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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. | | | | | |
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|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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