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27-84-45Page 460
1 1 Feb 01/00 1 1 1CES 1 TASK 27-84-45-000-007

 Removal of the Torque Shafts 6016CM(6066CM)/6020CM(6070CM)/6026CM(6076CM)/ 6030CM(6080CM)
 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 No specific adjustable access platform 3.5 m (11 ft. 6 in.) 98D27504030001 2 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
 Slats (98D27504030001) 27-80-00-866-005 Retracting the Slats on the Ground 27-84-45-991-001 Fig. 401 27-84-45-991-002 Fig. 402
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 3. Job Set-up
__________ (Ref. Fig. 401/TASK 27-84-45-991-001) Subtask 27-84-45-941-055
 A. Safety Precautions
 (1)
 Put the safety barriers in position.

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

 Subtask 27-84-45-860-070
 B. Aircraft Maintenance Configuration
 (1)
 Retract the slats fully (Ref. TASK 27-80-00-866-005).

 (2)
 Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) is on the flap/slat control lever on panel 114VU.

 Subtask 27-84-45-865-055
 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 27-84-45-010-055
 D. Get Access
 (1)
 Put the adjustable access platform in position below the applicable access panel.

 (2)
 Remove the applicable access panel:

 -
FOR 6016CM
 remove 521EB

 -
FOR 6020CM
 remove 521EB

 -
FOR 6026CM
 remove 522AB

 -
FOR 6030CM

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 remove 522CB
 -
FOR 6066CM
 remove 621EB

 -
FOR 6070CM
 remove 621EB

 -
FOR 6076CM
 remove 622AB

 -
FOR 6080CM
 remove 622CB.

 4. Procedure
_________
 (Ref. Fig. 402/TASK 27-84-45-991-002)
 Subtask 27-84-45-020-056
 A. Removal of the Torque Shafts
 (1)
 Install a LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) (Ref. TASK 27-50-00-400-003): - on the torque shaft, inboard of the applicable component - on the torque shaft, outboard of the applicable component.

 (2)
 Remove the nuts (10), the bolts (11) and then the shaft (9).

 (3)
 Remove the universal joint (8).

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 TASK 27-84-45-400-008
 Installation of the Torque Shafts 6016CM(6066CM)/6020CM(6070CM)/6026CM
 (6076CM)/6030CM(6080CM)

 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
__________________
　
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