-
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 warning notices
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 27-21-42Page 416 1 1 Feb 01/05R 1 1 1CES 1
C. Expendable Parts
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FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
R 51 cotter pin 27-21-01 03A-161 61 cotter pin 32-42-01 04 -010 68 cotter pin 27-21-01 01 -010 68 cotter pin 27-21-01 01A-010 77 cotter pin 32-42-01 04 -010 82 cotter pin 32-42-01 04 -010 89 cotter pin 32-42-01 04 -010 94 cotter pin 27-21-01 01 -010 94 cotter pin 27-21-01 01A-010 108 nuts 27-21-01 06 -010
D. Referenced Information
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REFERENCE DESIGNATION
-------------------------------------------------------------------------------
27-21-43-000-001 Removal of the Pedal Position Adjuster Assembly 27-21-43-400-002 Installation of the Pedal Position Adjuster Assembly 27-24-00-710-001 Operational Test of the Rudder Hydraulic Actuation 32-42-47-000-001 Removal of the Transmitter Unit - Brake Pedal (9GG) 32-42-47-400-001 Installation of the Transmitter Unit - Brake Pedal
(9GG) 32-43-12-000-001 Removal of the Brake Control Master Cylinder (2625GM,2626GM) 32-43-12-400-001 Installation of the Brake Control Master Cylinder (2625GM,2626GM)
3. Job Set-up
__________
Subtask 27-21-42-860-054
A. Aircraft Maintenance Configuration
(1)
Make sure that the pedal position adjuster assembly is removed (Ref. TASK 27-21-43-000-001).
(2)
Make sure that the brake control master cylinders (2625GM, 2626GM) are removed (Ref. TASK 32-43-12-000-001).
(3) Make sure that the brake pedal transmitter unit (9GG) is removed
(Ref. TASK 32-42-47-000-001).
(4) On the pedals (CAPT and F/O) make sure that the warning notices are
in position to tell persons not to operate them.
4. Procedure_________
R Subtask 27-21-42-420-051-A
R A. Installation of the F/O pedals
R (1) Apply COMMON GREASE (Material No. 04-004) on the attachment hardware.
R (2) Install the pedal assembly between the structure (107) through the
R avionics compartment.
R NOTE : Make sure that the rods (66), (67), (71) and (90) are____
R correctly installed in their bellcranks (60), (88), (72) and
R (91).
R (3) Install the bushes (105), the bolts (106) and the new nuts (108).
R (4) Install the bolt (95), the washer (92), the nut (93) and the new
R cotter pin (94) (Ref. Detail C).
R (5) Install the bolt (64), the washer (63), the nut (62) and the new
R cotter pin (61) (Ref. Detail D).
R (6) Install the bolt (65), the washer (87), the nut (86) and the new
R cotter pin (89) (Ref. Detail D).
R (7) Install the bolt (73), the washer (70), the nut (69) and the new
R cotter pin (68) (Ref. Detail E).
R (8) Install the bolt (55), the washer (54), the bonding strip (53), the
R nut (52) and the new cotter pin (51) (Ref. Detail B).
R (9) Install the bolt (104) on the post (72) with the bush (103) and the
R pedal (74).
R (10) Install the washer (101) and the nut (100).
R (11) Install the bolt (113) on the post (91) with the bush (112) and the
R pedal (85).
R (12) Install the washer (110) and the nut (109).
R R (13) Safety the nuts (100) and (109) with Lockwire corrosion resistant steel dia 0.8 mm (0.03 in.). 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2(20)
