(7)
Cut and remove the lockwire from the screws (17).
(8)
Remove the screws (17) and the washers (18). Disengage the flange
(13). Remove the half-shells (14).
(9)
At zone 310, remove the 4 screws (31) and the washers (32) (See
Detail H).
(10)
Release the quick-attach fasteners (28). Remove the chain guards (29) and (30).
(11)
Remove the screws (27) and the chain guide (26).
(12)
Remove the 6 screws (33), the washers (32) and the guard (34) (See Details H and J).
(13)
At zone 241:
(a)
Remove the locking clips (22) from the turnbuckles (23),
(b)
Turn the turnbuckles (23) until the cables (5), (6), (10), (11) are disconnected.
(14)
Disengage the chain (7) from the gear wheel of the lower shaft assembly (1).
(15)
Pull and remove the chain (7) and cables (5) (6) assembly. NOTE : Be careful with the ends of the cables (5) and (6) when they
____
move between the frames.
(16)
Disengage the upper end of the springs (41) from the 2 flanges (51) of the tension regulator (40) (See Details J and L).
(17)
Remove the cotter pin (43) and discard it. Remove the nut (44) and the washer (45) (See Detail J and Section KK).
(18)
Remove the bolt (47) and the spacer (46).
(19)
Lift the 2 flanges (51) and hold them in this position (See Detail L).
(20)
Remove the cotter pin (54) and discard it. Remove the nut (55) and the washer (53) (See Detail L and Section MM).
1EFF : 301-399, 1 27-41-44Page 423 1 1 May 01/05R 1 1 1CES 1
(21)
Remove the bolt (50) and the spacer (52).
(22)
Remove the cotter pin (56) and discard it. Remove the nut (57) and the washer (58) (See Detail L and Section PP).
(23)
Remove the bolt (60) and the spacer (59).
(24)
Disengage the chain (35) from the gear wheel of the input shaft (25) of the THS actuator (65) (See Details H and G).
(25)
Pull the cables (10) and (11) up to FR70. NOTE : Be careful with the ends of the cables (10) and (11) when they
____
move between the frames.
(26)
At FR70, remove the sleeve (16) and the flanges (12) and (13) (See Detail D and Section EE).
(27)
Pull and remove the chain (35) and cables (10) (11) assembly from the THS actuator (65) (See Detail Q).
R 1EFF : 301-399, 1 27-41-44Page 424 1 1 May 01/05 1 1 1CES 1 **ON A/C ALL
TASK 27-41-44-400-001
Installation of the THS Control Cables
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 CONTROLS ARE CLEAR.
_______ MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR 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 tensiometer No specific warning notices No specific access platform 1.5 m (4 ft. 11 in.) No specific access platform 1.6 m (5 ft. 3 in.) No specific access platform 2.8 m (9 ft. 2 in.) 0U190360 1 PIN - RIGGING 98D27403500000 1 PITCH TRIM CONTROL LOCKING 98F27003500000 1 LOCKING TOOL-CABLE
1EFF : ALL 1 27-41-44Page 425 1 1 May 01/05R 1 1 1CES 1
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific Lockwire corrosion resistant steel dia 0.8 mm (0.03 in.)
Material No. 04-004 USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
21 cable ties 27-41-03 05 -020 43 cotter pin 27-41-42 01 -110 54 cotter pin 27-41-42 01 -180 56 cotter pin 27-41-42 01 -180
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱3(119)
