(2)
Examine the MLG main fitting bushes for damage to the protective finish, corrosion and/or cracks at the following:
-
the aircraft attachment lugs
-
the retraction actuator attachment lug
-
the cardan pin lugs
-
the upper torque link attachment lug
-
the upper slave link attachment lug
-
the upper diaphragm and lower bearing attachment pins.
(3)
Examine the drain hole at the upper diaphragm retaining pin for corrosion.
1EFF : ALL 1 32-11-00Page 654 1 1 Aug 01/05 1 1 1CES 1
MLG Main Fitting Inspection Area
Figure 610/TASK 32-11-00-991-029
R 1EFF : 001-003, 051-052, 1 32-11-00Page 655 1 1 May 01/05 1 1 1CES 1
MLG Main Fitting Inspection Area
Figure 610A/TASK 32-11-00-991-029-A
R 1EFF : 004-049, 053-099, 101-149, 151-199, 1 32-11-00Page 656 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1
(4) If you find damage or corrosion, refer to (Ref. CMM 321133) for repair procedures.
R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 401-499,
Subtask 32-11-00-200-051-A
A. Detailed Inspection of MLG, Main Fitting
(1)
Preparation for inspection:
(a) Use a clean MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026) to clean the areas to be examined.
(2)
Examine the MLG main fitting bushes for damage to the protective finish, corrosion and/or cracks at the following:
-
the aircraft attachment lugs
-
the retraction actuator attachment lug
-
the cardan pin lugs
-
the upper torque link attachment lug
-
the upper slave link attachment lug
-
the upper diaphragm and lower bearing attachment pins.
(3)
Examine the drain hole at the upper diaphragm retaining pin for corrosion.
(4)
If you find damage or corrosion, refer to (Ref. CMM 321225) for repair procedures.
**ON A/C 301-399,
Subtask 32-11-00-200-051-B
A. Detailed Inspection of MLG, Main Fitting
(1) Preparation for inspection:
(a) Use a clean MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026) to clean the areas to be examined.
1EFF : ALL 1 32-11-00Page 657 1 1 Aug 01/05 1 1 1CES 1
(2)
Examine the MLG main fitting bushes for damage to the protective finish, corrosion and/or cracks at the following:
-
the aircraft attachment lugs
-
the retraction actuator attachment lug
-
the cardan pin lugs
-
the upper torque link attachment lug
-
the upper slave link attachment lug
-
the upper diaphragm and lower bearing retaining pins.
(3)
Examine the drain hole at the upper diaphragm retaining pin for corrosion.
(4)
If you find damage or corrosion, refer to (Ref. CMM 321222) for repair procedures.
**ON A/C ALL
5. Close-up
________ Subtask 32-11-00-410-068
A. Close Access
(1) Remove the access platform(s).
(2) Close the MLG doors (Ref. TASK 32-12-00-410-001). Subtask 32-11-00-942-080
B. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Remove the warning notice(s).
(3)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 32-11-00Page 658 1 1 Feb 01/05R 1 1 1CES 1
TASK 32-11-00-200-010
Detailed Inspection of MLG, Sliding Tube at Brake Attachment Flange, and other Interference Fit Bushes
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
1. Reason for the Job
__________________
Refer to the MPD TASK: 321137-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
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