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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | release the tail of the circlip | | | | | | | | | from the key slot of the locking| | | | | | | | | washer, | | | | | | | | | - hold the tail of the circlip, | | | | | | | | | - carefully pull the circlip | | | | | | | | | (clockwise) until it is | | | | | | | | | released from the chamfered slot| | | | | | | | | in the nut. | | | | | | | | | (b) Remove the locking washer from the| | | | | | | | | nut. | | | | | | | | | (c) Mark the position of the nut with | | | | | | | | | a pencil line. | | | | | | | | | (d) Loosen the nut and install the | | | | | | | | | nut at the initial position and | | | | | | | | | tighten with the TUBE SPANNER | | | | | | | | | (460008834). | | | | | | | | | (e) Make sure that the torque value is| | | | | | | | | 18 m.daN (132.74 lbf. ft). | | | | | | | | | (2) Remove the bottom cardan joint | | X | | | | | | | and check of the following | | | | | A | | | | dimensions: | | | | | | | | | (Ref. TASK 32-11-16-000-001) | | | | | | | | | (Ref. TASK 05-51-31-991-002) | | | | | | | | | - dimension A between 137.917 mm | | | | | C | | | | (5.429 in.) and 137.957 mm | | | | | | | | | (5.431 in.), | | | | | | | | | - dimension B between 138 mm | | | | | B | | | | (5.433 in.) and 138.06 mm | | | | | | | | | (5.435 in.). | | | | | | | | | (3) Install the bottom cardan joint | | X | | | | | | | (Ref. TASK 32-11-16-400-001). | | | | | | -------------------------------------------------------------------------------
Subtask 05-51-31-210-051
B. Inspection of the MLG Torque Links (Ref. TASK 32-11-27-200-001)
NOTE : All the necessary inspections are visual unless specified
____ differently in the text. Operators can refer to the Non-destructive Testing Manual and use non-destructive procedures.
1EFF : ALL 1 05-51-31Page 607 1 1 May 01/04R 1 1 1CES 1
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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the MLG Torque Links | | | | | | | | | | | | | | | | A.| | Visual Inspection of the MLG torque | X | | | | | | | | links for cracks, distortion. | | | | | | | | | Do a Magnetic Particle NDT check for | | | | | | | | | cracks at the apex lug of the MLG | | | | | | | | | torque links. | | | | | | | | | Do a check of the torque link gaps | | | | | | | | | (Ref. TASK 32-11-27-200-001). | | | | | | -------------------------------------------------------------------------------
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 05-51-31-210-052
C. Inspection of the MLG Torque Link Damper (Ref. TASK 32-11-27-210-001)
NOTE : All the necessary inspections are visual unless specified
____ differently in the test. Operators can refer to the Non-destructive Testing Manual and use non-destructive test procedures.
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the MLG Torque Link | | | | | | | | | Damper | | | | | | | | | | | | | | | | A.| | Do a visual inspection of the torque | X | | | | | | | | link damper | | | | | | | | | (Ref. TASK 32-11-27-200-001). | | | | | | -------------------------------------------------------------------------------
**ON A/C 301-399,
Subtask 05-51-31-210-052-A
C. Not Applicable
R **ON A/C ALL
Subtask 05-51-31-410-050
D. Close Access
(1) Close the main landing gear doors (Ref. TASK 32-12-00-410-001).
(2) Remove the access platform(s). Subtask 05-51-31-720-050
E. Do the following tests.
(1)
Do a functional test of the extension and retraction of the main landing gear (Ref. TASK 32-31-00-720-002).
(2)
Do a functional test of the free-fall extension system (Ref. TASK 32-33-00-720-001).
5. Close-up
________ Subtask 05-51-31-586-050
A. Lowering of the Aircraft
(1)
Lower the aircraft onto its wheels (Ref. TASK 07-11-00-586-002). Subtask 05-51-31-914-051
B. Protection
(1)
Apply SEALANTS (Material No. 09-004) on the end of the cardan joint. Subtask 05-51-31-942-050
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