B. Get Access
 (1)
 Open the doors of the nose gear (Ref. TASK 32-22-00-010-001).

 (2)
 Lift the aircraft at the forward jacking point (Ref. TASK 07-11-00-581-003).

 (3)
 Put the access platform in position.

 4. Procedure
_________ R (Ref. Fig. 602/TASK 32-21-00-991-004) Subtask 32-21-00-210-057
 A. Clearance Check
 (1)
 Push the gear leg against one of the bearings.

 (2)
 On the opposite side, measure the clearance J between the washer and the spherical bearing.

 (3)
 The clearance J must be between 0.1 and 0.2 mm.

 (4)
 The clearance J can be 1 mm. In this case you must correct it at the next C-check (Ref. TASK 32-21-11-000-002) (Ref. TASK 32-21-11-400-002).

 (5)
 If the clearance J is more than 1 mm, you must correct it immediately (Ref. TASK 32-21-11-000-002) (Ref. TASK 32-21-11-400-002).

 5. Close-up
________
 Subtask 32-21-00-942-059

 A. Aircraft Maintenance Configuration
 (1)
 Lower the aircraft on its wheels (Ref. TASK 07-11-00-586-001).

 (2)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (3)
 Remove the access platform(s).

 1EFF : ALL 1 32-21-00Page 614 1 1 May 01/05 1 1 1CES 1

R  Connection to the Structure Figure 602/TASK 32-21-00-991-004
 1EFF : 1 1 1CES  ALL  1 111 32-21-00 Page 615 May 01/05

 (4) Remove the ground support and maintenance equipment, the special and

 standard tools and all other items. Subtask 32-21-00-410-054
 B. Close the door of the nose gear (Ref. TASK 32-22-00-410-001).
 1EFF : ALL 1 32-21-00Page 616 1 1 May 01/05R 1 1 1CES 1

 TASK 32-21-00-200-005
 Detailed Inspection/Check of the NLG
 1. Reason for the Job
__________________
 Detailed Inspection/Check of the NLG after the aircraft goes off the runway/taxiway and the NLG wheels sank into the ground and/or the NLG found an obstacle on its path.
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific warning notice(s)
 No specific access platform 2.06 m (6 ft. 9 in.)
 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
05-51-24-200-001 Inspection after Leaving Runway or Taxiway 07-11-00-581-003 Lifting of the Aircraft at Forward Jacking Point, MLG Wheels on the Ground 07-11-00-586-001 Lowering of the Aircraft at Forward Jacking Point, MLG Wheels on the Ground 29-10-00-864-001 Depressurize the Green Hydraulic System
R 29-10-00-864-002 Depressurize the Yellow Hydraulic System 32-21-27-000-001 Removal of the Torque Link Assy 32-21-27-400-001 Installation of the Torque Link Assy 32-22-00-010-001 Nose Gear Doors - Ground Doors Opening 32-22-00-410-001 Nose Gear Doors - Ground Doors Closing 32-51-00-720-003 Functional Test of the Nose Wheel Steering with the Handwheel. 32-51-00-720-004 Functional Test of the Nose Wheel Steering with the Pedals. 32-51-51-000-001 Removal of the Nose Wheel Steering Servo-Control (6GC)
 1EFF : ALL 1 32-21-00Page 617 1 1 Aug 01/05 1 1 1CES 1

 3. Job Set-up
__________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 Subtask 32-21-00-860-052
 A. Aircraft Maintenance Configuration
 (1)
 make sure that you read the instructions given in the Inspection after the Aircraft goes off the runway/taxiway (Ref. TASK 05-51-24-200-001) before you do this task.

 (2)
 On the panel 400VU, make sure that the landing gear control lever is in the DOWN position.

 (3)
 On the panel 110VU, make sure that the free-fall control handle is in the usual position.

 (4)
 On the nose gear leg, on the electrical box (5CG), make sure that the towing lever is in the towing position (disengaged position).

 (5)
 Lift the aircraft at the forward jacking point (Ref. TASK 07-11-00-581-003).

 NOTE : During lifting, make sure that extension of the shock absorber
____
 is smooth and full.

 (6)
 Make sure that the Green hydraulic system is depressurized (Ref. TASK 29-10-00-864-001).
　
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