• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-20 20:51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

1. On the FLT CTL panel 24VU (23VU):
 -Release the FAC2 (FAC1) pushbutton switch.
2. On the center pedestal, on the RUD TRIM/PARKING BRK panel:
 -Make sure that the rudder trim indicator is energized.
 -Hold the RUD TRIM switch in the NOSE L position to get the maximum movement of the rudder.
R
R - Release the switch.
 -Push and release the RUD TRIM/RESET pushbutton switch.
3. On the FLT CTL panel 24VU (23VU):
 -Push the FAC2 (FAC1) pushbutton switch.
-On the FAC2 (FAC1) pushbutton switch,the OFF legend comes on and the FAULT legend stays off.
-The indicator shows approximately 0..
-On the F/CTL page on the lower ECAMdisplay unit, the rudder trim and therudder move to the left.
-
The left pedal is moves forward.

 -
The rudder trim indicator shows approximately the maximum threshold engraved on panel.

-
The rudder trim and the rudder go tothe zero position.

 -
The rudder trim indicator shows approximately 0..


-On this pushbutton switch, the OFFlegend goes off and the FAULT legend stays off.
 1EFF : ALL 1 22-62-00Page 503 1 1 Nov 01/02 1 1 1CES 1


 5. Close-up
________ Subtask 22-62-00-860-051
 A. Put the aircraft back to its initial configuration.
 (1)
 Depressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-10-00-864-003).

 (2)
 Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).

 (3)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).


 1EFF : ALL 1 22-62-00Page 504 1 1 Feb 01/98 1 1 1CES 1


 CONTROL SWITCH - RUDDER TRIM (9CC) - REMOVAL/INSTALLATION
_________________________________________________________ TASK 22-62-11-000-001 Removal of the RUD TRIM Control Switch (9CC) 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 : MAKE SURE THAT THE WHEEL CHOCKS 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 blanking caps No specific circuit breaker(s) safety clip(s) DMC519 1 ELECTRICIAN SERVICE TOOL KIT
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
22-62-11-991-002 Fig. 401
 1EFF : ALL 1 22-62-11Page 401 1 1 Feb 01/98 1 1 1CES 1

 3. Job Set-up
__________

 Subtask 22-62-11-865-050
 A. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AUTO FLT/FAC1/28VDC 5CC1 B04 121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU HYDRAULIC/PARK BRK/CTL/STBY 71GG N37 121VU HYDRAULIC/PARK BRK/CTL/NORM 70GG N36

R 122VU LIGHTING/INSTL LT/MAIN INST/PNL AND/PED 4LF Y04
 4. Procedure
_________
 Subtask 22-62-11-020-050

 A. Removal of the Panel 110VU
 (Ref. Fig. 401/TASK 22-62-11-991-002)

 (1)
 Loosen the four quarter-turn fasteners (8) to release the panel 110VU (11).

 (2)
 Carefully lift the panel 110VU (11) to get access to the electrical connectors (10).

 (3)
 Disconnect the four electrical connectors (10).

 (4)
 Put blanking caps on the disconnected electrical connectors.


 (5)
 Remove the panel 110VU (11).
 Subtask 22-62-11-020-051


 B.
 Removal of the RUD TRIM Control Switch (9CC)
 (Ref. Fig. 401/TASK 22-62-11-991-002)


 (1)
 Loosen the two screws (3) of the knob (2).

 (2)
 Remove the knob (2) from the shaft of the control switch (12).

 (3)
 Remove the screw (5), the pin (6) and the knob (4).
 
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 AUTO FLIGHT 自动飞行2(20)