A. Procedure
(1) Do the steps applicable to the test equipment available.
(2) Test Equipment 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.
(a) If there is: R
- approved test equipment available, go to Step (3) R
- no approved test equipment available, go to Step (6).
R (3) Get access to the tank wall connector 7509VC (for the center tank
R harness 17QT) in the right MLG bay (Ref. AMM TASK 32-12-00-010-001).
(4) Disconnect the free connector 7509VC-A from the receptacle 7509VC.
「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, 051-061, 101-105, 201-203, ∞∞28-46-00∞∞∞∞∞∞∞∞∞∞Page 238
301-399, May 01/05 CES
R RR (5) Do a resistance check of the sensor 20QJ at the tank wall connector 7509VC between pins <B and <C (Ref. AWM 28-46-03). Make sure the resistance is between 330 and 480 ohms. If there is: - continuity as specified, go to Step (6) - no continuity as specified (resistance check out of range), go to Step (9).
NOTE : The sensor status (wet or dry) and fuel/air temperature will____ have an effect on the resistance value.
(6) Replace the FLSCU-1 (7QJ) (Ref. AMM TASK 28-46-34-000-001) and (Ref. AMM TASK 28-46-34-400-001).
(7) If the fault continues:
R R (a) Get access to the tank wall connector 7509VC (for the center tank harness 17QT) in the right MLG bay (Ref. AMM TASK 32-12-00-010-001).
(b) Disconnect the free connector 7509VC-A from the receptacle 7509VC.
(c) Do a check (Ref. AWM 28-46-03) of the aircraft wiring (sensor input line - H) between the FLSCU-1 rack connector AB, pin 11A and the tank wall free connector 7509VC-A, pin <B.
(d) Do a check (Ref. AWM 28-46-03) of the aircraft wiring (sensor input line - L) between the FLSCU-1 rack connector AB, pin 11B and the tank wall free connector 7509VC-A, pin <C.
(e) Do a check (Ref. AWM 28-46-01) of the aircraft wiring (FLSCU-1 BITE 1 test command line) between the FLSCU-1 rack connector AA, pin 15B and the FQIC rack connector AB, pin 14F.
(f) Do a check (Ref. AWM 28-46-03) of the aircraft wiring (FLSCU-1 LS7 output line) between the FLSCU-1 rack connector AB, pin 3A and the FQIC rack connector AC, pin 3K.
R R (g) Repair all the unserviceable wiring and connectors (Ref. ESPM 20-00-00).
(h) Connect the free connector 7509VC-A to the receptacle 7509VC.
(i) Do the test given in Para. 3.B.
「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 : 301-399, ∞∞28-46-00∞∞∞∞∞∞∞∞∞∞Page 239
May 01/05 CES
(8) If the fault continues, do a test (Ref. ASM 28-46/01) with a multimeter to see if 28VDC is available at the FLSCU-1 (7QJ) rack connector AA, pin 1B.
(a) If the 28VDC is available:
- go to step (9).
(b) If the 28VDC is not available: 1 Do a check of the aircraft wiring (Ref. AWM 28-46-01) between:
_
- the FLSCU-1 (7QJ) rack connector AA, pin 1B and the C/B-1QJ. 2 Repair all the unserviceable wiring and connectors (Ref. ESPM
_
20-00-00).
3 Do the test given in Para. 3.B.
_
(9) If the fault continues or if there is no continuity in Step (5):
(a) Drain, open and vent the tank (Ref. AMM TASK 28-10-00-910-001) and (Ref. AMM TASK 28-10-00-910-002).
(b) Do a wiring check of the HARNESS-CHAN A, CTR TK (17QT) (Ref. AWM 28-46-03) and replace, if necessary (Ref. AMM TASK 28-42-44-000-001) and (Ref. AMM TASK 28-42-44-400-001).
(c) If the harness is serviceable, replace the SENSOR-HIGH LEVEL, CENTER TANK (20QJ) (Ref. AMM TASK 28-46-15-000-004) and (Ref. AMM TASK 28-46-15-400-012).
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Post SB 28-1087 For A/C 001-049,051-061,101-105,201-203,
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 FUEL 燃油4(54)
