_______
GREASE AND ASSEMBLY PASTE DO NOT MIX.
(1)
Clean the component interface and/or the adjacent area with MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(4)
Do one of the steps that follow:
CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT.
_______
GREASE AND ASSEMBLY PASTE DO NOT MIX.
(a)
Apply a thin layer of COMMON GREASE (Material No. 04-022) to the torque shaft splines.
- or
(b)
Apply a thin layer of COMMON GREASE (Material No. 04-018) to the torque shaft splines.
Subtask 27-84-45-420-082
B. Installation of the Torque Shaft 6024CM(6074CM)
(1)
Install the shafts (48) and (50).
(2)
Install the shaft (49) and attach it with the bolts (52) and the nuts (51).
(3)
TORQUE the nuts (51) to between 1.02 and 1.24 m.daN (90.26 and 109.73 lbf.in).
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(4)
Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
-
the nuts (51)
-
the bolts (52)
-
the flanges of the shafts (48), (49) and (50).
(5)
Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (Ref. TASK 27-50-00-000-003):
-
from the torque shaft, inboard of the applicable component
-
from the torque shaft, outboard of the applicable component.
Subtask 27-84-45-220-057
C. Dimensional/Visual Checks
(Ref. Fig. 402/TASK 27-84-45-991-002)
(1) Make sure that:
-you cannot see the spline engagement groove at the movable joint
-the dimension A is a minimum of 6.5 mm (0.2559 in.) at the movable joint.
Subtask 27-84-45-865-085
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
Subtask 27-84-45-710-056
E. Test
(1) Do an operational test of the slat power-transmission system (Ref. TASK 27-84-00-710-001). Make sure that the rotation of the torque shafts does not cause damage.
5. Close-up
________
(Ref. Fig. 401/TASK 27-84-45-991-001)
Subtask 27-84-45-866-054
A. Extend the Slats
(1) Make sure that the slats are fully extended (Ref. TASK 27-80-00-866-004).
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Subtask 27-84-45-865-086
B. 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
Subtask 27-84-45-410-057
C. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
R (2) Install the applicable access panels (Ref. TASK 57-41-37-400-003), R (Ref. TASK 57-41-37-400-002):
-
FOR 6024CM
install 522AT, 522AB, 521HB
-
FOR 6074CM
install 622AT, 622AB, 621HB.
Subtask 27-84-45-865-087
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
Subtask 27-84-45-866-055
E. Retract the Slats
(1) Retract the slats fully (Ref. TASK 27-80-00-866-005).
Subtask 27-84-45-942-059
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 27-84-45-000-011
Removal of the Torque Shaft 6032CM(6082CM)
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱8(10)
