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时间:2011-03-25 17:58来源:蓝天飞行翻译 作者:admin
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 Open the MLG doors (Ref. TASK 32-12-00-010-001).

 (3)
 Make sure that the ground safety locks are installed on the landing gear (Ref. TASK 32-00-00-481-001).

 (4)
 On the panel 400VU:

 -make sure that the landing-gear control-lever 6GA is in the DOWN position
 -put a warning notice in position to tell persons not to operate the landing gear.

 (5)
 Put warning notices, to tell persons not to pressurize the hydraulic systems:


 -in the cockpit, on the HYD overhead panel 40VU - on the hydraulic ground service-panels 197CB and 198CB - on the access door 195BB.
 Subtask 32-31-46-869-058
 B. Flight Configuration Precautions
 (1)
 If the electrical power is not necessary for other maintenance tasks, de-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002). Then it is not necessary to operate the LGCIU circuit breakers.

 (2)
 If the electrical power is necessary, do the precautions for flight configuration (Ref. TASK 32-00-00-860-001) before you open the circuit breakers.


 1EFF : ALL 1 32-31-46Page 447 1 1 Nov 01/04 1 1 1CES 1 Subtask 32-31-46-865-055


 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
 Subtask 32-31-46-860-058
 D. Aircraft Maintenance Configuration
 (1)
 Disconnect the isolation coupling of the PTU (Ref. TASK 29-23-00-860-001).

 (2)
 Depressurize the Green and Yellow hydraulic systems (Ref. TASK 29-00-00-864-001).

 (3)
 Depressurize the applicable hydraulic reservoirs (Ref. TASK 29-14-00-614-001).


 Subtask 32-31-46-010-054
 E. Get Access
 (1) Put the access platform in position:
 -
FOR 2503GM
 below zone 571


 -
FOR 2504GM
 below zone 671.

 

 4. Procedure
_________ (Ref. Fig. 404/TASK 32-31-46-991-004) Subtask 32-31-46-020-052
 A. Removal of the MLG Actuating Cylinder Wing-End Pin
 (1)
 Remove and discard the cotter pin (2).

 (2)
 Remove the nut (3), the washer (4), the nylon-washer (5), the bolt


 (6) and the collar (7).
 1EFF : ALL 1 32-31-46Page 448 1 1 Nov 01/04R 1 1 1CES 1


 MLG Actuating Cylinder Wing-End Pin - Location and Detail Figure 404/TASK 32-31-46-991-004
 1EFF : ALL 1 32-31-46Page 449 1 1 Nov 01/04R 1 1 1CES 1


 (3) Remove the pin (1) from the actuating cylinder and wing-mounting lug.

 1EFF : ALL 1 32-31-46Page 450 1 1 Nov 01/04R 1 1 1CES 1


 TASK 32-31-46-400-003
 Installation of the MLG Actuating Cylinder Wing-End Pin
 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 GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING

_______
 GEAR.

 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
 No specific warning notices

R 98D32104015000 1 GUIDE CONE
 B. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
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. 09-016  USA MIL-PRF-81733D TYPE II CLASS B
 CORROSION INHIBITING FILLET CONSISTENCY
 (Ref. 20-31-00)

 1EFF : ALL 1 32-31-46Page 451 1 1 Feb 01/05 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
 
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