• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 12:40来源:蓝天飞行翻译 作者:航空
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

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS


 -COMPONENTS THAT MOVE.
 1. Reason for the Job
__________________
 To install the access panels 540HB, 540JB, 540KB, 540LB, 540MB, 540NB, 540PB, 540QB, 540RB, 550AB, 550BB, 550CB, 550DB, 560AB, 640HB, 640JB, 640KB, 640LB, 640MB, 640NB, 640PB, 640QB, 640RB, 650AB, 650BB, 650CB, 650DB, 660AB.
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
 No specific warning notices
 No specific container 20 l (5.2833 USgal)
 No specific adjustable access platform 4 m (13 ft. 1 in.)

R No specific Torque Wrench : range 5.00 to 35.00 lbf.in R (0.05 to 0.40 m.daN) No specific Torque Wrench : range 36.00 to 220.00 lbf.in
 (0.40 to 2.60 m.daN)
 97A28002117002 1 PURGING TOOL
 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER

 

 B. Consumable Materials

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R  Material No. 04-012 
R R  Material No. 05-002 Material No. 09-007 
Material No. 11-026 
Material No. 15-004 
Material No. 19-003 
C. Expendable Parts

USA VV-P-236
 PURE MINERALVASELINE OR PETRO- LATUM (Ref. 20-31-00)
USA MIL-P-8116
PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)
USA MIL-S-4383
 BRUSHABLE FUEL RESISTANT COATING (Ref. 20-31-00)
GB DEF-STAN 68-148/1
 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
USA MIL-C-16173 GRADE 3
 CORROSION PREVENTIVE COMPOUND (Ref. 20-31-00)
USA AMS 3819
 LINT-FREE COTTON CLOTH (Ref. 20-31-00)

 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
1  sealing ring  28-12-46 01A-010
 1  sealing ring  57-27-11 03 -030
 2  sealing ring  57-27-11 03 -030
 2  sealing ring  57-27-11 04 -030
 3  sealing ring  28-12-46 02 -010
 3  sealing ring  57-27-11 04 -030
 4  sealing ring  57-27-11 04 -030
 4  sealing ring  57-27-11 05 -030
 5  sealing ring  28-12-47 01 -010
 6  sealing ring  57-27-11 06 -010
 7  sealing ring  28-12-45 01 -070
 8  sealing ring  57-27-11 08 -010

 

 D. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-11-28-650-003 Pressure Refuel with Automatic Control 20-28-00-912-002 Electrical Bonding of Components With Conductive Bolts and Screws in the Tanks 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
 from the External Power 28-00-00-200-001 Inspection of the Fuel Tank Bonding 28-00-00-200-001 Inspection of the Fuel Tank Bonding 28-10-00-910-001 Safety Procedures When You Do Work in a Fuel Tank 28-10-00-910-002 Access to the Fuel Tanks and the Work Areas 28-12-41-400-001 Installation of the Overpressure Protector 46QM
 (47QM) 28-12-45-400-002 Installation of the Panel Assembly 550CB(650CB) 28-12-46-400-001 Installation of the Overpressure-Protector Outlet 28-12-47-400-001 Installation of the NACA Vent Intake 28-25-00-650-001 Pressure Defuel 28-25-00-650-003 To Drain Remaining Fuel from the Wing Tanks and the
 Center Tank 28-25-00-869-001 Fuel Transfer 28-42-00-740-001 Status Report (BITE) 28-46-00-740-001 Functional (BITE) Test 57-55-11-000-001 Removal of the Flap Track Fairings Nos. 2, 3 and 4 57-55-11-000-004 Removal of the Flap Track Fairings Nos. 2, 3 and 4 57-55-11-400-001 Installation of the Flap Track Fairings Nos. 2, 3 and
 4 57-55-11-400-004 Installation of the Flap Track Fairings Nos. 2, 3 and 4 MPD 731000I11 (for corrective action)
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 57-27-11-991-002 Fig. 403
 **ON A/C 301-399,
 57-27-11-991-002-A Fig. 403A

 **ON A/C ALL


 3. Job Set-up
__________
 Subtask 57-27-11-941-071
 
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 WINGS 机翼2(72)