A320飞机维护手册 AMM 时间限制/维护检查 2(33)

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

 |  |  | . distortion, cracks, pulled or |  | |  |  |  |
 |  |  | torn fasteners and damaged |  | |  |  |  |
 |  |  | paintwork. |  | |  |  |  |
 |  |  | - all the components, the pipes, |  |  X  |  |  |  |
 |  |  | the ducts, the electrical looms, |  | |  |  |  |
 |  |  | the cables, the pulleys and the |  | |  |  |  |
 |  |  | mechanical linkages for: |  | |  |  |  |
 |  |  | . distortion, cracks, rupture, |  | |  |  |  |
 |  |  | fluid leakage and breaks. |  | |  |  |  |
 |  |  | |  | |  |  |  |
 |5.  |  | Belly Fairing |  | |  |  |  |
 |  |  | |  | |  |  |  |
 |  A.|  | Examine externally all the belly |  X  | |  |  |  |
 |  |  | fairing panels, specially the leading-|  | |  |  |  |
 |  |  | edge root fairing and upper and lower |  | |  |  |  |
 |  |  | wing fairings, for: |  | |  |  |  |
 |  |  | - erosion, distortion, cracks and |  | |  |  |  |
 |  |  | pulled or torn fasteners. |  | |  |  |  |
 |  |  | If you find damage: |  | |  |  |  |
 |  |  | (1) Remove the damaged panel and |  |  X  |  |  |  |
 |  |  | internally examine the belly |  | |  |  |  |
 |  |  | fairing structure. |  | |  |  |  |
 |  |  | (2) Examine all the components, pipes,|  |  X  |  |  |  |
 |  |  | ducts, electrical looms and their |  | |  |  |  |
 |  |  | mounts for distortion, cracks, |  | |  |  |  |
 |  |  | breaks and fluid leakage. |  | |  |  |  |
 |  |  | |  | |  |  |  |
 |6.  |  | Nose Landing Gear |  | |  |  |  |

 1EFF : ALL 1 05-51-14Page 605 1 1 Nov 01/02R 1 1 1CES 1

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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | |  A.| | Examine the nose landing gear. You |  X  | | | | | | | | must be specially careful when you | | | | | | | | | examine: | | | | | | | | | - the components, the pipes, the | | | | | | | | | electrical looms, the control rods | | | | | | | | | and the bellcranks. | | | | | | -------------------------------------------------------------------------------
Subtask 05-51-14-210-052
R C. Inspection of the Nacelles, Engines and Pylons (Ref. TASK 71-13-00-010-R 040) (Ref. TASK 78-36-00-010-040) (Ref. TASK 72-00-00-200-006) (Ref. TASK R 36-11-00-200-002)
 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Nacelles | | | | | | | | | | | | | | | |  A.| | Examine externally for erosion, |  X  | | | | | | | | distortion, delamination, cracked or | | | | | | | | | flaking paint, loose rivets and signs | | | | | | | | | of shearing: | | | | | | | | | - the air intake cowls, | | | | | | | | | - the fan cowls, | | | | | | | | | - the thrust reverser cowls of the | | | | | | | | | fan. | | | | | | | | | | | | | | | |  B.| | Examine the primary nozzle for |  X  | | | | | | | | erosion, delamination, distortion, | | | | | | | | | cracks, loose rivets and signs of | | | | | | | | | shearing. | | | | | | | | | If you find: | | | | | | | | | - only erosion: | | | | | | | | | no other inspection is necessary. | | | | | | | | | - other damage: | | | | | | | | | (1) Open the fan cowls | |  X  | | | | | | | (Ref. TASK 71-13-00-010-040). | | | | | | | | | (2) Open the fan thrust reverser cowls| | | | | | | | | (Ref. TASK 78-36-00-010-040). | | | | | | | | | Examine the cowls internally for | | | | | |

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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.|
　
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