A. Cracks None permitted If the connector has a crack replace it (Ref. CMM 71-50-03).
B. Damaged Threads None permitted If the connector is damaged replace it (Ref. CMM 71-50-03).
C. Connection Must be fully engaged Tighten the connector with your hand.
2. Examine the connector
adapter, look for:
A. Cracks None permitted If cracks are found replace the adapter (Ref. CMM 71-50-03).
B. Damage None permitted If damage is found replace the adapter, (Ref. CMM 71-50-03).
C. Connection Must be fully engaged Tighten the adapter as required.
D. Missing lockwire None permitted Replace the lockwire or
or safety cable safety cable (Ref. AMM 70-71-45).
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3. Examine the harness DR-25/16 outer jacket, look for:
A. Cracks
B. Cuts
4. Examine the harness M23053/13 Viton outer jacket, look for:
A. Cracks
B. Cuts
5. Examine the connector boots, look for:
A. Cracks
B. Missing sealant
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None permitted If cracks are found and it is not possible to remove the damaged harness from the aircraft, temporarily repair the outer jacket (Ref. AMM 70-71-53).
0.5 inch (12.7 mm) maximum length, 0.12 inch (3.04 mm) maximum width If cut is less than thepermitted limits, and itis not possible to removethe damaged harness, do temporary repair (Ref. AMM 70-71-53). If cut is more than the permitted limits replace the outer jacket (Ref. CMM 71-50-03).
None permitted If cracks are found repair the outer jacket (Ref. AMM 70-71-53).
None permitted If cuts are found replace the outer jacket (Ref. CMM 70-50-03).
None permitted If cracks are found replace the connector boot (Ref. CMM 71-50-03).
None permitted Add sealant where missing (Ref. CMM 71-50-03).
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6. Examine the transition fittings, look for:
A. Cracks None permitted
R
R B. Missing sealant None permitted
7. Examine the harness clamps and their attaching parts, look for:
A. Corrosion None permitted
B. Damage None permitted
C. Missing Parts None permitted
D. Loose fasteners None permitted
8. Examine the harness wires, if they are visible, look for :
A. Cracks, cuts and nicks None permitted
If cracks are found replace the transition fitting (Ref. CMM 71-50-03).
Add sealant where missing (Ref. CMM 71-50-03).
Replace clamps or hardware that is corroded (Ref. IPC 71-51-00).
Replace clamps or hardware that is damaged (Ref. IPC 71-51-00).
Replace clamps or hardware that is missing (Ref. IPC 71-51-00).
Tighten all loose, fasteners.
Replace the harness(Ref. TASK 71-51-43-000-043) and (Ref. TASK 71-51-43-400-043) or (Ref. TASK 71-51-43-000-044) and (Ref. TASK 71-51-43-400-044) or i
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-------------------------------------------------------------------------------(Ref. TASK 71-51-43-000-045) and (Ref. TASK 71-51-43-400-045) or (Ref. TASK 71-51-43-000-046) and (Ref. TASK 71-51-43-400-046) or (Ref. TASK 71-51-43-000-047) and (Ref. TASK 71-51-43-400-047) or (Ref. TASK 71-51-43-000-048) and (Ref. TASK 71-51-43-400-048) or (Ref. TASK 71-51-43-000-049) and (Ref. TASK 71-51-43-400-049) or (Ref. TASK 71-51-43-000-004) and (Ref. TASK 71-51-43-400-004) or (Ref. TASK 71-51-43-000-001) and (Ref. TASK 71-51-43-400-001) or (Ref. TASK 71-51-43-000-002) and (Ref. TASK 71-51-43-400-002) or (Ref. TASK 71-51-43-000-003) and (Ref. TASK 71-51-43-400-003) or (Ref. TASK 71-52-43-000-042) and (Ref. TASK 71-52-43-400-042) or (Ref. TASK 71-52-43-000-043) and (Ref. TASK 71-52-43-400-043)
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本文鏈接地址：A320飛機維護手冊 AMM 動力裝置 POWER PLANT 2(12)
