B. Safety Precautions
(1)
Make sure that the safety devices are installed on the landing gear (Ref. TASK 32-00-00-481-001).
(2)
Put a warning notice in the cockpit to tell persons not to operate the aircraft systems.
Subtask 05-51-12-010-051
C. Get Access
(1)
Put an access platform in position.
(2)
Open all the access panels in the main landing-gear well.
(3)
Open and/or remove the access panels in the wing trailing-edge falsework between rib1 and rib8.
Subtask 05-51-12-010-050
D. Get Access
(1)
Open the main gear doors and install the safety devices (Ref. TASK 32-12-00-010-001).
(2)
Open the nose gear doors and install the safety devices (Ref. TASK 32-22-00-010-001).
Subtask 05-51-12-866-050
E. Extension of the Flaps
(1) Fully extend the flaps (Ref. TASK 27-50-00-866-008).
4. Procedure
_________ Subtask 05-51-12-869-051
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 test procedures.
1EFF : ALL 1 05-51-12Page 603 1 1 Nov 01/00R 1 1 1CES 1
Subtask 05-51-12-210-051
B. Inspection of the Fuselage and the Nose Landing Gear Well
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----|
R |1. | | Fuselage | | | | | | | | | | | | | | | | A.| | Examine the external fuselage and the | X | | | | | | | | skin panels for distorsion, cracks, | | | | | | | | | pulled or torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | | | | | | | | | | If you find damage: | | | | | | | | | - internally examine the frames, the| | X | | | | | | | stringers and the cleats for | | | | | | | | | buckling, cracks and damaged | | | | | | | | | paintwork. | | | | | | | | | | | | | | | |2. | | NLG Well | | | | | | | | | | | | | | | | A.| | Examine: | X | | | | | | | | - the hinge fittings of the nose gear,| | | | | | | | | - the attach fittings of the actuating| | | | | | | | | cylinder, | | | | | | | | | - the drag strut and the attach | | | | | | | | | fittings, | | | | | | | | | for distortion, cracks and damaged | | | | | | | | | paintwork. | | | | | | | | | | | | | | | | B.| | Examine the gear well roof and the | X | | | | | | | | forward, aft and side wall structure | | | | | | | | | for distortion, cracks and damaged | | | | | | | | | paintwork. | | | | | | | | | If you find damage: | | | | | | | | | - in the avionics compartment, examine| | X | | | | | | | the nose-gear well roof and wall | | | | | | | | | structure for distortion, cracks and| | | | | | | | | damaged paintwork. | | | | | | | | | | | | | | | | C.| | Examine all the components, the hoses,| X | | | | | | | | the pipes, the electrical looms, the | | | | | | | | | control rods, the bellcranks and | | | | | | | | | their mounts for: | | | | | |
-------------------------------------------------------------------------------
|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----|
| | | - distortion,cracks,rupture and oil | | | | | | | | | leakage. | | | | | | -------------------------------------------------------------------------------
Subtask 05-51-12-210-053
R C. Inspection of the Belly Fairing and MLG Wells (Ref. Fig. 601/TASK 05-51-12-991-001, 602/TASK 05-51-12-991-002, 603/TASK 05-51-12-991-003)
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----|
R |1. | | Belly Fairing | | | | | | | | | | | | | | | | A.| | Examine the aft panels of the belly | X | | | | | | | | fairing for loose fasteners, cracked | | | | | | | | | or flaking paint and make sure that | | | | | | | | | the panels are correctly attached. | | | | | | | | | | | | | | | | B.| | Make sure that the belly fairing rods | X | | | | | | | | are correctly attached. | | | | | | | | | | | | | | | | C.| | Externally examine the cover of the | X | | | | | | | | keel beam for cracked or flaking paint| | | | | | | | | and delamination. Make sure that it is| | | | | | | | | correctly attached. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the panels and internally | | X | | | | | | | examine the structure of the belly| | | | | | | | | fairing for buckling, cracks and | | | | | | | | | damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (a) Remove all the panels of the belly| | | X | | | | | | fairing and examine the fuselage | | | | | | | | | skin for: | | | | | | | | | - buckling, | | | | | | | | | - loose rivets, | | | | | | | | | - cracked or flaking paint. | | | | | | | | | (b) Examine the pipes, the ducts, the | | | X | | |
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