「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 201
May 01/04 CES
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
28-21-00-810-827 Fuel - L(R) Wing Tank Pumps 1, Power Supply (Normal)
- C/B-1QA(2QA) Tripped
R 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 28-21/01
TSM 24 PB 101
AWM 28-21-01
3. Fault Confirmation
__________________
A. Table of the circuit breakers referred to in this procedure:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU FUEL/L WING TK/PUMP1 SPLY 1QA N23
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 202
Nov 01/02 CES
(1) Examine the C/B-FUEL/L WING TK/PUMP 1 SPLY (1QA).
(2) If the C/B-1QA:
(a) Is open (tripped), do Fuel - L(R) Wing Tank Pumps 1, Power Supply (Normal) - C/B-1QA(2QA) Tripped (Ref. TASK 28-21-00-810-827).
(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 left wing tank fuel pump No. 1 (21QA):
- do a fuel transfer (Ref. AMM TASK 28-21-00-710-007) use the left wing tank fuel pump No. 1 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 L TK PUMPS 1 P/BSW (13QA) to OFF (release out). This will de-energize the contactor 17QA.
(b) Before you do more steps, make sure that the wing area adjacent to the left outer fuel pump 21QA 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 21QA cable fairings (Ref. AMM TASK 28-21-49-000-001) and cover assembly (Ref. AMM TASK 28-21-51-000-001). 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(65)
