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时间:2011-03-26 00:00来源:蓝天飞行翻译 作者:admin
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 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
49VU L/G/LGCIU/SYS1/NORM 1GA C09 121VU HYDRAULIC/LGCIU/SYS2 2GA Q35 121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34
 4. Procedure
_________
 (Ref. Fig. 401/TASK 32-51-42-991-001) Subtask 32-51-42-020-053
 A. Removal of the Steering Cylinder
 NOTE : The removal procedure is the same for the front and the rear

____
 cylinder.
 It is better to start with the rear cylinder.

 (1)
 Before the removal of the rear cylinder, do the following steps:

 (a)
 Make sure that the NLG wheels are fully turned to the right.

 (b)
 Disconnect the electrical connector (9) from the proximity-sensor 24GA (10).

 (c)
 Put blanking caps on the disconnected electrical connectors.

 (d)
 Attach the disconnected electrical bundle to the leg during the maintenance operation.

 

 (2)
 Precaution: NOTE : When you remove the rubber protective coating, use a spatula

 (3)
 Disconnect the hydraulic couplings (2) and drain the hydraulic fluid.


____ to prevent damage to the surfaces of the components.
 1EFF : ALL 1 32-51-42Page 405 1 1 Aug 01/05R 1 1 1CES 1


 Nose-Wheel Steering Cylinder Figure 401/TASK 32-51-42-991-001
 1EFF : 1 1R 1CES  ALL  1 11 1 32-51-42 Page 406 Aug 01/05

 

 (4)
 Put blanking plugs on the disconnected line ends.

 (5)
 Remove the lockwire and the nine screws (6) and the washers (5). Discard the washers (5).

 (6)
 Remove the split washer (4).

 (7)
 Remove the cylinder (1).

 (8)
 Remove the seal (7) with its backuprings and discard them.


 1EFF : ALL 1 32-51-42Page 407 1 1 Aug 01/05R 1 1 1CES 1


 TASK 32-51-42-400-001
 Installation of the Nose Wheel Steering Cylinder
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific safety barriers
 No specific warning notice(s)
 No specific container 5 l (1.3208 USgal)
 No specific Torque Wrench : range 0.20 to 3.60 m.daN

 (2.00 to 26.00 lbf.ft)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific  corrosion resistant steel lockwire 0.8 mm (0.03 in.) dia.
 Material No. 05-047  C Z-11.904 ANTI COR. COMPOUND(HIGH TEMP.SILICONE SEALANT) (Ref. 20-31-00)
 Material No. 09-002  USA MIL-S-8802 TYPE I CLASS B FUEL TANK SEALANTPOLYSULFID(NO LONGER AVAILABLE (Ref. 20-31-00)
 Material No. 11-004A 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
 1EFF : ALL 1 32-51-42Page 408 1 1 Aug 01/05R 1 1 1CES 1


 C. Expendable Parts
 -------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
5 5 7 7 7 7 7  lockwashers lockwashers seal seal seal seal seal  32-51-42 01A-02032-51-42 01B-02032-51-42 01A-09032-51-42 01A-090A32-51-42 01A-140A32-51-42 01B-09032-51-42 01B-140
 D. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
R R R R R  07-11-00-586-001 09-10-00-584-002 29-10-00-864-001 29-10-00-864-002 32-00-00-860-001 32-00-00-860-002 32-51-00-720-003 32-69-00-740-001 32-51-42-991-001  Lowering of the Aircraft at Forward Jacking Point, MLG Wheels on the GroundTowing with the Nose Gear from the FrontDepressurize the Green Hydraulic System Depressurize the Yellow Hydraulic System Flight Configuration Precautions with Electrical Power Ground Configuration after Flight Configuration with Electrical PowerFunctional Test of the Nose Wheel Steering with the Handwheel.BITE Check Landing Gear Control Interface Unit (LGCIU) using MCDU to Ensure that Continuous BITE is OperativeFig. 401
 
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