• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 00:00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

_______
 CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.

 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 spillage container
 No specific Torque Wrench : range 0.20 to 3.60 m.daN

 (2.00 to 26.00 lbf.ft) No specific Torque Wrench : range 2.00 to 20.00 m.daN
 (15.00 to 150.00 lbf.ft)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R Material No. 02-003  F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)
 Material No. 04-011  USA MIL-G-4343
 SILICONE GREASE PNEUMATIC SYST AND SEALS
 (Ref. 20-31-00)

 Material No. 09-005  USA MIL-S-81733 CLASS C CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00)
 Material No. 19-010  USA AMS 5687
 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
 (Ref. 20-31-00)

 1EFF : ALL 1 52-36-18Page 406 1 1 Feb 01/05 1 1 1CES 1 C. Expendable Parts


 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
1  cotter pin  52-36-02 03 -080
 1  cotter pin  52-36-04 08C-080
 1  cotter pin  52-36-04 08D-080
 26  cotter pin  52-36-02 03 -080
 26  cotter pin  52-36-04 08C-080
 26  cotter pin  52-36-04 08D-080
 D. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-912-004
R 29-00-00-910-002 29-10-00-864-002
29-14-00-614-001 29-14-00-614-002 29-23-00-860-001 29-23-00-860-002 29-24-00-863-001 52-30-00-860-002 52-31-11-820-004
52-36-00-600-001 52-36-18-991-001
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)-Safety Procedures of the Hydraulic SystemDepressurize the Yellow Hydraulic SystemDepressurization of the Hydraulic ReservoirsPressurization of the Hydraulic Reservoirs through the Ground ConnectorDisconnection of the Isolation Coupling of the Power Transfer Unit (PTU)Connection of the Isolation Coupling of the Power Transfer Unit (PTU)Pressurize the Yellow Hydraulic System with the Electric PumpClose the FWD or AFT Cargo-Compartment Door with the Yellow Electric PumpAdjustment of the Door Opening AngleHydraulic System for the Cargo Compartment Doors -ServicingFig. 401
 1EFF : ALL 1 52-36-18Page 407 1 1 Feb 01/05 1 1 1CES 1


 3. Job Set-up
__________
 Subtask 52-36-18-860-057

 A. Aircraft Maintenance Configuration
 (1)
 Obey the hydraulic safety procedures (Ref. TASK 29-00-00-910-002).

 (2)
 Make sure that the Yellow hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-10-00-864-002)

 (3)
 Make sure that the reservoir of the Yellow hydraulic system is depressurized (Ref. TASK 29-14-00-614-001).

 (4)
 Make sure that the isolation coupling of the Power Transfer Unit (PTU) is disconnected (Ref. TASK 29-23-00-860-001).

 (5)
 Make sure that the warning notices are in position.


 (6) Make sure that the spillage container is below the flexible hoses. Subtask 52-36-18-865-051
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU HYDRAULIC/HYD POWER/Y 3803GX N30 122VU DOORS/CARGO 1MJ T12 123VU Y HYD/ELEC/PUMP 3802GX AB06
R 123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03
 1EFF : ALL 1 52-36-18Page 408 1 1 Feb 01/99 1 1 1CES 1 1EFF : ALL 1 52-36-18Page 409 1 1 Aug 01/01 1 1 1CES 1


 4. Procedure_________
 (Ref. Fig. 401/TASK 52-36-18-991-001)
 Subtask 52-36-18-820-050
 A. Pre-Adjustment of the Replacement Door Actuator
 
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 DOORS 舱门6(129)