28-21-00-810-802
28-21-00-810-808
AMM 24-22-00-710-001
AMM 24-22-17-000-001
AMM 24-22-17-400-001
ASM 24-22/02
ASM 28-21/01
Fuel Pumps - Right Wing Tank Fuel Pump No. 1 (Inner)
22QA System Malfunction
Fuel Pumps - Right 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
Removal of the AC Current Transformers (41XU1, 41XU2,
42XU1, 42XU2, 42XU3 and 42XU4)
Installation of the AC Current Transformers (41XU1,
41XU2, 42XU1, 42XU2, 42XU3 and 42XU4)
「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 A207
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).
(2) If a low fuel pressure indiction is shown when the right wing tank fuel pump No. 1 is supplied from:
(a) The normal supply (AC BUS 1 and through the contactor-18QA), do (Ref. TASK 28-21-00-810-802) and (Ref. TASK 28-21-00-810-808).
(b) The standby supply (direct from the Generator No. 1 and through the contactor-54QA), do Para. 4.A.
4. Fault Isolation
_______________
A. Procedure
(1) Do a check of (Ref. ASM 28-21/01) and replace, if necessary:
- the C/B-R WING TK/PUMP 1/STBY SPLY (12QA)
- the CT-AC, 1 (42XU3) (Ref. AMM TASK 24-22-17-000-001) and (Ref. AMM TASK 24-22-17-400-001).
- the CNTOR-R WING TK STBY SPLY, PUMP 1 (54QA).
(2) Do a check, with a multimeter, of the aircraft wiring (three phase electrical standby supply) (Ref. ASM 24-22/02) and (Ref. ASM 28-21/01) between:
- the contactor GLC-1 (9XU1) (Gen 1 connected terminals D, E and F) and the C/B-R WING TK/PUMP 1/STBY SPLY (12QA)
NOTE : Each phase of the wiring between these two units goes through
____ a different toroidal transformer of the CT-AC, 1 (42XU3). There is no direct electrical connection.
- the C/B-R WING TK/PUMP 1/STBY SPLY (12QA) and the CNTOR-R WING TK STBY SPLY, PUMP 1 (54QA)
- CNTOR-R WING TK STBY SPLY, PUMP 1 (54QA) and the PUMP-FUEL No. 1, R WING TK free connector 22QA-A.
(3) Repair the unserviceable wiring and connectors.
(4) 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 A208
May 01/04R
CES TASK 28-21-00-810-807
Fuel Pumps - Left Wing Tank Fuel Pump No. 1 Contactor Control Failure (Normal Supply)
WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
R WARNING : WHEN YOU DO WORK ON THE FUEL SYSTEM WIRING, YOU MUST USE TEST
_______ R EQUIPMENT THAT IS APPROVED (REFER TO INTERNATIONAL OR NATIONAL R SPECIFICATIONS FOR INTRINSICALLY SAFE TEST EQUIPMENT, E.G. EN50-020, R UL913 OR EQUIVALENT). TEST EQUIPMENT THAT IS NOT APPROVED CAN CAUSE R FIRE OR AN EXPLOSION.
1. Possible Causes
_______________
- CNTOR-L WING TK PUMP 1 SPLY (17QA)
- CNTOR-L WING TK STBY SPLY, PUMP 1 (53QA)
- 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) 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 FUEL 燃油1(115)
