| | | wing leading edges. | | | | | |
| | | (2) Examine the remaining tracks and | | X | | | |
| | | their mountings for distortion, | | | | | |
| | | cracks, pulled or torn fasteners | | | | | |
| | | and damaged paintwork. | | | | | |
| | | (3) Examine the rack teeth of the | | X | | | |
| | | remaining tracks and their | | | | | |
| | | attachments for distortion, cracks| | | | | |
| | | and pulled or torn fasteners. | | | | | |
| | | | | | | | |
|3. | | Slat Track Rib and Hold-Down Rib | | | | | |
| | | Structure | | | | | |
| | | | | | | | |
| A.| | Examine the ribs of tracks No. 5 and | X | | | | |
| | | 10 for distortion, cracks, pulled or | | | | | |
| | | torn fasteners, damaged paintwork and | | | | | |
| | | fuel leaks. | | | | | |
| | | | | | | | |
| B.| | Examine the hold-down stops for | X | | | | |
| | | distortion, cracks and damage. | | | | | |
| | | | | | | | |
| | | If you find damage on items A. or B.: | | | | | |
| | | (1) Open all the access panels of the | | X | | | |
| | | wing leading edges. | | | | | |
| | | (2) Examine the ribs of the remaining | | X | | | |
| | | tracks for distortion, cracks, | | | | | |
| | | pulled or torn fasteners, damaged | | | | | |
| | | paintwork and fuel leaks. | | | | | |
| | | (3) Defuel the wing tanks | | X | | | |
| | | (Ref. TASK 28-25-00-650-001). | | | | | |
| | | (4) Get access to the wing tanks | | X | | | |
| | | (Ref. TASK 28-10-00-910-002). | | | | | |
| | | (5) Examine the front spar area for | | X | | | |
| | | distortion, cracks and damaged | | | | | |
| | | sealant fillets. | | | | | |
| | | (6) Close access to the wing tanks | | | | | |
-------------------------------------------------------------------------------
1EFF : ALL 1 05-51-13Page 615 1 1 May 01/02R 1 1 1CES 1
Subtask 05-51-13-710-050
E. Operational Test of the Flight Control Surfaces (Ref. TASK 27-54-00-710-001), (Ref. TASK 27-84-00-710-001), (Ref. TASK 27-64-00-710-001).
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Do an operational test of the flaps | X | | | | | | | | (Ref. TASK 27-54-00-710-001). | | | | | | | | | Make sure that the flaps move | | | | | | | | | smoothly and freely. | | | | | | | | | | | | | | | |2. | | Do an operational test of the slats | X | | | | | | | | (Ref. TASK 27-84-00-710-001). | | | | | | | | | Make sure that the slats move | | | | | | | | | smoothly and freely. | | | | | | | | | | | | | | | |3. | | Do an operational test of the | X | | | | | | | | spoilers (Ref. TASK 27-64-00-710-001).| | | | | | | | | Make sure that the spoilers move | | | | | | | | | smoothly and freely. | | | | | | -------------------------------------------------------------------------------
5. Close-up
________
Subtask 05-51-13-410-050
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM 時間限制/維護(hù)檢查 2(30)
