C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
07-11-00-581-001 Lifting for Aircraft Maintenance Operations
07-11-00-586-002 Lowering of the Aircraft for Maintenance Operations
32-00-00-481-001 Installation of the Safety Devices on the Landing
Gears
32-00-00-860-001 Flight Configuration Precautions with Electrical
Power
32-12-00-010-001 Open the Main Gear Doors for Access
32-12-00-410-001 Close the Main Gear Doors after Access
32-41-11-000-006 Removal of the MLG Wheel
(2649GM,2650GM,2651GM,2652GM)
32-41-11-400-006 Installation of the MLG Wheel
(2649GM,2650GM,2651GM,2652GM)
32-42-27-000-001 Removal of the Brake (2641GM,2642GM,2643GM,2644GM)
32-42-27-400-001 Installation of the Brake
(2641GM,2642GM,2643GM,2644GM)
CMM 321133 (for corrective action)
CMM 321222 (for corrective action)
CMM 321225 (for corrective action)
32-11-00-991-030 Fig. 611
3. Job Set-up__________
Subtask 32-11-00-941-080
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Make sure that the ground safety locks are on the landing gear (Ref. TASK 32-00-00-481-001).
(3)
On the panel 400VU:
-make sure that the landing-gear control-lever 6GA is in the DOWN position
-put a warning notice in position to tell persons not to operate the landing gear controls.
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Subtask 32-11-00-860-060
B. Aircraft Maintenance Configuration
(1)
Open the main gear (MLG) doors (Ref. TASK 32-12-00-010-001).
(2)
Make sure the GROUND LOCK SLEEVE (460005835) is on the applicable MLG door actuator.
(3)
Do the flight configuration precautions procedure (Ref. TASK 32-00-00-860-001).
Subtask 32-11-00-581-051
C. Lifting of the Aircraft
(1) Lift the aircraft on jacks (Ref. TASK 07-11-00-581-001). Subtask 32-11-00-010-070
D. Get Access
(1)
Put the access platform in position.
(2)
Remove the wheels (Ref. TASK 32-41-11-000-006).
(3)
Remove the brakes (Ref. TASK 32-42-27-000-001).
(4)
Make sure that the warning notices are in position to stop operation of the landing gear and the brakes.
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4. Procedure
_________
(Ref. Fig. 611/TASK 32-11-00-991-030)
**ON A/C 001-003, 051-052,
Subtask 32-11-00-200-052
A. Detailed Inspection of MLG, Sliding Tube at Brake Attachment Flange, and other Interference Fit Bushes
(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 area to be examined.
(2)
Examine the brake attachment flanges for the following:
-damage to the protective finish
-corrosion or cracks on the installed bushes.
(3)
Examine the sliding tube bushes for damage to the protective finish, corrosion and/or cracks at the following locations:
-
the lower torque link attachment lug
-
the lower slave link attachment lug
-
the towing/debogging lug
-
the jacking dome.
(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 32-11-00-200-052-A
A. Detailed Inspection of MLG, Sliding Tube at Brake Attachment Flange, and other Interference Fit Bushes
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