Subtask 05-51-17-210-054
E. Inspection of the Vertical Stabilizer
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R R R R |ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Primary Structure of the Vertical | | | | | | | | | Stabilizer | | | | | | | | | | | | | | | | A.| | Examine the primary structure | X | | | | | | | | externally for distortion, cracks, | | | | | | | | | pulled or torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | If you find damage : | | | | | | | | | (1) Open the access panels and examine| | X | | | | | | | the attachment fittings and their | | | | | | | | | adjacent structure for : | | | | | | | | | - distortion, cracks, pulled or | | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | (2) Examine the front and rear spar | | X | | | | | | | webs for : | | | | | | | | | - distortion, cracks, pulled or | | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | (3) On the rear spar, examine the | | X | | | | | | | hydraulic lines, mechanical | | | | | | | | | linkages, electrical looms and | | | | | | | | | their mounts for : | | | | | | | | | - distortion, cracks, rupture and | | | | | | | | | fluid leakage. | | | | | |
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Subtask 05-51-17-210-055
F. Inspection of the Wings and Flight Control Surfaces
(Ref. TASK 28-25-00-650-001)
(Ref. TASK 28-10-00-910-002)
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Skin Panels | | | | | | | | | | | | | | | | A.| | Do an inspection of the skin panels : | X | | | | | | | | - make sure that there is (are) no : | | | | | | | | | - distortion or damage, | | | | | | | | | - 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 spar, the rear | | X | | | | | | | spar, the ribs, the skin panels | | | | | | | | | and the skin panel joints. | | | | | | | | | Make sure that : | | | | | | | | | - there is no distortion, | | | | | | | | | - there are no cracks, the skin | | | | | | | | | panels are correctly attached. | | | | | | | | | (4) Examine the internal structure and| | X | | | | | | | the fasteners. | | | | | | | | | Make sure that : | | | | | | | | | - there is no damage or | | | | | | R | | | distortion, | | | | | | | | | - the sealant beads are in good | | | | | | | | | condition, | | | | | | | | | - there are no pulled fasteners. | | | | | | | | | (5) Examine the attachment fittings of| | X | | | | | | | the engine pylon. | | | | | | | | | Make sure that : | | | | | | | | | - there is no distortion, | | | | | | | | | - there are no cracks, | | | | | | | | | - the components are correctly | | | | | | | | | attached. | | | | | | | | | (6) On the front and rear spars, | | X | | | | | | | examine the ducts, lines, cables, | | | | | | R | | | mechanical linkages and their | | | | | | | | | installation. | | | | | |
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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | Make sure that : | | | | | | | | | - there is no distortion, | | | | | | | | | - there are no cracks, | | | | | | | | | - there are no leaks, | | | | | | | | | - the components are correctly | | | | | | | | | attached. | | | | | | | | | | | | | | | | | | (7) Close access to the wing tanks | | | | | | | | | (Ref. TASK 28-10-00-910-002). | | | | | | | | | | | | | | | |2. | | Flaps and Slats | | | | | | | | | | | | | | | | A.| | Examine the slats, flaps and fairing. | X | | | | | | | | Make sure that there is (are) no : | | | | | | | | | - distortion, | | | | | | | | | - cracks or pulled fasteners, | | | | | | | | | - damage. | | | | | | | | | | | | | | | |3. | | Ailerons | | | | | | | | | | | | | | | | A.| | Examine the ailerons. | X | | | | | | | | Make sure that there is (are) no : | | | | | | | | | - damage or distortion, | | | | | | | | | - cracks or pulled fasteners. | | | | | | | | | If you find damage : | | | | | | | | | (1) Examine the aileron hinges and | | X | | | | | | | actuator : | | | | | | | | | Make sure that there is (are) no: | | | | | | | | | - cracks, | | | | | | | | | - damage or distortion. | | | | | | -------------------------------------------------------------------------------
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