(9) Connect the electrical supply cable connector 10QG-A to the
ACTUATOR-LP FUEL VALVE, ENG 2 (10QG).
(10) Do the Operational Test of the ENG 1(2) LP Fuel Valve 12QM(13QM) (Ref. AMM TASK 28-24-00-710-002).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞28-24-00∞∞∞∞∞∞∞∞∞∞Page 234
Feb 01/98 CES
TASK 28-24-00-810-809
Fuel LP Fuel Valve Engine 1 Operates Slowly In Both Directions
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 1 (9QG)
- VALVE-LP FUEL, ENG 1 (12QM)
- ENG/APU FIRE PNL (1WD)
- aircraft wiring (motor 2/ground/earth) between the ACTUATOR-LP FUEL VALVE, ENG 1 free connector 9QG-B, pin E and the ground/earth point 4003VN(522STA540)
- C/B-FUEL/LP VALVE/MOT 1/ENG 1 (1QG) (49VU210)
- aircraft wiring between the C/B-FUEL/LP VALVE/MOT 1/ENG 1 (1QG), terminal 2 and the ENG/APU PANEL (1WD) free connector 1WD-A, pin U
- C/B-FUEL/LP VALVE/MOT 2/ENG 1 (3QG) (121VU212)
- aircraft wiring between the C/B-FUEL/LP VALVE/MOT 2/ENG 1 (3QG), terminal 2 and the ENG/APU PANEL (1WD) free connector 1WD-B, pin <B
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific multimeter
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 26-12-12-000-001 Removal of the ENG/APU Fire Panel (1WD)
AMM 26-12-12-400-001 Installation of the ENG/APU Fire Panel (1WD) 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 28-24-01
AWM 94-05-02
「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 235
Nov 01/00 CES 3. Fault Confirmation
__________________
A. Procedure.
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).
(1) 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.
(2) 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).
(3) Make sure the ENG/MASTER 1 (3KC) switch (panel 115VU) is set to OFF.
(4) On the FUEL system page make sure the ENG 1 LP fuel valve symbol shows that the valve is closed (amber crossline).
(5) Make a note of the valve transit time for the following actions:
NOTE : The LP fuel valve symbol shows a 45 degree amber line while in
____
transit.
(a) Set the ENG/MASTER 1 (3KC) switch (panel 115VU) to ON, and immediately observe the ENG 1 LP fuel valve symbol on the FUEL system page.
(b) Make sure the ENG 1 LP fuel valve symbol changes to open (green in-line).
(6) Make a note of the valve transit time for the following actions:
NOTE : The LP fuel valve symbol shows a 45 degree amber line while in
____
transit.
(a) Set the ENG/MASTER 1 (3KC) switch (panel 115VU) to OFF, and immediately observe the ENG 1 LP fuel valve symbol on the FUEL system page.
(b) Make sure the ENG 1 LP fuel valve symbol changes to closed (amber crossline).
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