Subtask 27-84-44-942-051
B. 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.
TASK 27-84-44-000-003
Removal of the Steady Bearing FIN 6021CM(6071CM)
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 -------------------------------------------------------------------------------
27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)
27-84-45-000-007 Removal of the Torque Shafts 6016CM(6066CM)/6020CM(6070CM)/6026CM(6076CM)/ 6030CM(6080CM)
27-84-44-991-001 Fig. 401 27-84-44-991-002 Fig. 402
3. Job Set-up
__________
(Ref. Fig. 401/TASK 27-84-44-991-001, 402/TASK 27-84-44-991-002)
Subtask 27-84-44-941-060
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put a warning notice(s) in the cockpit to tell persons not to operate the slat controls.
(3)
Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) is on the flap/slat control lever.
Subtask 27-84-44-865-066
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
R 49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
Subtask 27-84-44-010-050
C. Get Access
(1)
Put the access platform in position below the applicable access panel.
(2)
Remove the applicable access panel:
-
FOR 6021CM
remove 521GB
-
FOR 6071CM
remove 621GB.
(3)
Remove the applicable torque shaft (26) (Ref. TASK 27-84-45-000-007):
-
FOR 6021CM
remove the torque shaft FIN 6020CM
-
FOR 6071CM
remove the torque shaft FIN 6070CM.
(4)
Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) is on the applicable torque shaft (Ref. TASK 27-50-00-400-003).
4. Procedure
_________
(Ref. Fig. 402/TASK 27-84-44-991-002) Subtask 27-84-44-020-052
A. Removal of the Steady Bearing FIN 6021CM (6071CM)
(1)
Remove the nuts (24) and the bolts (21).
(2)
Remove the steady bearing (22) from the torque shaft (25) and the nose rib (23).
TASK 27-84-44-400-003
Installation of the Steady Bearing FIN 6021CM(6071CM)
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 -------------------------------------------------------------------------------
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