10H and the RELAY-CTR TK PUMP 2 CTL (52QA), terminal A3

 - aircraft wiring ( 16 degrees signal(ground) line) between the SFCC No 2 (22CV) rack connector AA, pin 10H and the RELAY-CTR TK PUMP 1 CTL (51QA), terminal A3.


 5 Repair all the unserviceable wiring and connectors.
_

 6 Do the tests 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 A269
 201-299, 401-499, Aug 01/05 CES (b) The left side center tank pump 1 is shown off.

 

 1 Temporarily remove the FLSCU-1 (7QJ) from its rack (Ref. AMM
_
 TASK 28-46-34-000-001).

 2 Examine the FUEL page on the ECAM lower DU.
_

 3 If the center tank pump 1:
_ a Operates correctly and shows on:

_

 - replace the FLSCU-1 (7QJ) (Ref. AMM TASK 28-46-34-000-001) and (Ref. AMM TASK 28-46-34-400-001).
 b Shows off:
_

 - install the original FLSCU-1 (7QJ) removed from its rack in Step 1_ (Ref. AMM TASK 28-46-34-400-001).
 4 If the fault continues:
_

 a Do a check of (Ref. ASM 28-21/04), and replace if
_
 necessary, the:

 - RELAY-CTR TK AUTO CONTROL, PUMP 1 (41QA)
 
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