曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

 |  |  |  items you can see) for distortion,|  |  |  |  |  |
 |  |  |  cracks, pulled or torn fasteners  |  |  |  |  |  |
 |  |  |  and damaged paintwork.  |  |  |  |  |  |
 |  |  |  If you find damage:  |  |  |  |  |  |
 |  |  |  - tell Airbus Industrie about the |  |  X  |  |  |  |
 |  |  |  results.  |  |  |  |  |  |
 |  |  |(10) If you removed components, install|  X  |  |  |  |  |
 |  |  |  serviceable components:  |  |  |  |  |  |
 |  |  |  - for the retraction actuator  |  |  |  |  |  |
 |  |  |  (Ref. TASK 32-31-46-400-001)  |  |  |  |  |  |
 |  |  |  - for the lockstay actuator  |  |  |  |  |  |
 |  |  |  (Ref. TASK 32-11-21-400-001)  |  |  |  |  |  |
 |  |  |  - for the lockstay assembly  |  |  |  |  |  |
 |  |  |  (Ref. TASK 32-11-17-400-001)  |  |  |  |  |  |
 |  |  |  - for the MLG  |  |  |  |  |  |
 |  |  |  (Ref. TASK 32-11-11-400-001)  |  |  |  |  |  |
 |  |  |  - for the side-stay assembly  |  |  |  |  |  |
 |  |  |  (Ref. TASK 32-11-16-400-001)  |  |  |  |  |  |
 |  |  |  - for the shock absorber  |  |  |  |  |  |
 |  |  |  (Ref. TASK 32-11-13-400-001)  |  |  |  |  |  |

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1EFF : ALL 1 05-51-24Page 619 1 1 May 01/05R 1 1 1CES 1

 Subtask 05-51-24-210-051
 D. Inspection of the Wings (Ref. TASK 28-10-00-910-002) (Ref. TASK 28-25-00-650-001)
 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Wings | | | | | | | | | | | | | | | |  A.| | Examine the skin panels for: |  X  | | | | | | | | - damage to the paint, | | | | | | | | | - distortion, | | | | | | | | | - cracks, tears or fuel leaks. | | | | | | | | | If you find damage : | | | | | | | | | (1) Defuel the tanks. | |  X  | | | | | | | (Ref. TASK 28-25-00-650-001). | | | | | | | | | (2) Get access to the wing tanks | |  X  | | | | | | | (Ref. TASK 28-10-00-910-002). | | | | | | | | | (3) Examine the front and rear spars, | |  X  | | | | | | | the internal structure and the | | | | | | | | | fasteners for: | | | | | | | | | - distortion, | | | | | | | | | - cracks, | | | | | | | | | - the condition of the sealant | | | | | | | | | beads, | | | | | | | | | - pulled fasteners. | | | | | | | | | (4) Close access to the wings tanks | |  X  | | | | | | | (Ref. TASK 28-10-00-910-002). | | | | | | | | | (5) Examine the ducts, lines, pipes,  | |  X  | | | | | | | mechanical linkages and their | | | | | | | | | supports for: | | | | | | | | | - distortion, | | | | | | | | | - cracks or leaks of fluid, | | | | | | | | | - the correct attachment of | | | | | | | | | components, | | | | | | | | | - damage. | | | | | | | | | | | | | | | |2. | | Flaps and flap track fairings | | | | | | | | | | | | | | | |  A.| | Examine the flaps and the bottom flap |  X  | | | | | | | | track fairings for: | | | | | | | | | - distortion, | | | | | | | | | - dents, cracks, pulled or torn | | | | | | | | | fasteners, | | | | | | | | | - damage to the paint. | | | | | |
 1EFF : ALL 1 05-51-24Page 620 1 1 May 01/05R 1 1 1CES 1

 -------------------------------------------------------------------------------
|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | |  B.| | At rib 6, examine the flap track |  X  | | | | | | | | fairing and the adjacent structure | | | | | | | | | for: | | | | | | | | | - damage, | | | | | | | | | - cracks, pulled or torn fasteners, | | | | | | | | | - distortion. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the flap and carriages and| |  X  | | | | | | | tracks/beams for: | | | | | | | | | - distortion, | | | | | | | | | - cracks, | | | | | | | | | - damage. | | | | | | | | | (2) Examine the adjacent structure | |  X  | | | | | | | for: | | | | | | | | | - distortion, | | | | | | | | | - cracks, pulled or torn fasteners, | | | | | | | | | - damage. | | | | | | | | | (3) Examine wing internal structure | |  X  | | | | | | | adjacent to the front and aft | | | | | | | | | mountings of the flap beams for: | | | | | | | | | - distortion, | | | | | | | | | - cracks, | | | | | | | | | - damage to the sealant. | | | | | | | | | (4) Examine the area where the MLG is | |  X  | | | | | | | attached and the adjacent | | | | | | | | | structure for: | | | | | | | | | - cracks or leaks of fuel, | | | | | | | | | - distortion. | | | | | | -------------------------------------------------------------------------------
　
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