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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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 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-002  USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)
 C. Expendable Parts
 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
5 cotter pin 32-31-03 22 -180 11 cotter pin 32-31-03 22 -260A 19 cotter pin 32-31-03 22 -260A 21 cotter pin 32-31-03 22 -180
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 32-31-44Page 455 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1


 D. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-12-29-611-001 Fill the Hydraulic Fluid Reservoir with a Hand Pump 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
 External Power 29-10-00-864-001 Depressurize the Green Hydraulic System 29-14-00-614-001 Depressurization of the Hydraulic Reservoirs 29-23-00-860-001 Disconnection of the Isolation Coupling of the Power
 Transfer Unit (PTU) 29-23-00-860-002 Connection of the Isolation Coupling of the Power Transfer Unit (PTU) 32-00-00-481-001 Installation of the Safety Devices on the Landing Gears 32-00-00-860-001 Flight Configuration Precautions with Electrical Power 32-00-00-860-002 Ground Configuration after Flight Configuration with
 Electrical Power 32-12-00-010-001 Open the Main Gear Doors for Access 32-12-00-410-001 Close the Main Gear Doors after Access 32-31-00-720-002 Functional Test of the Normal Extension and
 Retraction of the Landing Gear 32-31-44-400-003 Installation of the Uplock Assembly 2509GM (2510GM)
 with A/C on Jacks 32-33-00-720-001 Functional Check of Free-Fall Extension 51-75-13-916-002 Repair to a layer of Corrosion Preventive Compound 32-31-44-991-006 Fig. 406
 3. Job Set-up
__________
 Subtask 32-31-44-860-060
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the aircraft is on jacks

 (2)
 Make sure that the PTU isolation coupling is disconnected (Ref. TASK 29-23-00-860-001).

 (3)
 Make sure that the aircraft electrical circuits are energized (Ref. TASK 24-41-00-861-002)

 (4)
 Make sure that the flight configuration precautions are obeyed (Ref. TASK 32-00-00-860-001).


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 (5)
 Make sure that the Green hydraulic system is depressurized (Ref. TASK 29-10-00-864-001).

 (6)
 Make sure that the reservoir of the Green hydraulic system is depressurized (Ref. TASK 29-14-00-614-001).


 Subtask 32-31-44-865-059
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------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 121VU HYDRAULIC/G HYD/PUMP ENG1/CTL 1701GK R35 121VU HYDRAULIC/G HYD/PUMP ENG1/MONG 1702GK R34
 Subtask 32-31-44-941-058
 C. Safety Precautions
 (1)
 Put the safety barriers in position.

 (2)
 Make sure that the ground safety locks are on the landing gear (Ref. TASK 32-00-00-481-001).

 (3)
 Put a warning notice on the ground service connection to tell persons not to pressurize the Green and Yellow hydraulic systems.

 (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.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 32-31-44Page 457 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 Subtask 32-31-44-560-054


 D. Preparation of the Replacement Component
 (1)
 Make sure that the dimension "Y" of the new support strut A is the same of that retained from the removed component.

 (2)
 Make sure that the dimension "Z" of the new support strut B is the same of that retained from the removed component. (Ref. Fig. 406/TASK 32-31-44-991-006)


 Subtask 32-31-44-820-053
 E. Adjustment of the Support Strut A and B
 (1)
 Make sure that the dimension "Y" of the new support strut A is 168.55 mm (6.64 in.). (Ref. Fig. 406/TASK 32-31-44-991-006)
 
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