(2)
Put blanking caps on the disconnected electrical connectors.
(3)
Disconnect the artificial feel and trim unit (1) from the lever arm
(2)
as follows:
(a)
Remove and discard the cotter pin (12).
(b)
Remove the nut (11), the washer (10), the bush (7) and the bolt (6).
(c)
Move the eye-end (23) clear of the lever arm (2).
(4)
Disconnect the artificial feel and trim unit (1) from the support bracket (5) as follows:
(a)
Remove and discard the cotter pins (20).
(b)
Remove the nuts (19), the washers (18), the bushes (15) and the bolts (14).
(5)
Move the fork-end (22) clear of the lugs of the support bracket (5).
(6)
Disconnect the universal joint (21) from the splined shaft (26) of the rudder trim actuator (4).
(7)
Remove the artificial feel and trim unit (1), between the frame and the structure at the right side of the aircraft.
Artificial Feel and Trim Unit - Sheet 1
Figure 401/TASK 27-23-41-991-001
1EFF : ALL 1 27-23-41 Page 405
1 1 Feb 01/98
1 1
1CES 1
Artificial Feel and Trim Unit - Sheet 2
Figure 402/TASK 27-23-41-991-002
1EFF : ALL 1 27-23-41 Page 406
1 1 Feb 01/98
1 1
1CES 1
NOTE : Do not disconnect the universal joint (21) from the splined
____ shaft (35) of the artificial feel and trim unit (1) unless a repair or a new installation is necessary.
NOTE : It may be necessary to:
____ -shorten the artificial feel and trim unit (1), and/or,
-remove two lower attachment bolts from the frame (one at each side), to increase the clearance available.
(8)
Disconnect the solenoid (3) from the artificial feel and trim unit (1), if necessary (Ref. TASK 27-23-17-000-001).
(9)
If necessary, disconnect the universal joint (21) from the splined shaft (35) of the artificial feel and trim unit (1) as follows:
(a)
Remove and discard the cotter pin (40).
(b)
Remove the nut (39), the washer (38), the bolt (36) and the saddle washer (37).
(c)
Remove the universal joint (21) from the splined shaft (35).
TASK 27-23-41-400-001
Installation of the Artificial Feel and Trim Unit
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 TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______
CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notices
No specific access platform 11.0 m (36 ft. 1 in.) R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft) R
6137-013 1 PIN - LOCKING
98D27207547000 1 PIN - RIGGING
98D27207548000 1 PIN - RIGGING
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R Material No. 04-004 USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00) Material No. 05-027 USA MIL-L-81309 RUST INHIBITOR(FOR CORROSION USE 15-004) (Ref. 20-31-00) Material No. 08-029 USA MIL-R-46082 TYPE I ADHESIVE (Ref. 20-31-00) Material No. 19-010 USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱2(107)
