(a) Continuity test, with an (intrinsically safe) multimeter, of each three phase wire (from end to end) (Ref. ESPM 20-52-21).
(b) Insulation test, with an (intrinsically safe) 500VDC insulation tester, between each phase wire (pole) and ground (Ref. ESPM 20-52-24).
(c) Insulation test, with an (intrinsically safe) 500VDC insulation tester, between each phase wire and the other two wires (pole to pole) (Ref. ESPM 20-52-24).
(16) Repair/replace the unserviceable wiring and connectors.
(a) If a wire is damaged, the complete section (length) of (each) wire (between the fuel pump connector 37QA-A (38QA-A) and the connector 7612VC-A (7577VC-A) that goes through pressure seal 7611VP (7508VP)) must be replaced (Ref. AWM 28-21-05) ((Ref. AWM 28-21-06)). This is because the wires are located in a fuel and vapour zone (Ref. ESPM 20-31-36).
(17) Install the serviceable cable on the forward and rear sides of the bulkhead at FR42.
(18) Do not connect the fuel pump supply cable end connector 37QA-A (38QA-A) to the pump receptacle.
(19) Do a wiring test, as detailed in the step (15), of the aircraft wiring (three phase electrical supply) between the connector 7612VC-A (7577VC-A) and the PUMP-FUEL No. 1 (2), CTR TK connector 37QA-A (38QA-A) (Ref. AWM 28-21-05) ((Ref. AWM 28-21-06)).
(a) If the test shows that the wiring:
1 Is serviceable, do step (20).
_
2 Is unserviceable, do steps (2) thru (19) again.
_
(20) Connect the fuel pump supply cable end connector 37QA-A (38QA-A) to the fuel pump receptacle.
(21) Close (reset) the C/B-29QA (30QA).
(22) Do the Functional Test of the Center-Tank Fuel Control (Manual Mode) (Ref. AMM TASK 28-21-00-720-001).
「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 B211
201-299, 401-499, Aug 01/05 CES
5. Close-up
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A. Procedure
(1) Make sure that the fuel pump is installed correctly and the bolts that attach the pump have been torque tightened (Ref. AMM TASK 28-21-51-400-002).
(2) Close the left (right) main landing gear door (Ref. AMM TASK 32-12-00-410-001).
(3) Close the access panel 195AB (196AB).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞28-21-00∞∞∞∞∞∞∞∞∞∞Page B212
201-299, 401-499, Aug 01/05 CES
R **ON A/C ALL
TASK 28-21-00-810-830
Fuel - L(R) Wing Tank Pumps 1, Power Supply (Smoke) - C/B-11QA(12QA) Tripped
WARNING : OBEY THE FUEL SAFETY PROCEDURES.
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1. Possible Causes
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- L WING TK/PUMP 1/STBY SPLY (11QA)
- R WING TK/PUMP 1/STBY SPLY (12QA)
- CT-AC, 1 (42XU3)
- CNTOR-L WING TK STBY SPLY, PUMP 1 (53QA)
- CNTOR-R WING TK STBY SPLY, PUMP 1 (54QA)
- aircraft wiring (three phase electrical standby supply)
2. Job Set-up Information
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A. Fixtures, Tools, Test and Support Equipment
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REFERENCE QTY DESIGNATION
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No specific multimeter
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 FUEL 燃油2(8)
