• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-25 18:04来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 1EFF : ALL 1 32-42-16Page 409 1 1 Aug 01/05 1 1 1CES 1


 (11)
 Remove the normal-brake servovalve manifold assembly from the MLG mounting lugs.

 (12)
 If you are to replace the manifold (19), remove these items:

 -
the pressure transducers (17) and (18) (Ref. TASK 32-42-21-000-001)

 -
the safety valves (3) (Ref. TASK 32-42-36-000-001)

 -
the servovalves (7) and (12) (Ref. TASK 32-42-48-000-001).

 


R 1EFF : 004-049, 053-099, 101-149, 151-199, 1 32-42-16Page 410 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1 **ON A/C ALL


 TASK 32-42-16-400-001
 Installation of the Normal-Brake Servovalve Manifold Assembly 2612GM (2613GM)
 WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______ NOTICES ARE IN POSITION.
 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 No specific Torque Wrench : range 0.20 to 3.60 m.daN
 (2.00 to 26.00 lbf.ft) No specific Torque Wrench : range 1.00 to 10.00 m.daN
 (8.00 to 75.00 lbf.ft)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-018  USA AMS 3267/3 CORROSION INHIBITING LOW ADHESION SEALANT (Ref. 20-31-00)
 Material No. 11-026 GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
 1EFF : ALL 1 32-42-16Page 411 1 1 May 01/05R 1 1 1CES 1


 C. Expendable Parts
 -------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION  |IPC-CSN
 -------------------------------------------------------------------------------
5 cotter pins 32-11-11 85A-005 9 tab washers 32-11-11 85D-020 9 tab washers 32-11-11 85E-020
 D. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
20-28-00-912-004  Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
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 32-11-43-400-002 Installation of the 1M and 2M Harnesses on the MLG
 Leg 32-42-00-710-001 Operational Check of the Normal Braking System 32-42-00-710-003 Operational Check of Antiskid Inhibition 32-42-00-870-001 Bleeding of the Normal Braking at the Brake Units 32-42-21-400-001 Installation of the Normal-Brake Pressure Transducer 32-42-36-400-001 Installation of the Normal Brake Safety-Valve
 2618GM(2617GM), 2616GM(2619GM)
 32-42-48-400-001 Installation of the Normal Brake Servovalve

 **ON A/C 001-002, 051-052,
 32-42-16-991-001  Fig. 401
R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 32-42-16-991-005  Fig. 402
 1EFF : ALL 1 32-42-16Page 412 1 1 Aug 01/05 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------


**ON A/C 001-003, 051-052,
 Post SB 32-1190 For A/C 001-002,051-052,
 32-42-16-991-005-A Fig. 402A
 **ON A/C ALL

 3. Job Set-up
__________
 **ON A/C 001-002, 051-052,

 (Ref. Fig. 401/TASK 32-42-16-991-001) R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 (Ref. Fig. 402/TASK 32-42-16-991-005)
 **ON A/C 001-003, 051-052,
 Post SB 32-1190 For A/C 001-002,051-052,

 (Ref. Fig. 402A/TASK 32-42-16-991-005-A)
 **ON A/C ALL


 
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 LANDING GEAR 起落架7(5)