- the CNTOR-R WING TK STBY SPLY, PUMP 1 (54QA)

 - the P/BSW-FUEL/R TK PUMPS/1 (14QA)

 - the RELAY-BUS 1/ESS. R TK PUMP 1 (64QA)

 - the P/BSW-EMER ELEC PWR/SMOKE DRILL (13XU).

 NOTE : The P/BSW-EMER ELEC PWR/SMOKE DRILL (13XU) is only
____ included to complete the list of possible causes. It can only be swapped with a serviceable spare.
 1 Do the test given in Para. 3.A.
_

 2 If the fault is removed /cleared:
_ a Replace all the unserviceable items.

_

 b Do the test given in Para. 3.A. for the left and right
_
 wing-tank fuel-pumps 1.

 (2) If the fault continues:
 (a) Do a check (Ref. ASM 28-21/01) of the aircraft wiring between:

 - the C/B-FUEL/PUMPS/1/R CTL AND L IND (4QA), terminal 2 and the RELAY-BUS 1/ESS. R TK PUMP 1 (64QA), terminal A2

 - the C/B-FUEL/PUMPS/1/R CTL AND L IND (4QA), terminal 2 and the RELAY-BUS 1/ESS. R TK PUMP 1 (64QA), terminal C1

 - the RELAY-BUS 1/ESS. R TK PUMP 1 (64QA), terminal A1 and the P/BSW-FUEL/R TK PUMPS/1 (14QA), terminal B3

 - the RELAY-BUS 1/ESS. R TK PUMP 1 (64QA), terminal X2 and the P/BSW-EMER ELEC PWR/SMOKE DRILL (13XU), terminal D1 the P/BSW-EMER ELEC PWR/SMOKE DRILL (13XU), terminal D3 and the aircraft ground at 2409VG

 - the C/B-FUEL/SMOKE/CONFIG/PUMP CTL (55QA), terminal 2 and the RELAY-BUS 1/ESS. R TK PUMP 1 (64QA), terminal X1

 - the P/BSW-FUEL/R TK PUMPS/1 (14QA), terminal B1 and the CNTOR-R WING TK PUMP 1 SPLY (18QA), terminal X

 - the CNTOR-R WING TK PUMP 1 SPLY (18QA), terminal Z and the CNTOR-R WING TK STBY SPLY PUMP 1 (54QA), terminal 4

 - the CNTOR-R WING TK STBY SPLY PUMP 1 (54QA), terminal 3 and the aircraft ground DC1 at 1176VT.

 (b) Repair all the unserviceable wiring and connectors (Ref. ESPM 20-00-00).

 (c) Do the test given in Para. 3.A.

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞28-21-00∞∞∞∞∞∞∞∞∞∞Page A214
 May 01/04R
 CES

 TASK 28-21-00-810-809

 Fuel Pumps - Left Wing Tank Fuel Pump No. 1 Contactor Control Failure (Standby Supply)
 WARNING : OBEY THE FUEL SAFETY PROCEDURES._______ 
R R R R R  WARNING : WHEN YOU DO WORK ON THE FUEL SYSTEM WIRING, YOU MUST USE TEST_______ EQUIPMENT THAT IS APPROVED (REFER TO INTERNATIONAL OR NATIONAL SPECIFICATIONS FOR INTRINSICALLY SAFE TEST EQUIPMENT, E.G. EN50-020, UL913 OR EQUIVALENT). TEST EQUIPMENT THAT IS NOT APPROVED CAN CAUSE FIRE OR AN EXPLOSION.
 1. Possible Causes_______________
 - CNTOR-L WING TK STBY SPLY, PUMP 1 (53QA) - CNTOR-L WING TK PUMP 1 SPLY (17QA) - P/BSW-FUEL/L TK PUMPS/1 (13QA) - RELAY-BUS 1/ESS. L TK PUMP 1 (63QA) - P/BSW-EMER ELEC PWR/SMOKE DRILL (13XU) - aircraft wiring
 2. Job Set-up Information______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific  multimeter
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------

28-21-00-810-801 28-21-00-810-807 ESPM 20-00-00
 AMM 24-22-00-710-001 ASM 28-21/01
Fuel Pumps - Left Wing Tank Fuel Pump No. 1 (Outer)
 21QA System Malfunction
Fuel Pumps - Left Wing Tank Fuel Pump No. 1 Contactor
 Control Failure (Normal Supply)

Operational Test of the Generator Line Contactor
 (GLC-1) Opening in the Smoke Procedure

 「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 A215
 May 01/04 CES

 3. Fault Confirmation__________________
 A. Test
 (1) Do the Operational Test of the Generator Line Contactor (GLC-1) Opening in the Smoke Procedure (Ref. AMM TASK 24-22-00-710-001).
 NOTE : During the job set-up of the operational test, the left and
____ right wing-tank fuel-pumps 1 are supplied by AC BUS 1 and DC BUS 1 (the normal operational supplies from engine 1).
 During the procedure of the operational test, when the generator line contactor (GLC-1) is open (GEN 1 LINE P/BSW released out), the left and right wing-tank fuel-pumps 1 are supplied from the electrical ground power unit through the transfer circuit.
　
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 FUEL 燃油1(118)