(a) Repair all the unserviceable wiring and connectors (Ref. ESPM 20-00-00).
「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, ∞∞28-15-00∞∞∞∞∞∞∞∞∞∞Page 211
201-299, 401-499, Aug 01/05 CES (b) Do the test given in Para.3.B.(2).
(10) Do a test, with a multimeter, to make sure that 28VDC is available at the RELAY-R WING TK LOW LEVEL CHANNEL B (6QP) terminals A2 and X1 (Ref. ASM 28-15/01).
(a) If the 28VDC:
- is not available, do step (11)
- is available, continue at step (12).
(11) Do a wiring check of the aircraft wiring (Ref. ASM 28-15/01) between the RELAY-R WING TK LOW LEVEL CHANNEL B (6QP) and the C/B-FUEL/XFR VALVE 1/WING/R (2QP).
(a) Repair all the unserviceable wiring and connectors (Ref. ESPM 20-00-00).
(b) Do the test given in Para. 3.B.(2).
(12) If the fault continues:
(a) Do a check of and replace, if necessary, the relays that follow:
- RELAY-L WING TK LOW LEVEL CHANNEL A (5QP)
- RELAY-R WING TK LOW LEVEL CHANNEL B (6QP)
- RELAY-L OR R REAR XFR VALVE OPEN LATCH (13QP).
(b) Do the test given in Para. 3.B.(2).
(13) If the fault continues:
(a) Do a wiring check of the aircraft wiring (Ref. ASM 28-15/01) between:
- the ACTUATOR connector 11QP-A, pin A and the RELAY 5QP, terminal A3
- the ACTUATOR connector 11QP-A, pin A and the RELAY 6QP, terminal B3
- the RELAY 5QP, terminal A1 and the RELAY 6QP, terminal B2
- the RELAY 5QP, terminal X2 and the RELAY 13QP, terminal A
- the RELAY 6QP, terminal X2 and the RELAY 13QP, terminal B
- the RELAY 13QP, terminal 1 and the FLSCU-1 rack connector 7QJ-AA, pin 5A
- the RELAY 13QP, terminal 3 and the FLSCU-2 rack connector 9QJ-AA, pin 5A.
(14) Repair all the unserviceable wiring and connectors (Ref. ESPM 20-00-00).
(15) Do the test given in Para. 3.B.(2).
「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, ∞∞28-15-00∞∞∞∞∞∞∞∞∞∞Page 212
201-299, 401-499, Aug 01/05 CES TASK 28-15-00-810-805
Intercell XFR Valve 29QM/72QM/10QP (Right Forward) Fault - Stays Closed When The Fuel In The Inner-cell Is At Low Level
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
_______________
- ACTUATOR-TRANSFER VALVE, R FWD SPAR (10QP)
- aircraft wiring
- RELAY-R WING TK LOW LEVEL CHANNEL A (8QP)
- RELAY-L WING TK LOW LEVEL CHANNEL B (7QP)
- RELAY-L OR R FWD XFR VALVE OPEN LATCH (14QP)
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific multimeter
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
ESPM 20-00-00 AMM 28-15-00-740-002 Functional (BITE) Test of the Intercell Transfer
Valves AMM 28-15-51-000-001 Removal of the Actuator 9QP(10QP) AMM 28-15-51-400-001 Installation of the Actuator 9QP(10QP) AMM 28-46-00-740-001 Functional (BITE) Test ASM 28-15/02
「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, ∞∞28-15-00∞∞∞∞∞∞∞∞∞∞Page 213
201-299, 401-499, Aug 01/05 CES
3. Fault Confirmation
__________________
A. Table of the circuit breakers used in this procedure:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FUEL/FQI/CHAN/1 1QT A13 121VU FUEL/FQI/CHAN/2 2QT M27 121VU FUEL/XFR VALVE2/WING/R 4QP M23 121VU FUEL/XFR VALVE2/WING/L 3QP M22
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) FUEL 燃油1(25)
