Also, if the ground/earth was missing from the pin E, of connector 10QG-A, motor 1 of the actuator would not operate. In such a case the valve would move slowly in both directions powered by motor 2 only.
3 Reconnect the electrical supply connector 10QG-A to the
_ ACTUATOR-LP FUEL VALVE, ENG 2 (10QG).
(b) Disconnect the electrical supply connector 10QG-B from the ACTUATOR-LP FUEL VALVE, ENG 2 (10QG).
1 Do a check to see if 28VDC is available between the pins as
_
shown in the table that follows.
-------------------------------------------------| SIGNAL LINE | CONNECTOR 10QG-B | |-----------------------------|-------------------| | MOTOR 2 OPEN 28VDC SUPPLY | A | | MOTOR 2 GROUND/EARTH | E | -------------------------------------------------
NOTE : If the ground/earth is missing from the pin E, of
____ connector 10QG-B, motor 2 of the actuator would not operate. In such a case the valve would move slowly in both directions powered by motor 1 only.
(5) If the supplies are:
(a) Correct as given in the tables above:
1 Replace the ACTUATOR-LP FUEL VALVE, ENG 2 (10QG), (Ref. AMM
_ TASK 28-24-51-000-001), and (Ref. AMM TASK 28-24-51-400-001).
2 If the fault continues:
_
- replace the VALVE-LP FUEL, ENG 2 (13QM), (Ref. AMM TASK 28-24-41-000-001), and (Ref. AMM TASK 28-24-41-400-001).
(b) Not correct as given in the tables above:
- do a check of the RELAY-ENG/MASTER 2 (12QG) 103VU126 and replace if necessary.
(6) Do the test given in Para. 3.A.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞28-24-00∞∞∞∞∞∞∞∞∞∞Page 260
Feb 01/98 CES
(7) If the fault continues do a wiring check (Ref. AWM 28-24-02) of the:
- aircraft wiring (motor 1 open supply) between the RELAY-ENG/MASTER2 (12QG), terminal A3, and the electrical supply connector 10QG-A, pin A
- aircraft wiring (motor 2 open supply) between the RELAY-ENG/MASTER2 (12QG), terminal B3, and the electrical supply connector 10QG-B, pin A.
(8) Repair all the unserviceable wiring and connectors.
(9) Do the test given in Para. 3.A.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞28-24-00∞∞∞∞∞∞∞∞∞∞Page 261
Feb 01/98 CES
TASK 28-24-00-810-815
Fuel LP Fuel Valve Engine 2 Closes Slowly, Opens Correctly
WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
WARNING : WHEN YOU WORK ON THE FUEL SYSTEM WIRING, YOU MUST USE TEST EQUIPMENT
_______ THAT IS APPROVED TO EUROPEAN SPECIFICATION EN50-020. THE USE OF TEST EQUIPMENT THAT IS NOT APPROVED CAN CAUSE FIRE OR AN EXPLOSION.
1. Possible Causes
_______________
- ACTUATOR-LP FUEL VALVE, ENG 2 (10QG)
- VALVE-LP FUEL, ENG 2 (13QM)
- RELAY-ENG/MASTER 2 (12QG) 103VU126
- aircraft wiring (motor 1 close supply) between the RELAY-ENG/MASTER 2 (12QG), terminal A1, and the electrical supply connector 10QG-A, pin C
- aircraft wiring (motor 2 close supply) between the RELAY-ENG/MASTER 2 (12QG), terminal B1, and the electrical supply connector 10QG-B, pin C
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific multimeter
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R AMM 28-24-41-000-001 Removal of the LP Fuel Valve 12QM(13QM)
R AMM 28-24-41-400-001 Installation of the LP Fuel Valve 12QM(13QM) AMM 28-24-51-000-001 Removal of the LP Fuel Valve Actuator AMM 28-24-51-400-001 Installation of the LP Fuel Valve Actuator ASM 26-21/02 ASM 28-24/01 ASM 76-12/01 AWM 28-24-02 AWM 94-06-02
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞28-24-00∞∞∞∞∞∞∞∞∞∞Page 262
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