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R 122VU LIGHTING/INSTL LT/MAIN INST/PNL AND/PED 4LF Y04
Subtask 32-33-11-010-050
C. Get access to the NLG free-fall extension mechanical system
(1)
Open the nose landing-gear doors (Ref. TASK 32-22-00-010-001).
(2)
Put the access platform in position in zone 123.
(3)
Put the access platform in position below the lateral avionics-compartment door 822.
(4) Open the lateral avionics-compartment door 822.
Subtask 32-33-11-480-050
D. Installation of Rigging Pins
(Ref. Fig. 401/TASK 32-33-11-991-002)
(1) Put the PIN, RIGGING - RUDDER CONTROL (98A27901002000) (26) in position on the lower bellcrank (27).
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Free-Fall Control-Handle Assembly - Location
Figure 401/TASK 32-33-11-991-002
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(2) Put the RIGGING PIN (98A27801001000) (20) in position on the cable quadrant (21).
Subtask 32-33-11-010-052
E. Get access to the control handle
(Ref. Fig. 402/TASK 32-33-11-991-001)
(1)
In the cockpit, turn by a quarter turn the fasteners (2) of the panels (1) and (3).
(2)
Remove the panels (1) and (3) from their housings.
(3)
Remove the printer (5) (Ref. TASK 31-35-22-000-001).
(4)
Remove the screws (7), the nuts (4), the washers (11) and the bushes (10).
(5)
Loosen the screws (9) and move the casing (8) at an angle.
4. Procedure
_________
(Ref. Fig. 402/TASK 32-33-11-991-001) Subtask 32-33-11-020-050
A. Removal of the Control Handle
(1)
Remove the screws (6) and (12).
(2)
Lift the panel (13), disconnect the plugs (14) and remove the panel (13).
(3)
Remove the handle assembly (15) from its housing.
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Free-Fall Control-Handle Assembly
Figure 402/TASK 32-33-11-991-001
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TASK 32-33-11-400-001
Installation of the Free-Fall Control-Handle Assembly
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
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REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific lockwire
No specific shims
No specific warning notice(s)
No specific access platform 1.7 m (5 ft. 7 in.)
R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
No specific lockwire corrosion resistant steel 0.8mm (0.032in) dia.
Material No. 04-004 USA MIL-PRF-23827 TYPE I
SYNTH.ESTER BASED GREASE HIGH PRESSURE
(Ref. 20-31-00)
Material No. 04-022 USA MIL-PRF-81322 GRADE 2
SYNTHE.HYDROCARBON GREASE HIGH PRESSURE
(Ref. 20-31-00)
Material No. 11-002 USA MIL-PRF-680
DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT)
(Ref. 20-31-00)
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C. Expendable Parts
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FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
cotter pin 32-33-01 03 -010
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
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31-35-22-400-001 Installation of the Printer (4TW)
32-00-00-481-001 Installation of the Safety Devices on the Landing
Gears
32-22-00-010-001 Nose Gear Doors - Ground Doors Opening
32-22-00-410-001 Nose Gear Doors - Ground Doors Closing
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本文鏈接地址：A320飛機維護手冊 AMM LANDING GEAR 起落架5(134)
