R (d) Apply a thin layer of COMMON GREASE (Material No. 04-022) to the bolt (6).
1EFF : ALL 1 32-31-41Page 409 1 1 Feb 01/04 1 1 1CES 1
(e) Put the rod (4) in position. CAUTION : INSTALL THE BOLTS AT THE TOP OF THE CONTROL RODS WITH
_______ THE HEADS ON THE INNER SIDE OF THE MECHANISM.
-IF NOT, THE NUTS CAN TOUCH THE CRANK LEVERS AND CAUSE DAMAGE WHEN THE MECHANISM OPERATES.
(f)
Install the bolt (6) with the heads on the inner side of the mechanism.
(g)
Install the washer (3) and the nut (2).
(h)
TORQUE the nut (2) to between 0.6 and 0.61 m.daN (53.09 and 53.98 lbf.in) and safety it with the new cotter pin (1).
(11) Apply a layer of SEALANTS (Material No. 09-013) to:
-
the head of the bolts (6) and (7)
-
the nut (2) and the washer (3)
-the nut (11) and the washer (9). Subtask 32-31-41-710-050
C. Operational Test
(1)
Do a full door close/door open cycle (Ref. TASK 32-22-00-010-001) and (Ref. TASK 32-22-00-410-001).
(2)
Make sure that the door operation is correct.
5. Close-up
________ Subtask 32-31-41-860-051
A. Put the aircraft back to its initial configuration.
(1)
Remove the access platform.
(2)
Remove the safety barriers.
(3)
Remove the warning notice(s).
(4)
Make sure that the work area is clean and clear of tool(s) and other items.
1EFF : ALL 1 32-31-41Page 410 1 1 Feb 01/04R 1 1 1CES 1
UPLOCK ASSY - MLG (2509GM,2510GM) - REMOVAL/INSTALLATION
________________________________________________________ TASK 32-31-44-000-001 Removal of the MLG Uplock Assembly 2509GM (2510GM) WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______
YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
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 : OBEY THE HYDRAULIC SAFETY PROCEDURES.
_______
1. Reason for the Job
__________________ R Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking caps
No specific blanking plugs
No specific circuit breaker(s) safety clip(s)
No specific warning notices
No specific access platform 1.5 m (4 ft. 11 in.)
No specific container 5 l (1.3208 USgal)
1EFF : ALL 1 32-31-44Page 401 1 1 May 01/99 1 1 1CES 1 B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
External Power 29-00-00-910-002 Safety Procedures of the Hydraulic System 29-10-00-864-001 Depressurize the Green Hydraulic System 29-14-00-614-001 Depressurization of the Hydraulic Reservoirs 29-23-00-860-001 Disconnection of the Isolation Coupling of the Power
Transfer Unit (PTU) R 32-00-00-860-001 Flight Configuration Precautions with Electrical R Power
32-12-00-010-001 Open the Main Gear Doors for Access
32-31-44-991-001 Fig. 401
32-31-44-991-002 Fig. 402
3. Job Set-up
__________
Subtask 32-31-44-860-050
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002)
(2)
Depressurize the Green hydraulic system (Ref. TASK 29-10-00-864-001).
Subtask 32-31-44-010-050
B. Get Access
(1) Open the applicable MLG door (Ref. TASK 32-12-00-010-001).
Subtask 32-31-44-869-050
C. Disconnection of the PTU Isolation Coupling
(1)
Depressurize the reservoir of the Green hydraulic system (Ref. TASK 29-14-00-614-001).
(2)
Disconnect the PTU isolation coupling (Ref. TASK 29-23-00-860-001).
(3)
Obey the flight configuration precautions (Ref. TASK 32-00-00-860-001).
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