- receptacle 212VC and connector 212VC-A
- receptacle 1973VC and connector 1973VC-A
- terminal block 7517VT and all of its connections
- receptacle 7575VC and connector 7575VC-A
- pressure seal feedthrough 7505VP
- receptacle 7509VC-A, pins H, W, G, M, Z, N and <A
- adjacent and related connecting wires.
「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, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page 232
201-299, 401-499, Aug 01/05 CES
(b) Electrical Tests Do a continuity test (Ref. ESPM 20-52-21) and a test for a short circuit (Ref. ESPM 20-52-22) of the wires that follow (Ref. AWM 28-42-14) and (Ref. AWM 28-42-15):
- FQIC rack connector 3QT-A, pin 7H to connector 7509VC-A, pin H (permittivity signal)
- FQIC rack connector 3QT-A, pin 5H to connector 7509VC-A, pin W (common drive return)
- FQIC rack connector 3QT-A, pin 15G to connector 7509VC-A, pin G (common drive)
- FQIC rack connector 3QT-A, pin 6F to connector 7509VC-A, pin M (density signal)
- FQIC rack connector 3QT-A, pin 7F to connector 7509VC-A, pin Z (density signal return)
- FQIC rack connector 3QT-A, pin 9F to connector 7509VC-A, pin N (density supply/drive)
- FQIC rack connector 3QT-A, pin 10F to connector 7509VC-A, pin <A (density supply/drive return).
(c) Repair all the unserviceable wiring and connectors (Ref. ESPM 20-00-00).
(d) Connect:
- the connector 7509VC-A to the fused adaptor
- the fused adaptor to the tank wall receptacle 7509VC.
(e) Install the initial FQIC 3QT (Ref. AMM TASK 28-42-34-400-001).
(f) Do the test given in Para. 3.B.
(11) If the fault continues, drain and open the tank to the air (Ref. AMM TASK 28-10-00-910-001) and (Ref. AMM TASK 28-10-00-910-002).
(12) Do a check of the HARNESS-CHAN A, CTR TK (17QT) (Ref. AWM 28-42-14) and (Ref. AWM 28-42-15) and replace, if necessary, (Ref. AMM TASK 28-42-44-000-001) and (Ref. AMM TASK 28-42-44-400-001).
(13) If the harness 17QT is serviceable, replace the CADENSICON-CTR TK (20QT) (Ref. AMM TASK 28-42-16-000-002) and (Ref. AMM TASK 28-42-16-400-002).
NOTE : Make sure that the cadensicon transit pin is removed.
____
NOTE : If the center tank cadensicon sensor is replaced, 2000kg
____ (4400lb) of fuel must be put in the center tank before you can fully test the cadensicon.
「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, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page 233
201-299, 401-499, Aug 01/05 CES
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
5. Close-up
________
A. Close-up and Removal of Equipment
(1) Do the EIS Stop Procedure (Ref. AMM TASK 31-60-00-860-002).
(2) If applicable, close the MLG doors (Ref. AMM TASK 32-12-00-410-001).
(3) If necessary, de-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
(4) Make sure that the work area is clean, clear of tool(s) and other items.
(5) 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, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page 234
201-299, 401-499, Aug 01/05 CES
**ON A/C ALL
TASK 28-42-00-810-804
Fuel Quantity Probe 21QT1(2), Left(Right) Wing Tank
WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
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
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 FUEL 燃油2(121)
