(4)
Engage the right input universal joint (15) of tee gearbox (1) in the right input of the tee gearbox (1).
(5)
Put the tee gearbox (1) in position on the support bracket.
(6)
Attach the tee gearbox (1) to the support bracket with the bolts (18) and the washers (19).
(7)
At the bonding point continue as follows (Ref. TASK 20-28-00-912-004):
(a)
Seal bolt (18) with SEALANTS (Material No. 09-013).
(b)
Apply STRUCTURE PAINTS (Material No. 16-003) (dyed blue) to the bonding point.
(8)
Apply SPECIAL MATERIALS (Material No. 05-005) to the bolt heads (18).
(9)
Examine the assembly of the input universal joint (15) as follows:
(a)
Measure dimension X. Dimension X must be a minimum of 6.5 mm (0.2559 in.).
(b)
Make sure that you can not see the indicator groove.
(10)
If you can see the indictor groove continue as follows:
(a) Measure all the related torque shafts, universal joints and gearboxes and refer to LIEBHERR technical data.
(11)
Apply COMMON GREASE (Material No. 04-018) to the splines of the left input universal joint (22).
(12)
Engage the left input universal joint (22) of tee gearbox (1) in the left input of the tee gearbox.
(13)
Install the torque shaft 6006CM (26) as follows:
(a)
Put the torque shaft (26) in position.
(b)
Make sure that the flange holes of the torque shaft (26) are in line with the flange holes of the input universal joint (22).
(c)
If the flange holes of the torque shaft (26) are not in line with the flange holes of the input universal joint (22), continue as follows:
(d)
Install the bolts (8) to connect the torque shaft (26) to the input universal joint (22).
(e)
Install the nuts (7) on the bolts (8).
(f)
Examine the assembly of the input universal joint (22) as follows:
1_ Remove the input universal joint (22).
2_ Turn the input universal joint (22) by the number of splines
necessary to put it in line.
3_ Install the input universal joint (22).
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.
_
(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 (8) to between 1.02 and 1.24 m.daN (90.26 and
109.73 lbf.in).
(i) Apply SPECIAL MATERIALS (Material No. 05-005) to the bolts (8) and the nuts (7).
Subtask 27-84-42-860-051
C. Preparation for the Test
(1)
Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT from the right slat transmission.
(2)
Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT from the left slat transmission.
(3)
Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (Ref. TASK 27-00-00-080-002) from the slat/flap control lever.
(4)
Remove the warning notice(s).
(5)
Make sure that the work area is clean and clear of tool(s) and other items.
Subtask 27-84-42-865-052
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
Subtask 27-84-42-710-050
E. Do the operational test of the slat system, (Ref. TASK 27-84-00-710-001).
5. Close-up
________
(Ref. Fig. 401/TASK 27-84-42-991-001) Subtask 27-84-42-410-050
A. Close Access
(1)
Install the bellows (3) as follows:
(a) Install the V-clamp (4), the bellows (3) and the clamp (2).
(2)
TORQUE the V-clamp (4) to 0.55 m.daN (48.67 lbf.in).
(a) TORQUE the clamp (2) to 0.28 m.daN (24.77 lbf.in).
(3)
Install the access panel 191BB.
(4)
Make sure that the work area is clean and clear of tool(s) and other items.
(5) Remove the access platform(s). Subtask 27-84-42-865-053
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 21HH, 22HH, 23HH, 24HH
GEARBOX - BEVEL 63.5 DEG (6009CM,6011CM,6059CM,6061CM) - REMOVAL/INSTALLATION
_____________________________________________________________________________ TASK 27-84-43-000-001 Removal of the Bevel Gearbox 63.5 6009CM,6011CM (6059CM,6061CM) WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱7(108)
