(3)
Clean the aircraft externally (Ref. TASK 12-21-11-615-001).
Subtask 05-51-25-210-064
B. Internal Inspection
(Ref. TASK 35-12-41-100-001)
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the cabin area | | | | | | | | | | | | | | | | A.| |Examine the cabin area for dust | X | | | | | | | |contamination. | | | | | | | | |If you find contamination: | | | | | | R | | |(1) Clean all the surfaces that have | | X | | | | R | | | contamination. | | | | | | | | | | | | | | | | B.| |Examine the cockpit for dust | X | | | | | | | |contamination. | | | | | | | | |If you find contamination: | | | | | | R | | |(1) Clean all the surfaces that have | | X | | | | R | | | contamination. | | | | | | | | |(2) Examine the oxygen full face | | X | | | | | | | masks for contamination. | | | | | | | | | If you find contamination : | | | | | | | | | (a) Clean the oxygen full face | | | X | | | | | | masks | | | | | | | | | (Ref. TASK 35-12-41-100-001). | | | | | | | | | | | | | | | | C.| |Examine the avionics compartment (all | X | | | | | | | |the items you can see), specially: | | | | | | | | |- around the ventilated components | | | | | | | | |- the plugs | | | | | | | | |- the equipment | | | | | | | | |for dust contamination. | | | | | | | | |If you find contamination: | | | | | | R | | |(1) Clean all the surfaces that have | | X | | | | R | | | contamination. | | | | | | | | | | | | | | | | D.| |Examine the cargo compartments for dust| X | | | | | | | |contamination. | | | | | | | | |If you find contamination: | | | | | | R | | |(1) Clean all the surfaces that have | | X | | | | R | | | contamination | | | | | | R | | | (specially the PDU sensors). | | | | | |
-------------------------------------------------------------------------------
|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | |(2) Examine the cargo drainage system | | X | | | | | | | (if installed) for dust | | | | | | | | | contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (a) Replace the filters of the | | | X | | | | | | drain funnels. | | | | | | -------------------------------------------------------------------------------
Subtask 05-51-25-210-065
C. Inspection of the Fuselage, the Wings and the Stabilizers
(Ref. TASK 53-15-11-200-001) (Ref. TASK 56-11-11-200-001)
(Ref. TASK 56-11-12-200-001) (Ref. TASK 56-12-11-200-001)
(Ref. TASK 56-21-13-200-001) (Ref. TASK 56-31-00-210-001)
(Ref. AMM 122227 PB 301)
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the fuselage | | | | | | | | | | | | | | | | A.| | Examine the radome skin for damage | X | | | | | | | | (Ref. TASK 53-15-11-200-001). | | | | | | | | | | | | | | | | B.| | Examine the windshield, the fixed | X | | | | | | | | windows and the sliding windows for | | | | | | | | | damage: | | | | | | | | | - for the windshield | | | | | | | | | (Ref. TASK 56-11-11-200-001) | | | | | | | | | - for the fixed windows | | | | | | | | | (Ref. TASK 56-11-12-200-001) | | | | | | | | | - for the sliding windows | | | | | | | | | (Ref. TASK 56-12-11-200-001) | | | | | | | | | | | | | | | | C.| | Examine the passenger cabin windows | X | | | | | | | | the passenger/crew doors and | | | | | | | | | the emergency exit windows for | | | | | | | | | damage | | | | | | | | | (Ref. TASK 56-21-13-200-001) | | | | | | | | | (Ref. TASK 56-31-00-210-001). | | | | | | | | | | | | | | | | D.| | Examine all of the fuselage skin, the | X | | | | |
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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | belly fairing and the wing-to-fuselage| | | | | | | | | fairings for damage. | | | | | | | | | | | | | | | | E.| | Examine the ram air inlet and outlet, | X | | | | | | | | the air inlet and outlet flaps for | | | | | | | | | damage. | | | | | | | | | | | | | | | |2. | | Inspection of the Wings | | | | | | | | | | | | | | | | A.| | Examine all the static dischargers for| X | | | | | | | | damage. | | | | | | | | | | | | | | | | B.| | Examine the top and bottom skin of the| X | | | | | | | | wings for damage. | | | | | | | | | | | | | | | | C.| | Examine the flap track fairings for | X | | | | | | | | damage. | | | | | | | | | | | | | | | | D.| | Examine the skin of all the control | X | | | | | | | | surfaces (slats, flaps, ailerons | | | | | | | | | and spoilers), specially the leading | | | | | | | | | and the trailing edges, for damage. | | | | | | | | | | | | | | | | E.| | Examine the hinge areas of the | X | | | | | | | | spoilers and the ailerons for | | | | | | | | | contamination. | | | | | | | | | | | | | | | | F.| | Examine the flap tracks, flap inter | X | | | | | | | | connecting strut, track 4 sensor, | | | | | | | | | roller mechanisms, steady bearings and| | | | | | | | | universal joints for contamination. | | | | | |
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