(2)
 Remove the warning notice(s).

 (3)
 Remove the access platform(s).

 (4)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 1EFF : ALL 1 27-84-45Page A414 1 1 Feb 01/00R 1 1 1CES 1

 TASK 27-84-45-000-013
R Removal of the Torque Shaft 6046CM(6096CM)
 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
______________________
 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(s)
 No specific access platform 3.5 m (11 ft. 6 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-80-00-866-005 Retracting the Slats on the Ground
 27-81-42-000-001 Removal of the PPU Adaptor Plate 6048CM(6098CM)
 27-84-45-991-001 Fig. 401
 27-84-45-991-003 Fig. 403

 INTENTIONALLY BLANK

R 1 1 27-84-45Page A416 1 1 Feb 01/00 1 1 1CES 1

 3. Job Set-up
__________ (Ref. Fig. 401/TASK 27-84-45-991-001) Subtask 27-84-45-941-075
 A. Safety Precautions
 (1)
 Put the safety barriers in position.

 (2)
 Put a warning notice(s) in position to tell persons not to operate the slat controls.

 Subtask 27-84-45-860-075
 B. Aircraft Maintenance Configuration
 (1)
 Retract the slats fully (Ref. TASK 27-80-00-866-005).

 (2)
 Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is on the flap/slat control lever on panel 114VU.

 Subtask 27-84-45-865-104
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
 Subtask 27-84-45-010-062
 D. Get Access
 (1)
 Put the access platform in position below the applicable zone 522 (622).

 (2)
 Remove the PPU adaptor plate (Ref. TASK 27-81-42-000-001).

 4. Procedure
_________
 (Ref. Fig. 401/TASK 27-84-45-991-001, 403/TASK 27-84-45-991-003) Subtask 27-84-45-020-062
 A. Removal of the Torque Shaft 6046CM (6096CM)
 (1) Remove the shaft (47).

 TASK 27-84-45-400-014
 Installation of the Torque Shaft 6046CM(6096CM)
 WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING

_______
 NOTICES ARE IN POSITION.

 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

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
 No specific warning notice

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-018
 GENERAL PURPOSE ASSEMBLY PASTE (Ref. 20-31-00)

 Material No. 04-022  USA MIL-PRF-81322 GRADE 2
 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE
 (Ref. 20-31-00)
　
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