(2)
Remove the nut (31), the washer (32) and the bolt (38).
(3)
In the cockpit, remove the screws (10) and the washers (11).
(4)
Remove the screws (6) and the washers (7).
(5)
Cut and remove the lockwire from the nut (43).
(6)
Fully loosen the nut (43).
(7)
Fully tighten the screw (44).
(8)
Remove the clip (45).
(9)
Lightly pull the handle (15) so that you can remove the pin (16).
(10)
Remove the pin (16). NOTE : The pin (16) has a slot so that you can disengage it from the
____
cable (17) when you remove it.
(11)
Pull the cable (17) lightly down and remove the cover (5) with the rod (39).
(12)
Remove the locking-pin (46).
(13)
Remove the pin (40). NOTE : The pin (40) has a slot so that you can disengage it from the
____
cable (17) when you remove it.
(14)
Remove the cable (17).
(15)
Remove the screw (44) and the nut (43).
(16)
Remove the cotter pin (22) and discard it.
(17)
Remove the nut (21), the washer (20) and the bolt (18).
(18)
Remove the cotter pin (23) and discard it.
1EFF : ALL 1 27-21-43Page 409 1 1 May 01/00R 1 1 1CES 1
(19)
Remove the nut (24), the bolt (27) and the washers (25).
(20)
Lift the lower part of the rack assembly (26) to compress the springs
(41) and (42). Remove the spacer (28).
(21)
Remove the rack assembly (26) and the springs (41) and (42).
(22)
Remove the cotter pins (33) and discard them.
(23)
Remove the washers (34) and the pins (36).
(24)
Remove the actuator (37).
1EFF : ALL 1 27-21-43Page 410 1 1 May 01/00R 1 1 1CES 1
TASK 27-21-43-400-002
Installation of the Pedal Position Adjuster Assembly
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.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 1.5 m (4 ft. 11 in.) 98A27901002000 1 PIN, RIGGING - RUDDER CONTROL
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)
1EFF : ALL 1 27-21-43Page 411 1 1 Aug 01/04R 1 1 1CES 1
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
22 cotter pin 27-21-01 02B-040 23 cotter pin 27-21-01 02B-040 30 cotter pin 27-21-01 02B-040 33 cotter pins 27-21-01 02B-095
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from the External Power 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground Power Supply
**ON A/C 001-049, 051-062, 101-105, 151-152, 201-205,
27-21-43-991-003 Fig. 401
R **ON A/C 063-099, 106-149, 153-199, 206-299, 301-399, 401-499,
27-21-43-991-003-A Fig. 401A
**ON A/C 001-049, 051-062, 101-105, 151-152, 201-205,
27-21-43-991-004 Fig. 402
R **ON A/C 063-099, 106-149, 153-199, 206-299, 301-399, 401-499,
27-21-43-991-004-A Fig. 402A -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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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(23)
