R 1EFF : 301-399, 1 32-11-27Page 619 1 1 May 01/04 1 1 1CES 1 1EFF : ALL 1 32-11-27Page 620 1 1 May 01/04 1 1 1CES 1 Subtask 32-11-27-942-052
R R R 4_ Subtract dimension X from the maximum dimension U to give thesleeve clearance. A maximum in-service sleeve clearance of 0.25 mm (0.0098 in.) is permitted.
R R 5_ Use an internal micrometer to measure the internal diameter Vof the sleeve (3) and record the maximum dimension.
R R R 6_ Use an external micrometer 25-50 mm (1.0-2.0 in.) to measurethe external diameter N of the pin (1) and record the minimum dimension.
R R NOTE : Measure the diameter of the pin where it touches the____ bottom torque link.
R R R 7_ Subtract dimension N from the maximum dimension V to give thepin clearance. A maximum in-service pin clearance of 0.144 mm (0.0056 in.) is permitted.
R R 8_ Install the sleeves (2) and (3) and the torque-link apex pin(1) (Ref. TASK 32-11-27-400-001).
R NOTE : Refer to (Ref. CMM 321222) for corrective action.____
**ON A/C ALL
5. Close-up________
Subtask 32-11-27-410-051
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Install the applicable MLG brakes (Ref. TASK 32-42-27-400-001) and the wheels (Ref. TASK 32-41-11-400-006).
Subtask 32-11-27-860-054
B. Aircraft Maintenance Configuration
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Lower the applicable MLG off the jack (Ref. TASK 07-12-00-582-002) or lower the aircraft off jacks (Ref. TASK 07-11-00-586-002).
C. Remove the Equipment
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the safety barriers.
(3)
Remove the warning notice(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 32-11-27Page 621 1 1 May 01/04R 1 1 1CES 1
TASK 32-11-27-210-001
Detailed Inspection of the Torque-Link Damper-Assemblies
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
__________________
R R Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
No specific warning notice
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004 USA MIL-T-81533
1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
(Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
1EFF : ALL 1 32-11-27Page 622 1 1 May 01/04 1 1 1CES 1 C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-12-32-611-006 Replenishment of the MLG Torque Link Damper 32-00-00-481-001 Installation of the Safety Devices on the Landing
Gears 32-11-27-991-006 Fig. 604
3. Job Set-up
__________
Subtask 32-11-27-941-055
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.
4. Procedure
_________
(Ref. Fig. 604/TASK 32-11-27-991-006)
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