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时间:2011-03-28 13:54来源:蓝天飞行翻译 作者:航空
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 1. Possible Causes
_______________
 - ENG/APU FIRE PNL (1WD) R - aircraft wiring R
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
28-24-00-810-801
28-24-00-810-802 R AMM 26-12-12-000-001 R AMM 26-12-12-400-001 R AMM 26-21-00-710-004 R R R AMM 26-21-00-710-004 R R R AMM 28-24-00-710-002 R
ASM 26-21/02
 ASM 28-24/01
 ASM 76-12/01

RFuel LP Fuel Valve Engine 1 Does Not OpenFuel LP Fuel Valve Engine 1 Does Not Close Removal of the ENG/APU Fire Panel (1WD) Installation of the ENG/APU Fire Panel (1WD) Operational Test of Fire Control Pushbutton Switch Sub-functions Related to Engine Shut Down and Isolation (With External Air-supply Unit) Operational Test of Fire Control Pushbutton Switch Sub-funtions Related to Engine Shut Down and Isolation (With APU) Operational Test of the ENG 1(2) LP Fuel Valve 12QM (13QM)
 「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 211
 Nov 01/00 CES

 

 3. Fault Confirmation__________________ 
R  A. Test 

R  (1) Do the Operational Test of the ENG 1(2) LP Fuel Valve 12QM (13QM) 
R  (Ref. AMM TASK 28-24-00-710-002). 

R  (a) If the ENG 1 LP Fuel Valve 12QM does not open, do (Ref. TASK 28-
24-00-810-801). 
R  (b) If the ENG 1 LP Fuel Valve 12QM does not close, do (Ref. TASK 28-
24-00-810-802). 

R  (2) If the Operational Test of the ENG 1 LP Fuel Valve 12QM operates 
R  correctly, do the Operational Test of the Fire Control P/BSW 
R  Sub-functions Related to Engine 1 Shut Down and Isolation (Ref. AMM 
R  TASK 26-21-00-710-004) or (Ref. AMM TASK 26-21-00-710-004). 
R  (3) If during step (2), when the ENG 1 FIRE P/BSW is first pushed (LP 
R  valve close command) the ACTUATOR-LP FUEL VALVE, ENG 1 (9QG): 

R  (a) Does not close, go to Para. 4.A. 

R  (b) Operates correctly, no maintenance steps are necessary. 

R  NOTE : You can get more data from the:____ 
R  - the Description and Operation section of the Aircraft 
R  Maintenance Manual (AMM) Chapters 26-12-00, 26-21-00, 
R  28-24-00, and 76-12-00 
R  - Trouble Shooting Manual (TSM), Task Supporting Data, 
R  (Ref. P. Block 301) 
R  - Aircraft Schematic Manual (ASM) (Ref. ASM 26-21/02) 
R  (Ref. ASM 28-24/01) and (Ref. ASM 76-12/01).
 4. Fault Isolation_______________ 
R  A. Procedure 

R (1) Do a check of (Ref. ASM 28-24/01) and replace, if necessary, the R ENG/APU FIRE PNL (1WD) (Ref. AMM TASK 26-12-12-000-001) and (Ref. AMM R TASK 26-12-12-400-001).
 「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 212
 Nov 01/00 CES

 

R  (2) If the fault continues, do a check of the aircraft wiring (Ref. ASM 
R  28-24/01) between: 
R  - the connector 1WD-A, pin V and the ACTUATOR-LP FUEL VALVE, ENG 1 
R  connector 9QG-A, pin C (MOT 1, 9QG close supply) 
R  - the connector 1WD-B, pin <C and the ACTUATOR-LP FUEL VALVE, ENG 1 
R  connector 9QG-B, pin C (MOT 2, 9QG close supply). 
R
 (3) Repair all the unserviceable wiring and connectors.
 (4) 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 213
 Nov 01/00 CES


 TASK 28-24-00-810-804

 

 Fuel LP Fuel Valve Engine 1 Status Is Not Available On The FUEL System Page
 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)

 - SDAC-1 (1WV1)
 
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