• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-21 13:53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

 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/FCDC1/SPLY 20CE1 B10 49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 121VU FLIGHT CONTROLS/FCDC2/SPLY 20CE2 Q20 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18 121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
 Subtask 27-34-51-140-054
 C. Cleaning
 (1)
 Clean the component interface and/or the adjacent area.

 (2)
 Make sure that the parts retained from the removed component are clean and in the correct condition.


 1EFF : ALL 1 27-34-51Page 459 1 1 May 01/05R 1 1 1CES 1


 4. Procedure
_________
 (Ref. Fig. 406/TASK 27-34-51-991-005) Subtask 27-34-51-420-057
 A. Install the servo control actuator MSVT
 (1)
 Apply COMMON GREASE (Material No. 04-004) to the bolts (4).

 (2)
 Install the O rings (6) and (7) in the MSVT (3).

 (3)
 Put the MSVT (3) in position on the servo control actuator and support it.

 (4)
 Install the washers (5) and the bolts (4) into the MSVT (3).

 (5)
 TORQUE the bolts (4) to between 0.33 and 0.41 m.daN (29.20 and 36.28 lbf.in)

 (6)
 Remove the blanking caps.


 (7)
 Connect the electrical connectors. Subtask 27-34-51-081-053

 B. Remove Locking Devices
 (1) Remove the PIN-SIDE STICK LOCKING from the CAPT and F/O side stick controllers.

 (2)
 Remove the SETTING TOOL-NEUTRAL, ELEVATOR from the elevator. Subtask 27-34-51-865-059


 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 15CE1, 15CE2, 16CE1, 16CE2, 19CE1, 19CE2, 19CE3, 20CE1, 20CE2, 21CE1, 21CE2, 22CE
 Subtask 27-34-51-710-053
 D. Operational Test
 (1) Do an operational test of the servo controls. (Ref. TASK 27-34-00-710-001)
 1EFF : ALL 1 27-34-51Page 460 1 1 May 01/05R 1 1 1CES 1


 5. Close-up
________ Subtask 27-34-51-410-055
 A. Visual Inspection
 (1) Make sure that the work area is clean and clear of tool(s) and other items.
 Subtask 27-34-51-410-056
 B. Close Access
 (1) Close the trailing edge access panels 334DB and/or 344DB (Ref. TASK 55-13-11-400-001)
 Subtask 27-34-51-942-055
 C. Remove Ground Equipment
 (1)
 Remove the warning notice(s).

 (2)
 Remove the access platform(s).


 1EFF : ALL 1 27-34-51Page 461 1 1 May 01/05R 1 1 1CES 1


 TASK 27-34-51-000-009 Removal of the Servo Control Actuator Eye-End WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
 WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______ MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
 WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
 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 : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______ FALL CAN INJURE OR KILL YOU.
 CAUTION : DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF
_______ CARBONFIBER REINFORCED PLASTIC.
 1. Reason for the Job__________________ Self explanatory.
 2. Job Set-up Information______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific variable access platform No specific warning notices 98D27309001000 1 TOOL-ELEVATOR NEUTRAL SETTING 98D27903500000 2 PIN-SIDE STICK LOCKING
 1EFF : ALL 1 27-34-51Page 462 1 1 May 01/05R 1 1 1CES 1


 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
 
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 FLIGHT CONTROLS 飞行操纵3(73)