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 28-21-00-710-007 Operational Test of the Main Fuel-Pump System with
Fuel Flow by Transfer
AMM 28-21-00-720-001 Functional Test of the Center-Tank Fuel Control
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 28-21-45-400-003 Installation of the Sequence Valve
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 51-76-12-300-001 Local Repair of the Fuel Tank Sealant
AMM 51-76-12-300-002 Repair of the Fuel Tank Fillet
ASM 28-21/03
TSM 24 PB 101
AWM 28-21-06
3. Fault Confirmation
__________________
A. Table of the circuit breakers referred to in this procedure:
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
121VU FUEL/CTR TK/PUMP2 SPLY 30QA P26
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) Examine the C/B-FUEL/CTR TK/PUMP2 SPLY (30QA).
「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 A239
201-299, 401-499, Aug 01/05 CES (2) If the C/B-30QA:
(a) Is open (tripped), do Fuel - Center Tank Pumps 1(2), Power Supply
- C/B-29QA(30QA) Tripped (Ref. TASK 28-21-00-810-829).
(b) Is closed (set), do the Functional Test of the Center-Tank Fuel Control (Manual Mode) (Ref. AMM TASK 28-21-00-720-001).
4. Fault Isolation
_______________
A. Procedure
(1) If a fuel low pressure indication is shown for the center tank fuel pump No. 2 (38QA):
- do a fuel transfer, (Ref. AMM TASK 28-21-00-710-007) use the center 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 CTR TK PUMP 2 P/BSW (34QA) to OFF (release out). This will de-energize the contactor 36QA.
(b) Open the right main landing gear door for access (Ref. AMM TASK 32-12-00-010-001).
(c) Get access to the center tank fuel pump No. 2, 38QA (Ref. AMM TASK 28-21-51-000-002).
(d) Before you do more steps make sure that fuel from a leak or spillage does not contaminate the areas (in zones 148 and 196) that follow:
- the center tank bottom skin adjacent to the right fuel pump 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 right main landing gear bay
- the rear side of the bulkhead at FR 42 below the center tank.
1 If necessary:
_ a Repair all the leaks:
_
- (Ref. AMM TASK 51-76-12-300-001)
- (Ref. AMM TASK 51-76-12-300-002).
b Clean the area of the fuel spillage.
_
c Clean and dry the fuel pump supply cable and the end
_
connector 38QA-A.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞28-21-00∞∞∞∞∞∞∞∞∞∞Page A240
201-299, 401-499, Aug 01/05 CES
(e) Disconnect the supply cable end connector 38QA-A from the fuel pump receptacle.
(f) If, in step (d) or (e), any damage can be seen in this area, go to step (k) 1_.
(g) Set the CTR TK PUMP 1 P/BSW (33QA) to ON (push in). This will energize the contactor 36QA and the 115VAC three phases will be supplied to the fuel pump connector 38QA-A.
(h) Do a test with an (intrinsically safe) multimeter to make sure that each of the 115VAC three phases are available at the connector 38QA-A (Ref. ASM 28-21/03).
(i) Set the CTR TK PUMP 2 P/BSW (34QA) to OFF (release out). This will de-energize the contactor 36QA. 中國航空網 m.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(128)
