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时间:2011-03-29 09:34来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

_______________
 A. If the fault symptom is identified by the ECAM warning message ENG1 FF DISCREPANCY:
 - replace the DMC-1 (1WT1) (Ref. AMM TASK 31-63-34-000-001) and (Ref. AMM TASK 31-63-34-400-001).
 (1) If the fault continues:

 - replace the DMC-2 (1WT2).

 (2) If the fault continues:

 - replace the DMC-3 (1WT3).

 (3) If the fault continues:


 - replace the FWC-1 (1WW1) (Ref. AMM TASK 31-53-34-000-001) and (Ref. AMM TASK 31-53-34-400-001).
 F 『 EEFF : ALL E ∞∞73-00-00∞∞∞∞∞∞∞∞∞∞Page 201
 E E Nov 01/02 E E ECES
E F 『 E C F M E E E E 56 E E E (4) If the fault continues:


 - replace the FWC-2 (1WW2) (Ref. AMM TASK 31-53-34-000-001) and (Ref. AMM TASK 31-53-34-400-001).
 B. Test
 (1) Do a minimum idle check (Ref. AMM TASK 71-00-00-710-006).
 F 『 EEFF : ALL E ∞∞73-00-00∞∞∞∞∞∞∞∞∞∞Page 202
 E E Feb 01/98 E E ECES
E

 F 『
 E C F M E
 E E
 E 56 E
 E E


 TASK 73-00-00-810-860
 Disagree between the Fuel-Flow Indication and the ECU Output on Engine 2
 1. Possible Causes
_______________
 - DMC-1 (1WT1)

 - DMC-2 (1WT2)

 - DMC-3 (1WT3)

 - FWC-1 (1WW1)

 - FWC-2 (1WW2)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 31-53-34-000-001 Removal of the Flight Warning Computer (FWC) (1WW1,1WW2) R AMM 31-53-34-400-001 Installation of the Flight Warning Computer (FWC)
 (1WW1,1WW2)
 AMM 31-63-34-000-001 Removal of the DMC (1WT1,1WT2,1WT3)
 AMM 31-63-34-400-001 Installation of the DMC (1WT1,1WT2,1WT3)
 AMM 71-00-00-710-006 Minimum Idle Check

 3. Fault Confirmation
__________________
 A. Test
 (1) Not applicable, the fault is evident.
 4. Fault Isolation
_______________
 A. If the fault symptom is identified by the ECAM warning message ENG2 FF DISCREPANCY:
 - replace the DMC-1 (1WT1) (Ref. AMM TASK 31-63-34-000-001) and (Ref. AMM TASK 31-63-34-400-001).
 (1) If the fault continues:

 - replace the DMC-2 (1WT2).

 (2) If the fault continues:

 - replace the DMC-3 (1WT3).

 (3) If the fault continues:


 - replace the FWC-1 (1WW1) (Ref. AMM TASK 31-53-34-000-001) and (Ref. AMM TASK 31-53-34-400-001).
 F 『 EEFF : ALL E ∞∞73-00-00∞∞∞∞∞∞∞∞∞∞Page 203
 E E Nov 01/02 E E ECES
E F 『 E C F M E E E E 56 E E E (4) If the fault continues:


 - replace the FWC-2 (1WW2) (Ref. AMM TASK 31-53-34-000-001) and (Ref. AMM TASK 31-53-34-400-001).
 B. Test
 (1) Do a minimum idle check (Ref. AMM TASK 71-00-00-710-006).
 F 『 EEFF : ALL E ∞∞73-00-00∞∞∞∞∞∞∞∞∞∞Page 204
 E E Feb 01/98 E E ECES
E

 F 『
 E C F M E
 E E
 E 56 E
 E E


 TASK 73-00-00-810-861
 Disagree between the Fuel-Flow Indication and the ECU Output on Engine 1
 1. Possible Causes
_______________
 - FWC-1 (1WW1)

 - FWC-2 (1WW2)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 31-53-34-000-001 Removal of the Flight Warning Computer (FWC) (1WW1,1WW2) R AMM 31-53-34-400-001 Installation of the Flight Warning Computer (FWC) (1WW1,1WW2) AMM 71-00-00-710-006 Minimum Idle Check
 3. Fault Confirmation
__________________
 A. Test
 (1) Not applicable, the fault is evident.
 4. Fault Isolation
_______________
 A. If the fault symptom is identified by the ECAM warning message ENG1 FF DISCREPANCY and CHECK message near the FF indication on the upper ECAM display unit:
 - replace the FWC-1 (1WW1) (Ref. AMM TASK 31-53-34-000-001) and (Ref. AMM TASK 31-53-34-400-001).
 (1) If the fault continues:
 - replace the FWC-2 (1WW2).
 
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