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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | torn fasteners. | | | | | | | | | (2) Internally examine the lower part | | X | | | | | | | of the pressure bulkhead FR70, on | | | | | | | | | the forward and the aft face, in | | | | | | | | | the area below the | | | | | | | | | passenger-compartment floor level,| | | | | | | | | between the L STGR28 and R STGR28,| | | | | | | | | the pressure dome, the frame | | | | | | | | | segment and the vertical cross | | | | | | | | | beam at the aircraft center line | | | | | | | | | for: | | | | | | | | | - distorsion, cracks and dents. | | | | | | | | | | | | | | | |2. | | APU Air Intake and Tail Cone | | | | | | | | | Attachment Fittings | | | | | | | | | | | | | | | | A.| | Examine the APU diverter, intake flap,| X | | | | | | | | intake nose and drain mast for | | | | | | | | | distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork | | | | | | | | | (Ref. TASK 49-16-00-210-001). | | | | | | | | | If you find damage: | | | | | | | | | (1) Internally examine the diverter | | X | | | | | | | system, the ball bearing control | | | | | | | | | and the flap actuator for | | | | | | | | | distortion. | | | | | | | | | Make sure that they are correctly | | | | | | | | | attached. | | | | | | -------------------------------------------------------------------------------
R **ON A/C 106-149, 211-299, 301-399, 401-499,
Subtask 05-51-21-210-050-B
A. Inspection of the Tail Area (Ref. TASK 49-16-00-210-002)
NOTE : You must do this inspection if:
____
-
the tail hits the runway during the take-off,
-
the tail hits the runway during the landing.
NOTE : All inspections are visual unless the text gives other
____
instructions.
R 1EFF : 051-099, 106-149, 211-299, 301-399, 1 05-51-21Page 606 1401-499, 1Aug 01/05 1 1 1CES 1 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Fuselage | | | | | | | | | | | | | | | | A.| | Examine the skin panels, the splices | X | | | | | | | | and the rivets for distortion, cracks,| | | | | | | | | pulled or torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Internally examine the frames, the| | X | | | | | | | cleats and the stringers for | | | | | | | | | distortion, cracks, pulled and | | | | | | | | | torn fasteners. | | | | | | | | | (2) Internally examine the lower part | | X | | | | | | | of the pressure bulkhead FR70, on | | | | | | | | | the forward and the aft face, in | | | | | | | | | the area below the | | | | | | | | | passenger-compartment floor level,| | | | | | | | | between the L STGR28 and R STGR28,| | | | | | | | | the pressure dome, the frame | | | | | | | | | segment and the vertical cross | | | | | | | | | beam at the aircraft center line | | | | | | | | | for: | | | | | | | | | - distorsion, cracks and dents. | | | | | | | | | | | | | | | |2. | | APU Air Intake and Tail Cone | | | | | | | | | Attachment Fittings | | | | | | | | | | | | | | | | A.| | Examine the APU diverter, intake flap,| X | | | | | | | | intake nose and drain mast for | | | | | | | | | distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork | | | | | | | | | (Ref. TASK 49-16-00-210-002). | | | | | | | | | If you find damage: | | | | | | | | | (1) Internally examine the diverter | | X | | | | | | | system, the ball bearing control | | | | | | | | | and the flap actuator for | | | | | | | | | distortion. | | | | | | | | | Make sure that they are correctly | | | | | | | | | attached. | | | | | | -------------------------------------------------------------------------------
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 05-51-21Page 607 1 1 Aug 01/05 1 1 1CES 1
**ON A/C ALL
5. Close-up
________ Subtask 05-51-21-410-050
A. Close Access
(1) CLOSE THE ACCESS DOORS 312AR, 314AR, 315AL, 316AR. Subtask 05-51-21-942-050
B. Put the aircraft back to the serviceable condition.
(1)
Remove the access platform(s).
(2)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
INSPECTION AFTER NLG TOWING OVERLOAD OR OVERRUN - INSPECTION/CHECK__________________________________________________________________
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