(8)
 Install the grommet (10) and put the cover (5) in position. Engage the drive (6) in the fork of the rotating mechanism (12).

 (9)
 Install the washers (8) and the screws (7).

 (10) Tighten the screws (7) and safety them with the lockwire corrosion resistant steel 0.8 mm (0.03in).
 Subtask 32-49-17-865-052
 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GV
 Subtask 32-49-17-720-050
 D. Functional Test
 (1) Do the functional test of the Tire Pressure Indicating System (Ref. TASK 32-49-00-720-001).
 5. Close-up
________ Subtask 32-49-17-860-051
 A. Put the aircraft back to its initial configuration.
 (1)
 Remove the safety barriers.

 (2)
 Remove the warning notice(s).

 1EFF : 051-099, 1 32-49-17Page 406 1 1 May 01/05 1 1 1CES 1

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

 items.

 1EFF : 051-099, 1 32-49-17Page 407 1 1 May 01/05 1 1 1CES 1

R  ROTATING MECHANISM - TPIS MLG (6GV,7GV,8GV,9GV) - REMOVAL/INSTALLATION______________________________________________________________________
 TASK 32-49-18-000-001
 Removal of the Rotating Mechanism
 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__________________
 Self Explanatory
 2. Job Set-up Information______________________ 
R  A. Fixtures, Tools, Test and Support Equipment 
R R R  -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R R  No specific No specific No specific  circuit breaker(s) safety clip(s) safety barriers warning notice 
R  B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R  32-00-00-481-001 32-48-51-000-005 32-49-18-991-001  Installation of the Safety Devices on the Landing GearsRemoval of the Fan Assy (7GS,8GS,9GS,10GS) Fig. 401 

R 1EFF : 051-099, 1 32-49-18Page 401 1 1 May 01/05 1 1 1CES 1 1EFF : 051-099, 1 32-49-18Page 402 1 1 May 01/05 1 1 1CES 1

 3. Job Set-up__________ 
R  Subtask 32-49-18-941-051 
R  A. Safety Precautions 
R  (1) Put the safety barriers in position. 
R  (2) Make sure that the ground safety locks are on the landing gear 
R  (Ref. TASK 32-00-00-481-001). 
R  (3) On the panel 400VU: 
R  - make sure that the landing-gear control-lever 6GA is in the DOWN 
R  position 
R  - put a warning notice in position to tell persons not to operate the 
R  landing gear. 
R  Subtask 32-49-18-865-050 
R  B. Open, safety and tag this(these) circuit breaker(s): 
R  -------------------------------------------------------------------------------
R  PANEL DESIGNATION IDENT. LOCATION 
R  -------------------------------------------------------------------------------
R  121VU HYDRAULIC/TIRE/PRESS 1GV M31
 Subtask 32-49-18-010-050 
R  C. Get Access
 (1) Remove the applicable brake fan assembly and mounting sleeve
 (Ref. TASK 32-48-51-000-005). 
R  4. Procedure_________ 
R  (Ref. Fig. 401/TASK 32-49-18-991-001) 
R  Subtask 32-49-18-020-050 
R  A. Removal of the Rotating Mechanism 
R  (1) Make sure that the connectors (3) and (5) are disconnected. 
R  (2) Remove the nuts (7) and the washers (6). 
R  (3) Remove the rotating mechanism (4).

R  Rotating Mechanism 
R  Figure 401/TASK 32-49-18-991-001
 1EFF :  051-099,  1  32-49-18 Page 403 
1  1  May 01/05
 1  1
 1CES  1

R  TASK 32-49-18-400-001 
R  Installation of the Rotating Mechanism 
R  WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING_______ 
R  NOTICES ARE IN POSITION. 
　
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