(2)
Apply SEALANTS (Material No. 09-019) to the face of the bevel gearbox
(1) which touches the support bracket.
Subtask 27-84-41-420-050
B. Installation of the Bevel Gearbox
(1)
Put the bevel gearbox (1) in position on the support bracket.
(2)
Attach the bevel gearbox (1) to the support bracket with the bolts
(16) and the washers (17).
(3)
At the bonding point continue as follows (Ref. TASK 20-28-00-912-004):
(a)
Seal bolt (16) with SEALANTS (Material No. 09-013).
(b)
Apply STRUCTURE PAINTS (Material No. 16-003) (dyed blue) to the bonding point.
(4)
Apply SPECIAL MATERIALS (Material No. 05-005) to the bolt heads (16).
(5)
Apply COMMON GREASE (Material No. 04-018) to the splines of the input universal joints (4), (10).
(6)
Engage the input universal joints (4), (10) of the bevel gearbox (1) in the bevel gearbox inputs.
(7)
Install the torque shaft 6002CM (7) as follows:
(a)
Put the torque shaft (7) in position.
(b)
Make sure that the flange holes of the torque shaft (7) are in line with the flange holes of the input universal joint (4).
(c)
If the flange holes of the torque shaft are not in line with the flange holes of the input universal joint (4), continue as follows:
(d)
Install the bolts (6) to connect the torque shaft (7) to the input universal joint (4).
(e)
Install the nuts (5) on the bolts (6).
(f)
Examine the assembly of the input universal joint (10) as follows:
1_ Remove the input universal joint (4).
2_ Turn the input universal joint (4) by the number of splines
necessary to put it in line.
3_ Install the input universal joint (4).
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 (5) 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 (6) and the nuts (5).
(8) Install the torque shaft 6004CM (13) as follows:
(a)
Put the torque shaft (13) in position.
(b)
Make sure that the flange holes of torque shaft (13) are in line with the flange holes of the input universal joint (10).
(c)
If the flange holes of the torque shaft (13) are not in line with the flange holes of the input universal joint (10), continue as follows:
(d)
Install the bolts (12) to connect the torque shaft (13) to the input universal joint (10).
(e)
Install the nuts (11) on the bolts (12).
(f)
Examine the assembly of the input universal joint (10) as follows:
1_ Remove the input universal joint (10).
2_ Turn the input universal joint (10) by the number of splines
necessary to put it in line.
3_ Install the input universal joint (10).
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 (11) 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 (12) and the nuts (11).
Subtask 27-84-41-860-051
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 27-84-41-865-052
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱7(104)
