(3)
Put the warning notices in position in the cockpit to tell persons not to operate the systems.
(4)
Put the access platform in position.
4. Procedure
_________
Subtask 05-51-15-210-051
A. General
NOTE : All the necessary inspections are visual unless the text gives
____ other instructions. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive procedures.
(1) Inspection recommendations on composite parts
R (a) If you find damage (signs of impact, damaged paintwork,
R abrasions, scratches or dents) on a composite part, you must do an inspection of the related damaged area for delamination and internal damage.
(2)
If there is damage to the aircraft structure, refer to the Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures.
(3)
If you replace a component because of an inspection, you must do an operational test of the related system.
(4)
If a tire burst occurs when the landing gear is fully retracted, then only examine the items of equipment below:
-
the landing gear well,
-
the landing gear doors,
-
the landing gear assemblies,
-
the hydraulic bay compartment.
(5)
If a tire burst occurs because of emergency operation of the brakes or locking of the brakes, do an inspection (Ref. TASK 05-51-16-200-001).
Subtask 05-51-15-210-055
B. Inspection of the Fuselage (FR1 to FR34)
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Fuselage Lower Surface | | | | | | | | | | | | | | | | A.| | Examine the skin panels for | X | | | | | | | | distortion, pulled or torn fasteners | | | | | | | | | and damaged paintwork. | | | | | | R | | | If you find damage: | | | | | | | | | (1) Remove the floor panels of the | | X | | | | | | | avionics and/or forward cargo | | | | | | R | | | compartment and examine: | | | | | | | | | - the frames | | | | | | | | | - the stringers | | | | | | | | | - the cleats | | | | | | | | | - the fittings | | | | | | | | | for distortion, cracks, pulled or | | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork adjacent to the damaged | | | | | | | | | area. | | | | | | R | | | (2) Examine: | | X | | | | | | | - the components | | | | | | | | | - the pipes | | | | | | | | | - the ducts | | | | | | | | | - the electrical looms | | | | | | | | | - the control cables | | | | | | | | | - the pulleys | | | | | | | | | - the mounts | | | | | | | | | for cracks, rupture, fluid | | | | | | | | | leakage. | | | | | | | | | Also examine the condition of the | | | | | | | | | safety devices. | | | | | | | | | | | | | | | | B.| | In the nose landing-gear well, | X | | | | | | | | examine: | | | | | | | | | - the structure | | | | | | | | | - the components | | | | | | | | | - the pipes | | | | | |
-------------------------------------------------------------------------------
|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.|
| |CODE| | 1 | 2 | 3 |SIGN|FIG.|
|----|----|---------------------------------------|-----|-----|-----|----|----|
| | | - the ducts | | | | | |
| | | - the electrical looms | | | | | |
| | | - the control cables | | | | | |
| | | - the pulleys | | | | | |
| | | - the mounts | | | | | |
| | | for distortion, rupture, fluid | | | | | |
| | | leakage. | | | | | |
| | | Also examine the condition of the | | | | | |
| | | safety devices. | | | | | |
| | | | | | | | |
R | C.| | Examine: | X | | | | |
| | | - the nose landing-gear doors | | | | | |
| | | - the hinges | | | | | |
| | | - the attachments of the actuating | | | | | |
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