-------------------------------------------------------------------------------
|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | and damaged paintwork. | | | | | | | | | If you find damage : | | | | | | | | | (1) Examine the upper fuselage section| | |  X  | | | | | | internally (the frames, stringers,| | | | | | | | | cleats, and splices) for : | | | | | | | | | - distortion, cracks pulled or | | | | | | | | | torn fasteners, damaged | | | | | | | | | paintwork. | | | | | | | | | | | | | | | | D.| | From FR47 to FR70 : | | | | | | | | | - examine the frames, skin panels, | | | | | | | | | splices, stringers and rivets for: | | | | | | | | | - distortion, cracks, pulling, tears | | | | | | R | | | and damaged paintwork. | | | | | | | | | | | | | | | | E.| | Examine the cut-out corners and rivets| | | | | | | | | of the emergency-exit surround panel | | | | | | | | | for : | | | | | | R | | | - distortion, cracks, pulling, tears | | | | | | | | | and damaged paintwork. | | | | | | | | | | | | | | | |4. | | Horizontal stabilizer cut-out | | | | | | | | | | | | | | | |  A.| | Examine the cut-out corners for |  X  | | | | | | | | cracks. | | | | | | | | | If you find damage : | | | | | | | | | Examine the cut-out edges of the top  | |  X  | | | | | | | and bottom stringers for : | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | NOTE: Do these inspections together, | | | | | | | | | with the horizontal stabilizer | | | | | | | | | inspection. | | | | | | -------------------------------------------------------------------------------

 **ON A/C ALL

 Subtask 05-51-17-210-052
 C. Inspection of the Pylons and the Nacelles
 (Ref. TASK 71-13-00-010-040)
 (Ref. TASK 78-36-00-010-040)

 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Pylons | | | | | | | | | | | | | | | |  A.| | Examine for distortion and cracks the |  X  | | | | | | | | pylon lateral panels around the access| | | | | | | | | door cut-outs between : | | | | | | | | | - ribs 2 and 3, | | | | | | | | | - ribs 5 and 6. | | | | | | | | | If you find damage : | | | | | | | | | (1) Open the engine cowlings and | |  X  | | | | | | | examine the main frame, the lower | | | | | | | | | spar, and the rib-to-panel | | | | | | | | | attachments for: | | | | | | | | | - distortion, cracks, pulled or | | | | | | | | | torn fasteners. | | | | | | | | | (2) Examine all the ducts, lines, | |  X  | | | | | | | electrical looms and their mounts | | | | | | | | | for distortion, cracks, rupture | | | | | | | | | and fluid leakage. | | | | | | | | | | | | | | | |2. | | Nacelles | | | | | | | | | | | | | | | |  A.| | Examine the nacelle and the primary |  X  | | | | | | | | nozzle externally for : | | | | | | | | | - distortion, cracks, delamination, | | | | | | R | | | cracked or flaking paint, loose | | | | | | R | | | rivets, signs of shearing. | | | | | | | | | If you fing damage : | | | | | | | | | (1) Open the fan cowl doors | |  X  | | | | | | | (Ref. TASK 71-13-00-010-040). | | | | | | | | | (2) Open the thrust reverser doors | | | | | | | | | (Ref. TASK 78-36-00-010-040). | | | | | | | | | Examine internally for signs of | | | | | | | | | damage. | | | | | | | | | (3) Examine the attachments of the air| |  X  | | | |

 -------------------------------------------------------------------------------
R
R
R
|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | intake cowl to the fan case for | | | | | | | | | distortion, cracks, and pulled or | | | | | | | | | torn fasteners. Examine the | | | | | | | | | attachments of the primary nozzle | | | | | | | | | to the engine. | | | | | | | | | (4) Examine all the cowl attachment | |  X  | | | | | | | points on the pylon. Examine all | | | | | | | | | the cowl hinge fittings. | | | | | | | | | (5) Visually examine the engine | |  X  | | | | | | | equipment, support, fasteners, | | | | | | | | | brackets and pipes for damage. | | | | | | -------------------------------------------------------------------------------
Subtask 05-51-17-210-053
 D. Inspection of the Horizontal Stabilizer
 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Wing center box (rib 3) | | | | | | | | | | | | | | | |  A.| | Examine the top and bottom skin panels|  X  | | | | | | | | and actuator fittings, the ribs and | | | | | | | | | the spar rivets for : | | | | | | | | | - distortion, cracks, pulling, tears | | | | | | | | | and damaged paintwork. | | | | | | | | | If you find damage : | | | | | | | | | (1) Examine the rear spar web on each | |  X  | | | | | | | side of the pivot bearing fittings| | | | | | | | | for : | | | | | | | | | - distortion, cracks, pulled or | | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | (2) Examine the hydraulic lines, | |  X  | | | | | | | mechanical linkages electrical | | | | | | | | | looms and their mounts for : | | | | | | | | | - distortion, cracks, rupture | | | | | | | | | and fluid leakage. | | | | | | -------------------------------------------------------------------------------
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM 時間限制/維護檢查 2(53)