- SDAC-2 (1WV2)
- aircraft wiring (motor 1/ground/earth) between the ACTUATOR-LP VALVE, ENG 1 (9QG) connector 9QG-A, pin E and the ground/earth point 4001VN(521STA332)
- aircraft wiring(closed signal line/SDAC-1) between the ACTUATOR-LP VALVE, ENG 1 (9QG) connector 9QG-A, pin B and the SDAC-1 (1WV-1) connector AA, pin 2C
- aircraft wiring (open signal line/SDAC-1) between the ACTUATOR-LP VALVE, ENG 1 (9QG) connector 9QG-A, pin D and the SDAC-1 (1WV-1) connector AA, pin 1C
- aircraft wiring(closed signal line/SDAC-2) between the ACTUATOR-LP VALVE, ENG 1 (9QG) connector 9QG-A, pin B and the SDAC-2 (1WV-2) connector AA, pin 2C
- aircraft wiring (open signal line/SDAC-2) between the ACTUATOR-LP VALVE, ENG 1 (9QG) connector 9QG-A, pin D and the SDAC-2 (1WV-2) connector AA, pin 1C
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 28-24-00-710-002 Operational Test of the ENG 1(2) 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
AMM 31-55-34-000-001 Removal of the SDAC (1WV1,1WV2)
AMM 31-55-34-400-001 Installation of the SDAC (1WV1,1WV2)
ASM 26-21/02
ASM 28-24/01
ASM 76-12/01
AWM 28-24-01
AWM 31-54-77
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞28-24-00∞∞∞∞∞∞∞∞∞∞Page 214
Feb 01/98 CES
3. Fault Confirmation
__________________
A. Not applicable, the fault is evident.
NOTE : You can get more data from the:
____
- Aircraft Maintenance Manual (AMM) Chapters 26-12-00, 26-21-00, 28-24-00, and 76-12-00 - Description and Operation (D and O)
- Trouble Shooting Manual (TSM), Task Supporting Data, (Ref. P. Block 301)
- Aircraft Schematic Manual (ASM) (Ref. ASM 26-21/02), (Ref. ASM 28-24/01), and (Ref. ASM 76-12/01).
4. Fault Isolation
_______________
A. On the ENG/APU FIRE PANEL (1WD) located on the overhead panel 20VU, make sure that the ENG 1 FIRE PUSH pushbutton switch (P/BSW) is in the closed and guarded position.
(1) On the ECAM Control Panel 11VU, push (in) the FUEL P/BSW to get the FUEL system page on the ECAM lower display unit (DU).
(2) Set the ENG/MASTER 1 (3KC) switch (panel 115VU) to OFF.
(3) Disconnect the electrical supply cable connector (9QG-A) from the ACTUATOR-LP FUEL VALVE, ENG 1 (9QG).
(4) Examine the ENG 1 LP fuel valve symbol on the FUEL system page.
(a) If the ENG 1 LP fuel valve symbol shows in transit (diagonal amber line):
1_ Temporarily put a ground/earth on free connector 9QG-A, pin B
and examine the ENG 1 LP fuel valve symbol on the FUEL system
page, - make note.
2_ Remove the ground/earth temporarily placed on free connector
9QG-A, pin B.
3_ Temporarily put a ground/earth on free connector 9QG-A, pin D
and examine the ENG 1 LP fuel valve symbol on the FUEL system
page, - make note.
4_ Remove the ground/earth temporarily placed on free connector
9QG-A, pin D.
5_ If in steps 1_ and 3_ the LP fuel valve symbol agrees with the
table that follows:
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞28-24-00∞∞∞∞∞∞∞∞∞∞Page 215
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--------------------------------------------------------------
| CONNECTOR 9QG-A, PIN GROUNDED | LP FUEL VALVE SYMBOL |
|--------------------------------|-----------------------------|
| B | AMBER CROSS LINE = CLOSED |
| D | AMBER IN LINE = OPEN |
--------------------------------------------------------------
- do a check (Ref. AWM 28-24-01) of the aircraft wiring (motor 1/ground/earth) between the ACTUATOR-LP VALVE, ENG 1 (9QG) connector 9QG-A, pin E and the ground/earth point 4001VN(521STA332).
6 Repair all the unserviceable wiring and connectors.
_
7 Connect the electrical supply cable connector 9QG-A to the
_ ACTUATOR-LP VALVE FUEL VALVE, ENG 1 (9QG).
8 Do the Operational Test of the ENG 1(2) LP Fuel Valve
_ 12QM(13QM) (Ref. AMM TASK 28-24-00-710-002).
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 FUEL 燃油2(38)
