(18) Install the fuel pump, rear and intermediate, fairings (Ref. AMM TASK 28-21-49-400-001). Make sure that the fuel pump supply cable does not get caught under the fairings.
(19) Do a wiring test, as detailed in the step (15), of the aircraft wiring (three phase electrical supply) (Ref. ASM 28-21/01) between the CNTOR-L(R) WING TK PUMP 1 SPLY 17QA(18QA) and the PUMP-FUEL No. 1, L(R) WING TK connector 21QA-A(22QA-A).
(a) If the wiring test:
1 Is serviceable, do step (20).
_
2 Is unserviceable, do steps (15) thru (19) again.
_
(20) Connect the fuel pump supply cable end connector 21QA-A(22QA-A) to the fuel pump receptacle.
(21) Close (reset) the C/B-1QA(2QA).
(22) Do the Operational Test of the Wing-Tanks Fuel Control (Ref. AMM TASK 28-21-00-710-001).
**ON A/C ALL
5. Close-up
________
A. Procedure
(1) Make sure that the fuel pump is installed correctly and the two bolts that attach the pump have been torque tightened (Ref. AMM TASK 28-21-51-400-001).
(2) Install the fuel pump cover plate and the front fairing (Ref. AMM TASK 28-21-49-400-001).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
「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 A293
May 01/04R CES
TASK 28-21-00-810-828
Fuel - L(R) Wing Tank Pumps 2, Power Supply - C/B-7QA(8QA) Tripped
WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
WARNING : DO NOT CLOSE AN OPEN (TRIPPED) CIRCUIT BREAKER RELATED TO A
_______
FUEL-PUMP.
IF YOU CLOSE THE CIRCUIT BREAKER, THERE IS A RISK:
- OF FIRE OR OF AN EXPLOSION
- OF DAMAGE TO THE AIRCRAFT WIRING AND STRUCTURE.
1. Possible Causes
_______________
- PUMP-FUEL NO 2, L WING TK (25QA)
- PUMP-FUEL NO 2, R WING TK (26QA)
- CNTOR-L WING TK PUMP 2 SPLY (19QA)
- CNTOR-R WING TK PUMP 2 SPLY (20QA)
- C/B-FUEL/L WING TK/PUMP 2 SPLY (7QA)
- C/B-FUEL/R WING TK/PUMP 2 SPLY (8QA)
- aircraft wiring
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific multimeter
No specific 500VDC insulation tester
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AD 2002-221(B)
ASRM 57-21-11
AWM 93-01-07
AWM 93-01-20
AWM 93-01-21
ESPM 20-52-21
ESPM 20-52-24
ESPM 20-53-21
AMM 28-21-00-710-001 Operational Test of the Wing-Tank Fuel Control
AMM 28-21-49-000-001 Removal of the Fuel Pump Fairings
AMM 28-21-49-400-001 Installation of the Fuel Pump Fairings
AMM 28-21-51-000-001 Removal of the Fuel Pumps 21QA(26QA) and 25QA(22QA)
「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 A294
May 01/04R CES
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 28-21-51-400-001 Installation of the Fuel Pumps 21QA(26QA) and
25QA(22QA)
AMM 51-76-12-300-001 Local Repair of the Fuel Tank Sealant
AMM 51-76-12-300-002 Repair of the Fuel Tank Fillet
SIL 57-0086
ASM 28-21/02
3. Fault Confirmation
__________________
A. Table of the circuit breakers used in this procedure:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU FUEL/L WING TK/PUMP2 SPLY 7QA N26 121VU FUEL/R WING TK/PUMP2 SPLY 8QA Q26
B. Test
WARNING : DO NOT CLOSE AN OPEN (TRIPPED) CIRCUIT BREAKER RELATED TO A
_______ FUEL-PUMP. IF YOU CLOSE THE CIRCUIT BREAKER, THERE IS A RISK:
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320 Trouble Shooting Manual 排故手册 FUEL 燃油1(152)
