R -----------------------------------------------------
R (7) At the test point, if 28VDC:
R
R - was available, do step (8)
R
R - was not available, do step (9).
R (8) Replace the ACTUATOR-FUEL CROSSFEED VALVE (5QE) (Ref. AMM TASK 28-23-R 51-000-001) and (Ref. AMM TASK 28-23-51-400-001).
R (9) Do a check (Ref. ASM 28-23/01) of the P/BSW-FUEL/X FEED (4QE) and, if
R necessary, replace it.
R (10) Do a check of the applicable aircraft wiring (Ref. ASM 28-23/01) as
R follows:
R (a) If the actuator 5QE motor 1:
R 1_ Does not turn to the open position:
R - do a wiring check between the P/BSW-4QE, terminal A1 and the
R connector 5QE-A, pin A.
R 2_ Does not turn to the close position:
R - do a wiring check between the P/BSW-4QE, terminal A2 and the
R connector 5QE-A, pin C.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞28-23-00∞∞∞∞∞∞∞∞∞∞Page 203
Nov 01/03 CES
R (b) If the actuator 5QE motor 2:
R 1_ Does not turn to the open position:
R - do a wiring check between the P/BSW-4QE, terminal B1 and the
R connector 5QE-B, pin A.
R 2_ Does not turn to the close position:
R - do a wiring check between the P/BSW-4QE, terminal B2 and the
R connector 5QE-B, pin C.
R (c) Repair all the unserviceable wiring and connectors (Ref. ESPM 20-
R 00-00).
R (11) Do the test given in Para. 3.B.
R (12) If the fault continues, replace the VALVE-FUEL CROSSFEED (10QM) (Ref.
R AMM TASK 28-23-41-000-001) and (Ref. AMM TASK 28-23-41-400-001).
5. Close-up________
R A. Close Access
R
R (1) Put the aircraft back to its initial configuration.
R (2) Remove the ground support and maintenance equipment, the special and
R standard tools and all other items.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞28-23-00∞∞∞∞∞∞∞∞∞∞Page 204
Nov 01/03 CES
TASK 28-23-00-810-802
Fuel-Crossfeed Valve P/BSW-4QE, ON and/or OPEN legends do not come on
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
_______________
- P/BSW-FUEL/X FEED (4QE)
- ACTUATOR-FUEL CROSSFEED VALVE (5QE)
- BOARD-ANN LT TEST & INTFC (6LP)
- ON indicator light (lamp/filament/bulb)
- OPEN indicator light (lamp/filament/bulb)
- aircraft wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
28-23-00-810-801 Fuel-Crossfeed Valve Does Not Open (Close) or Opens
(Closes) Slowly ESPM 20-00-00 AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
External Power AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power AMM 28-23-51-000-001 Removal of the Crossfeed Valve Actuator 5QE AMM 28-23-51-400-001 Installation of the Crossfeed Valve Actuator 5QE AMM 31-60-00-860-001 EIS Start Procedure AMM 31-60-00-860-002 EIS Stop Procedure AMM 33-14-00-710-001 Operational Test of the Annunciator Light Test System
in the Cockpit AMM 33-14-33-000-001 Removal of the Annunciator-Light Test and Interface-Board (1LP, 2LP, 3LP, 4LP, 5LP, 6LP, 7LP, R 8LP, 9LP, 10LP, 11LP, 12LP, 18LP, 19LP, 20LP) AMM 33-14-33-400-001 Installation of the Annunciator-Light Test and Interface-Board (1LP, 2LP, 3LP, 4LP, 5LP, 6LP, 7LP,
R 8LP, 9LP, 10LP, 11LP, 12LP, 18LP, 19LP, 20LP) ASM 28-13/01 ASM 28-23/01 AWM 24-91-07 AWM 28-23-01
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 FUEL 燃油2(24)
