(e)
TORQUE the nuts (7) to between 1.02 and 1.24 m.daN (90.26 and
109.73 lbf.in).
(f)
Apply SPECIAL MATERIALS (Material No. 05-005) to the bolts (6) or
(14)
as assembled and the nuts (7).
(10)
Install the torque shaft 6202CM (6252CM) (9) as follows:
(a)
Put the torque shaft (9) in position.
(b)
Make sure that the flange holes of the torque shaft (9) are in line with the flange holes of the input universal joint (5).
(11)
If the flange holes of the torque shaft (9) are not in line with the flange holes of the input universal joint (5), continue as follows:
(a)
Remove the torque shaft (9) complete with the attached input universal joint from the input of the Power Control Unit (PCU).
(b)
Turn the torque shaft (9) as necessary to put it in line.
1EFF : ALL 1 27-54-41Page 413 1 1 May 01/04R 1 1 1CES 1
(c) Install the torque shaft (9) complete with the attached input universal joint in the input of the PCU.
(12)
Install the bolts (6) and the nuts (7) to attach the torque shaft (9) to the input universal joint (5).
(13)
Examine the assembly of the input universal joint (5) 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.
(14)
If you can see the indicator groove continue as follows:
(a) Measure all the related torque shafts, universal joints and gearboxes and refer to LIEBHERR technical data.
(15)
TORQUE the nuts (7) to between 1.02 and 1.24 m.daN (90.26 and 109.73 lbf.in).
(16)
Apply SPECIAL MATERIALS (Material No. 05-005) to the bolts (6) and the nuts (7).
Subtask 27-54-41-860-052
C. Preparation for the Test
(1)
Remove the PIN RIGGING-FLAPS from the flap transmission,
FOR 6203CM
from the left flap transmission.
FOR 6253CM
from the right flap 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). Subtask 27-54-41-865-052
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
Subtask 27-54-41-710-050
E. Do the operational test of the flap system (Ref. TASK 27-54-00-710-001).
5. Close-up
________ Subtask 27-54-41-410-050
A. Close Access
(1)
Remove the access platform(s).
(2)
Close the main doors of the main gear (Ref. TASK 32-12-00-410-001).
STEADY BEARING ASSY (6207CM,6213CM,6215CM,6219CM,6223CM,6225CM,6229CM,6231CM,_____________________________________________________________________________ 6257CM,6263CM,6265CM,6269CM,6273CM,6275CM,6279CM...) - REMOVAL/INSTALLATION___________________________________________________________________________
TASK 27-54-44-000-001
Removal of the Steady Bearings FIN 6207CM(6257CM)/6213CM(6263CM)
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.
R R R R R CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:_______ - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS. - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS. - MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
1. Reason for the Job__________________
Self Explanatory
2. Job Set-up Information______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific No specific No specific No specific 98D27803500001 circuit breaker(s) safety clip(s)safety barrierswarning noticeaccess platform 2.5 m (8 ft. 2 in.)1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵5(11)