(23)
Engage the input universal joint (2) of the bevel gearbox (1) in the bevel gearbox input.
(24)
Install the torque shaft 6012CM (6062CM) (5) as follows:
(a)
Put the torque shaft (5) in position.
(b)
Make sure that the flange holes of the torque shaft (5) are in line with the flange holes of the input universal joint (2).
(c)
If the flange holes of the torque shaft (5) are not in line with the flange holes of the input universal joint (2), continue as follows:
1 Remove the input universal joint (2).
_ 2 Turn the input universal joint (2) by the number of splines
_ necessary to put it in line.
3 Install the input universal joint (2).
_
(d)
Install the bolts (3) to connect the torque shaft (5) to the input universal joint (2).
(e)
Install the nuts (4) on the bolts (3).
(f) Examine the assembly of the input universal joint (2) as follows:
(g)
If you can see the indicator groove continue as follows: 1 Measure all the related torque shafts, universal joints and
_ gearboxes and refer to LIEBHERR technical data.
(h)
TORQUE the nuts (4) to between 1.02 and 1.24 m.daN (90.26 and
1_ Measure dimension X. Dimension X must be a minimum of 6.5 mm
(0.2559 in.).
2_ Make sure that you can not see the indicator groove.
109.73 lbf.in).
(i) Apply SPECIAL MATERIALS (Material No. 05-005) to the bolts (3) and the nuts (4).
Subtask 27-84-43-860-051
C. Preparation for the Test
(1)
Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT FOR 6059CM, 6061CM from the right slat transmission. FOR 6009CM, 6011CM from the left slat transmission.
(2)
Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (Ref. TASK 27-00-00-080-002) from the slat/flap control lever.
(3)
Remove the warning notice(s).
(4)
Make sure that the work area is clean and clear of tool(s) and other items.
Subtask 27-84-43-865-052
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
Subtask 27-84-43-710-050
E. Do the operational test of the slat system (Ref. TASK 27-84-00-710-001).
5. Close-up
________ Subtask 27-84-43-410-050
A. Close Access
(1)
Install the applicable access panels: FOR 6009CM, 6011CM install 191BT, 191CT. FOR 6059CM, 6061CM install 192BT, 192CT.
(2)
Remove the access platform(s).
STEADY BEARING ASSY - TRANSMISSION (6007CM,6017CM,6019CM,6021CM,6023CM,6025CM,
______________________________________________________________________________ 6031CM,6057CM,6067CM,6069CM,6071CM,6073CM,6075CM...) - REMOVAL/INSTALLATION
___________________________________________________________________________
TASK 27-84-44-000-001
Removal of the Steady Bearing FIN 6007CM(6057CM)
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 warning notice(s)
No specific access platform 3.5 m (11 ft. 6 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-84-45-000-002 Removal of the Torque Shafts 6006CM(6056CM) 32-12-00-010-001 Open the Main Gear Doors for Access 27-84-44-991-001 Fig. 401 FOR FIN 6057CM 27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
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