「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 279
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B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
28-21-00-810-828 Fuel - L(R) Wing Tank Pumps 2, Power Supply -
C/B-7QA(8QA) Tripped 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 28-21-00-710-007 Operational Test of the Main Fuel-Pump System with
Fuel Flow by Transfer AMM 28-21-15-000-003 Removal of the Fuel-Pump Pressure-Switch. AMM 28-21-15-400-001 Installation of the Fuel-Pump Pressure-Switch. AMM 28-21-45-000-001 Removal of the Sequence Valve AMM 28-21-45-400-003 Installation of the Sequence Valve 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) 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
SB 24-1070
SIL 57-0086
ASM 28-21/02
TSM 24 PB 101
AWM 28-21-04
3. Fault Confirmation
__________________
A. Table of the circuit breakers referred to in this procedure:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
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:
- OF FIRE OR OF AN EXPLOSION
- OF DAMAGE TO THE AIRCRAFT WIRING AND STRUCTURE.
「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 280
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(1) Examine the C/B-FUEL/R WING TK/PUMP 2 SPLY (8QA).
(2) If the C/B-8QA:
(a) Is open (tripped), do Fuel - L(R) Wing Tank Pumps 2, Power Supply
- C/B-7QA(8QA) Tripped (Ref. TASK 28-21-00-810-828).
(b) Is closed (set), do the Operational Test of the Wing-Tanks Fuel Control (Ref. AMM TASK 28-21-00-710-001).
4. Fault Isolation
_______________
R **ON A/C 001-049, 051-099, 101-105, 151-154, 201-207,
A. Procedure
(1) If a fuel low pressure indication is shown for the right wing tank fuel pump No. 2 (26QA):
- do a fuel transfer (Ref. AMM TASK 28-21-00-710-007) use the right wing tank fuel pump No. 2 to do the fuel transfer.
(2) If the fuel starts to transfer go to step (3). If the fuel does not start to transfer:
(a) Set the R TK PUMPS 2 P/BSW (16QA) to OFF (release out). This will de-energize the contactor 20QA.
(b) Before you do more steps, make sure that the wing area adjacent to the right outer fuel pump 26QA fairings and cover is not contaminated with fuel from a fuel leak or spillage.
1 If necessary:
_ a Repair all the leaks:
_
- (Ref. AMM TASK 51-76-12-300-001)
- (Ref. AMM TASK 51-76-12-300-002)
- (Ref. SIL 57-0086).
b Clean the area of the fuel spillage.
_
(c) Remove all the fuel pump 26QA cable fairings (Ref. AMM TASK 28-21-49-000-001) and cover assembly (Ref. AMM TASK 28-21-51-000-001).
(d) Disconnect the supply cable end connector 26QA-A from the fuel pump receptacle.
(e) If, in step (c) or (d), any damage can be seen on the supply cable or the aircraft structure, go to step (j) 1_.
「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 281
May 01/05 CES
(f) Set the R TK PUMPS 2 P/BSW (16QA) to ON (push in). This will energize the contactor 20QA and the 115VAC three phases will be supplied to the fuel pump connector 26QA-A. 中國航空網(wǎng) 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(102)
