- OF FIRE OR OF AN EXPLOSION
- OF DAMAGE TO THE AIRCRAFT WIRING AND STRUCTURE.
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
_______________
- PUMP-FUEL NO 1, CTR TK (37QA)
- PUMP-FUEL NO 2, CTR TK (38QA)
- CNTOR-CTR TK PUMP 1 SPLY (35QA)
- CNTOR-CTR TK PUMP 2 SPLY (36QA)
- C/B-FUEL/CTR TK/PUMP 1 SPLY (29QA)
- C/B-FUEL/CTR TK/PUMP 2 SPLY (30QA)
- aircraft wiring
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific (intrinsically safe) multimeter
No specific (intrinsically safe) 500VDC insulation tester
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞28-21-00∞∞∞∞∞∞∞∞∞∞Page B206
201-299, 401-499, Aug 01/05 CES
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
ASRM 53-00-00
AWM 93-01-07
AWM 93-01-20
AWM 93-01-21
ESPM 20-31-36
ESPM 20-52-21
ESPM 20-52-24
AMM 28-21-00-720-001 Functional Test of the Center-Tank Fuel Control
AMM 28-21-51-000-002 Removal of the Fuel Pumps 37QA(38QA)
AMM 28-21-51-400-002 Installation of the Fuel Pumps 37QA(38QA)
AMM 32-12-00-010-001 Open the Main Gear Doors for Access
AMM 32-12-00-410-001 Close the Main Gear Doors after Access
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
AWM 28-21-05
AWM 28-21-06
3. Fault Confirmation
__________________
A. Table of the circuit breakers used in this procedure:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU FUEL/CTR TK/PUMP2 SPLY 30QA P26 121VU FUEL/CTR TK/PUMP1 SPLY 29QA P23
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.
(1) Not applicable.
4. Fault Isolation
_______________
A. Procedure
NOTE : This procedure is written for the C/B-FUEL/CTR TK/PUMP 1 SPLY 29QA
____ with the C/B-FUEL/CTR TK/PUMP 2 SPLY 30QA given in parenthesis, if different.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞28-21-00∞∞∞∞∞∞∞∞∞∞Page B207
201-299, 401-499, Aug 01/05 CES
(1) Do all the steps (2) thru (20) before you close the C/B-FUEL/CTR TK/PUMP 1 (2) SPLY 29QA (30QA) in step (21).
(2) Make sure that the CTR TK/PUMP 1 (2) P/BSW 33QA (34QA) shows OFF (released out).
(3) Open the left (right) main landing gear door for access (Ref. AMM TASK 32-12-00-010-001).
(4) Get access to the center tank fuel pump No. 1 (2) 37QA (38QA) (Ref. AMM TASK 28-21-51-000-002).
(5) Before you do more steps make sure that the areas, in the zones 147
(148) and 195 (196), that follow are not contaminated with fuel from a leak or spillage:
- the center tank bottom skin adjacent to the left (right) fuel pump 37QA (38QA)
- the hydraulic compartment below the wing box (center tank) and forward side of the rear bulkhead at FR42
- the rear wall (spar) of the center tank in the left (right) main landing gear bay
- the rear side of the bulkhead at FR 42 below the center tank. 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2(6)
