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Subtask 05-51-14-210-054
E. Inspection of the Wings (Ref. TASK 32-11-00-200-001)
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Leading Edge, Fillets and Slats | | | | | | | | | | | | | | | | A.| | Examine for erosion, distortion, | X | | | | | | | | cracks and pulled or torn fasteners. | | | | | | | | | If you find: | | | | | | | | | (1) Only erosion: | | | | | | | | | - no other inspection is necessary.| | | | | | | | | (2) Other damage: | | | | | | | | | - examine the leading edge | | X | | | | | | | section internally at and near | | | | | | | | | the damage, for distortion, | | | | | | | | | cracks and pulled or torn | | | | | | | | | fasteners, | | | | | | | | | - examine the ducts and the related| | X | | | | | | | attach points for damage, | | | | | | | | | - examine the slat section for | | X | | | | | | | distortion, cracks, pulled | | | | | | | | | or torn fasteners and damaged | | | | | | | | | paintwork, | | | | | | | | | - examine the actuators, the slat | | X | | | | | | | tracks and the slat-track attach | | | | | | | | | points for damage, | | | | | | | | | - examine the slat tracks for | | X | | | | | | | brinelling on the roller tracks. | | | | | | | | | - examine the aileron servo-| | X | | | | | | | controls and the hinge fittings | | | | | | | | | for damage, | | | | | | | | | - examine the spoiler actuators | | X | | | | | | | and the hinge fittings for | | | | | | | | | damage. | | | | | | | | | | | | | | | |2. | | Wing Tip Fairings and Navigation | | | | | | | | | Lights | | | | | | | | | | | | | | | | A.| | Examine for erosion, distortion, | X | | | | | | | | cracks, and pulled or torn fasteners. | | | | | | | | | | | | | | | |3. | | Main Landing Gear (MLG) and Doors | | | | | | | | | | | | | | |
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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.|
| |CODE| | 1 | 2 | 3 |SIGN|FIG.|
|----|----|---------------------------------------|-----|-----|-----|----|----|
| A.| | If the MLG was extended during the | | | | | |
| | | bird or hail strike: | | | | | |
| | | - examine the MLG. Examine the doors, | X | | | | |
| | | the components, the pipes, the | | | | | |
| | | cables, the pulleys and the | | | | | |
| | | electrical looms installed on the | | | | | |
| | | MLG | | | | | |
| | | (Ref. TASK 32-11-00-200-001). | | | | | |
| | | | | | | | |
| B.| | If the MLG was retracted during the | | | | | |
| | | bird or hail strike: | | | | | |
| | | - examine the MLG doors for damage. | X | | | | |
| | | | | | | | |
|4. | | Main Structure of the Wing | | | | | |
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