(2)
Install the applicable access panel:
-
FOR 6022CM
install 521AT
-
FOR 6072CM
install 621AT.
Subtask 27-84-45-865-083
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
Subtask 27-84-45-866-053
E. Retract the Slats
(1) Retract the slats fully (Ref. TASK 27-80-00-866-005).
Subtask 27-84-45-942-058
F. Removal of Equipment
(1)
Remove the safety barriers.
(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.
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TASK 27-84-45-000-010
Removal of the Torque Shaft 6024CM(6074CM)
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
__________________
R R 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 access platform 3.5 m (11 ft. 6 in.) 98D27504030001 2 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R 27-50-00-400-003 27-80-00-866-004 57-41-37-000-003 57-41-37-000-004 27-84-45-991-001 27-84-45-991-003 Installation of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)Extending the Slats on the Ground Removal of the Access Panel 522AT(622AT) Removal of the Pressure-Relief Panels 521AB(621AB), 521CB(621CB), 521EB(621EB), 522AB(622AB), 522CB(622CB)Fig. 401Fig. 403
3. Job Set-up__________
(Ref. Fig. 401/TASK 27-84-45-991-001)
Subtask 27-84-45-941-056
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 27-84-45-860-072
B. Aircraft Maintenance Configuration
(1) Extend the slats fully (Ref. TASK 27-80-00-866-004).
(2) Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is on the flap/slat control lever on panel 114VU.
Subtask 27-84-45-865-056
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
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Subtask 27-84-45-010-057
D. Get Access
R (1) Put the access platform in position below the zone 522(622).
R R R (2) Remove the applicable access panels (Ref. TASK 57-41-37-000-003), (Ref. TASK 57-41-37-000-004): - FOR 6024CM remove 522AT, 522AB, 521HB - FOR 6074CM remove 622AT, 622AB, 621HB.
4. Procedure_________
(Ref. Fig. 403/TASK 27-84-45-991-003)
Subtask 27-84-45-020-059
A. Removal of the Torque Shafts 6024CM (6074CM)
(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 components - on the torque shaft, outboard of the applicable components.
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