- aircraft wiring between the FQIC (3QT) rack connector B, contact 2E and

 the PRESELECTOR-FUEL QTY (5QT) connector A, contact L R - aircraft wiring between the FQIC (3QT) rack connector pin B05F and R MSW-REFUEL.DEFUEL CTL DOOR POSITION (20QU) R - aircraft wiring between the FQIC (3QT) rack connector pin B05F and R RELAY-L/G POSITION, SYS 1 (11GB) R - aircraft wiring between the RELAY-FQIC C/O SPLY (9QT) 103VU terminal A2, R and the FQIC (3QT) rack connector, pin C08H. R - aircraft wiring between the FQIC (3QT) rack connector C, contact 7C and R the PRESELECTOR-FUEL QTY, COCKPIT (10QT) rack connector A, contact N R - aircraft wiring between the FQIC (3QT) rack connector C, contact 8C and R the RELAY-REFUEL/DEFUEL CTL PNL DOOR POSITION (14QU), terminal C1 R - aircraft wiring between the RELAY-COCKPIT REFUEL POWER (26QU) terminal C1, R and the FQIC (3QT) rack connector C, contact 7E R - aircraft wiring between the FQIC (3QT) rack connector C, contact 5C and R the PRESELECTOR-FUEL QTY, COCKPIT (10QT) connector A, pin M R - aircraft wiring between the FQIC (3QT) rack connector C, contact 7H and R the PRESELECTOR-FUEL QTY (5QT) rack connector A, contact N R - aircraft wiring between the SW-MODE SELECT/REFUEL/DEFUEL/XFR (3QU) R terminal 3D and the FQIC (3QT) rack connector C, contact 8E R - aircraft wiring between the FQIC (3QT) rack connector C, contact 5D and R the PRESELECTOR FUEL QTY, COCKPIT (10QT) connector A, pin L R - aircraft wiring between the FQIC (3QT) rack connector C, contact 7G and R the IND-FUEL QTY MULTI TANK (6QT) rack connector A, contact N R - aircraft wiring between the FQIC (3QT) rack connector C, contact 4J and R the PRESELECTOR-FUEL QTY (5QT) connector A, contact M R - aircraft wiring between the C/B-FUEL/FQI/CHANNEL 1 AND 2 (8QT) and the R FQIC (3QT) rack connector C, contact 9E R - aircraft wiring between the FQIC (3QT) rack connector C, contact 4K and R the PRESELECTOR-FUEL QTY (5QT) connector A, contact L R - aircraft wiring between the SW-REFUEL VALVES/OPEN/NORMAL/SHUT, R WING TK R (6QU) terminal 3, and the FQIC (3QT) rack connector C, contact 8B R - aircraft wiring between the SW-REFUEL VALVES/OPEN/NORMAL/SHUT, L WING TK
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞28-25-00∞∞∞∞∞∞∞∞∞∞Page 204
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R R R R R R R R R  (5QU) terminal 3, and the FQIC (3QT) rack connector C, contact 8A - aircraft wiring between the SW-REFUEL VALVES/OPEN/NORMAL/SHUT, CTR TK (4QU) terminal 3, and the FQIC (3QT) rack connector C, contact 9B - aircraft wiring between the FQIC (3QT) rack connector C, contact 8J, and the RELAY-R WING TK REFUEL VALVE CONTROL (16QU), terminal X1 - aircraft wiring between the FQIC (3QT) rack connector C, contact 8K, and the RELAY-L WING TK REFUEL VALVE CONTROL (15QU), terminal X1 - aircraft wiring between the FQIC (3QT) rack connector C, contact 9J, and the RELAY-CTR TK VALVE CONTROL (17QU), terminal X1
 2. Job Set-up Information______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
28-25-00-810-803 AMM 12-11-28-650-003 AMM 12-11-28-650-004 AMM 28-42-21-000-001 AMM 28-42-21-000-002 AMM 28-42-21-400-001 AMM 28-42-21-400-002 AMM 28-42-34-000-001 AMM 28-42-34-400-001 ASM 28-25/01 ASM 28-25/01 ASM 28-42/03 Refuel-Valve System Failure in Manual Control (Fails to Open)Pressure Refuel with Automatic ControlPressure Refuel with Manual ControlRemoval of the Fuel Quantity Preselector 5QTRemoval of the Fuel Quantity Preselector 10QTInstallation of the Fuel Quantity Preselector 5QTInstallation of the Fuel Quantity Preselector 10QTRemoval of the Fuel Quantity-Indicating Computer (FQIC) (3QT)Installation of the Fuel Quantity-Indicating Computer (FQIC) (3QT)
 3. Fault Confirmation__________________
 A. Make sure that the steps in the pressure refuel with auto control (Ref. AMM TASK 12-11-28-650-003), are complied with.
 NOTE : The refuel valve will not open if the related tank is full of____ fuel.

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞28-25-00∞∞∞∞∞∞∞∞∞∞Page 205
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 4. Fault Isolation
_______________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 A. If the optional PRESELECTOR is installed:
 - do the refuel from the other unit.
 (1) If the fault continues:

 - do the pressure refuel with manual control (Ref. AMM TASK 12-11-28-650-004).

 (2) If the fault continues with manual control:

 - do (Ref. TASK 28-25-00-810-803).
　
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 FUEL 燃油2(61)