(2)
Dry the parts: WARNING : USE A PROTECTIVE EYE SHIELD/GOGGLES WHEN YOU USE COMPRESSED
_______ AIR. DEBRIS AND/OR HIGH PRESSURE AIR CAN DAMAGE YOUR EYES.
WARNING : DO NOT PUT COMPRESSED GAS IN CONTACT WITH YOUR SKIN. THE
_______ GAS CAN GO THROUGH THE SKIN AND MAKE BUBBLES IN THE BLOOD. THIS CONDITION CAN KILL YOU.
(a) Use compressed air to dry the cleaned areas.
(3)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(4)
Do an inspection of the component interface and/or the adjacent area.
(5)
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.
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Subtask 27-54-45-420-061
B. Installation of the Torque Shaft 6228CM(6278CM)
(1)
Put the retaining ring (87) temporarily in position on the shaft of the universal joint (88).
(2)
Install the universal joint (88) and align the pin hole with the flange of the steady bearing.
(3)
Install the torque shaft (86) and attach it with the pin (85) and the retaining ring (87).
(4)
Install the torque shaft (84) and attach it with the bolts (90) and the nuts (89).
(5)
TORQUE the nuts (89) to between 1.02 and 1.24 m.daN (90.26 and 109.73 lbf.in).
(6)
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.
(7)
Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (Ref. TASK 27-50-00-000-003).
Subtask 27-54-45-916-059
C. Application of Special Materials
(1) Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
-
the nuts (89)
-
the bolts (90)
-
the flanges of the torque shafts (84) and (86).
Subtask 27-54-45-865-093
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
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Subtask 27-54-45-710-061
E. Operational Test of the Flap System
(1)
Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever.
(2)
Retract the flaps fully (Ref. TASK 27-50-00-866-009).
(3)
Do an operational test of the flap system (Ref. TASK 27-54-00-710-001). Make sure that the operation of the torque shafts is satisfactory.
5. Close-up
________
**ON A/C 001-049, 051-061, 101-103, 201-203,
(Ref. Fig. 401/TASK 27-54-45-991-001) R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
(Ref. Fig. 401A/TASK 27-54-45-991-001-A)
**ON A/C ALL
Subtask 27-54-45-410-059
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the COLLAR-SAFETY, SPOILER from the piston rod of the servo-control.
(3)
Put the applicable spoiler back to the 'O' (Operation) position (Ref. TASK 27-60-00-866-002).
(4)
On the servo-control, make sure that the pointer on the hex-head is opposite the letter 'O' (Operation) on the housing.
(5)
Install the applicable access panel:
-
FOR 6228CM
install 575DB, 575EB
-
FOR 6278CM
install 675DB, 675EB.
Subtask 27-54-45-942-061
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.
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TASK 27-54-45-000-013
Removal of the Torque Shaft 6232CM(6282CM)
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
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本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵5(59)
