R  (j) Safety the nut (4) with the new cotter pin (5). 
R  (k) Install the sleeve (12), the new tab washer (11) and the bolt 
R  (10). 
R  (l) Use the TOOL-HOLDING (460006437) to hold the pin (8) and TORQUE 
R  the bolt (10) to between 0.83 and 1.24 m.daN (73.45 and 109.73 
R  lbf.in). 
R  (m) Bend the tabs of the tab washer (11) to safety the bolt (10). 
R  (n) Do the dimensional check on the lockstay actuator and the 
R  lockstay center-joint (Ref. TASK 32-11-00-220-003). 
R  (o) Lubricate the greasers on the actuating cylinder (7) (Ref. TASK 
R  12-22-32-640-001). 
R  (p) Apply a layer of SEALANTS (Material No. 09-016) to: 
R  - the head of the bolt (10) 
R  - the head of the pin (8) 
R  - the head of the pin (2) 
R  - the nut (4). 
R  (4) Remove the MLG spring expander tool (Ref. TASK 32-11-19-081-001). 
R  5. Close-up________ 
R  Subtask 32-00-00-865-059 
R  A. Remove the safety clip(s) and the tag(s) and close this(these) circuit 
R  breaker(s): 
R  1GA, 2GA, 52GA. 
R  Subtask 32-00-00-942-063 
R  B. Removal of Equipment 
R  (1) Make sure that the work area is clean and clear of tool(s) and other 
R  items. 
R  (2) Remove the safety barriers. 
R  (3) Remove the warning notice(s). 
R  (4) Remove the ground support and maintenance equipment, the special and 
R  standard tools and all other items.

_______________________________________________
 1. General
_______
 (Ref. Fig. 001)
 The Main Landing Gear (MLG) retracts into bays on the underside of the aircraft. The MLG bays are closed by the MLG doors (Ref. 32-12-00).
R
 2. Component Location
__________________
 The MLG (Ref. 32-11-00) is in the wing between the rear spar and gear rib 5 at zones 730 and 740. They support the aircraft on the ground and absorb loads during landing, take off and taxi.
 3. System Description
__________________
 The MLG includes these parts:

 -
a MLG shock absorber

 -
a side stay assembly which includes a lock stay

 -
a retraction actuator

 -electrical and hydraulic dressings
 -a torque-link damper.
 The MLG legs have twin wheels, each wheel has a multi-disc brake unit (Ref. 32-40-00).
 4.
 Power Supply

____________
 Not applicable

 5.
 Interface

_________
 Not applicable

 6.
 Component Description

_____________________
 Not applicable

 7.
 Operation/Control and Indicating

________________________________
 The extension and retraction system (Ref. 32-30-00):

 -extends and retracts the landing gear
 - opens and closes the related doors (Ref. 32-12-00).

 Proximity sensors on the MLG and the MLG doors give position data to the Landing Gear Control and Interface Unit (LGCIU).
 Each MLG has three doors (Ref. 32-12-00):
 1EFF : ALL 1 32-10-00Page 1 1 1 Feb 01/02 1 1 1CES 1

R  Main Landing-Gear Leg and Doors Figure 001
 1EFF : 1 1 1CES  ALL  1 111 32-10-00 Page 2 Feb 01/02

 -
a fixed fairing door that is attached to the MLG leg

 -
a hinged door that is attached to the underside of the wing

 -
a main door that is hydraulically operated and closes the section of the fuselage after the MLG has retracted or extended.

 8. BITE Test
_________
 Not applicable
 1EFF : ALL 1 32-10-00Page 3 1 1 Feb 01/98 1 1 1CES 1 MAIN GEAR - DESCRIPTION AND OPERATION

_____________________________________
 1. General
_______
 The main landing gear (MLG) has two leg assemblies. The MLG legs, each with a twin-wheel assembly, are installed in the wings. They retract inboard into bays in the fuselage. The MLG supports the aircraft on the ground and (through the shock absorbers in the legs) absorbs the loads during landing, take-off and taxiing. When an MLG is extended, a side-stay assembly prevents sideways movement of the MLG and helps keep it extended.
 2. Component Location
__________________
 -------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA
　
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