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ENGINE FUEL AND CONTROL - GENERAL - FAULT ISOLATION PROCEDURES
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TASK 73-00-00-810-859
Disagree between the Fuel-Flow Indication and the ECU Output on Engine 1
1. Possible Causes
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- DMC-1 (1WT1)
- DMC-2 (1WT2)
- DMC-3 (1WT3)
- FWC-1 (1WW1)
- FWC-2 (1WW2)
2. Job Set-up Information
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A. Referenced Information
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REFERENCE DESIGNATION
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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
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本文链接地址：A320 Trouble Shooting Manual 排故手册 发动机燃油和控制 1(24)
