(2)
If the torque link damper is at the REFILL level position:
-make sure that the MLG safety locks are in position (Ref. TASK 32-00-00-481-001)
-fill the damper (Ref. TASK 12-12-32-611-006). Subtask 32-11-11-942-052
B. Removal of 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.
R 1EFF : ALL 1 32-11-11Page 603 1 1 May 01/05 1 1 1CES 1
Torque Link Damper Figure 601/TASK 32-11-11-991-010
R 1EFF : 1 1 1CES ALL 1 111 32-11-11 Page 604 May 01/00
R **ON A/C 001-049, 051-061, 101-105, 201-203,
TASK 32-11-11-200-003
Detailed Inspection of Forward Pintle Pin Lock Bolt Installation
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: 321111-06
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
No specific safety barriers
No specific warning notice
No specific access platform 3 m (9 ft. 10 in.)
R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft)
R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 32-11-11Page 605 1 1 May 01/05 1 1 1CES 1 B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-002 USA MIL-S-8802 TYPE I CLASS B
FUEL TANK SEALANTPOLYSULFID(NO LONGER AVAILABLE
(Ref. 20-31-00)
R Material No. 09-025 USA MIL-PRF-81733 CORROSION INHIBITING SEALANT SPRAYABLE (Ref. 20-31-00)
Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
Material No. 16-016 C Z-12.383
EXTERNAL DECORATION PAINT (Ref. 20-31-00)
Material No. 16-021 F ASNB70720
FLEXIBLE POLYURETHANE (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
4 cotter pin 32-11-05 02 -130 4 cotter pin 32-11-05 02A-130 7 washer 32-11-11 66A-100 7 washer 32-11-11 66D-100 7 washer 32-11-11 66F-100
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-22-32-640-001 Lubrication of the MLG and Doors 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power
29-10-00-863-001 Pressurize the Green Hydraulic System
29-10-00-863-002 Pressurize the Yellow Hydraulic System
29-10-00-864-001 Depressurize the Green Hydraulic System
29-10-00-864-002 Depressurize the Yellow Hydraulic System
29-14-00-614-001 Depressurization of the Hydraulic Reservoirs
R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 32-11-11Page 606 1 1 May 01/05 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-14-00-614-002 29-23-00-860-001 29-23-00-860-002 32-00-00-481-001 32-00-00-860-001 32-00-00-860-002 32-11-11-000-001
32-11-11-400-001 CMM 200000 32-11-11-991-024
R **ON A/C 051-052,
R 32-11-11-991-025-A Pressurization of the Hydraulic Reservoirs through the Ground ConnectorDisconnection of the Isolation Coupling of the Power Transfer Unit (PTU)Connection of the Isolation Coupling of the Power Transfer Unit (PTU)Installation of the Safety Devices on the Landing GearsFlight Configuration Precautions with Electrical PowerGround Configuration after Flight Configuration with Electrical PowerRemoval of the MLG Leg AssemblyInstallation of the MLG Leg Assembly(for corrective action)Fig. 602
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