A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵9(160)

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 Subtask 27-96-00-865-087
 C. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 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/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
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 4. Procedure
_________ Subtask 27-96-00-710-077
 A. Operational Test of the THS Actuator Electrical Control (Activation For BITE Test)
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. Ground setting with the ELAC2
 A. On the center pedestal:
 -move the pitch trim control wheel to the 13.5.UP position.
 B. On the panel 24VU:
-push the FLT CTL/ELAC2 pushbutton switch.
 C. On the panel 24VU:
-release the FLT CTL/ELAC2 pushbutton switch.
 2. Ground setting with the ELAC1.
 A. On the center pedestal:
 -move the pitch trim control wheel to the 13.5.UP position.
 B. On the panel 23VU:
-push the FLT CTL/ELAC1 pushbutton switch.
The OFF legend of this pushbuttonswitch goes off.
 On the center pedestal:
 -the pitch trim control wheel goes back to 0.
The OFF legend of this pushbuttonswitch comes on.
The OFF legend of this pushbuttonswitch goes off.
 On the center pedestal:
 -the pitch trim control wheel goes back to 0.
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 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
A. On the panel 23VU:
-release the FLT CTL/ELAC1 pushbutton switch.
 3. Ground setting with the SEC1.
 A. On the center pedestal:
 -move the pitch trim control wheel to the 13.5.UP position.
 B. On the panel 23VU:
-
push the FLT CTL/SEC1 pushbutton switch.

 A.
 On the panel 23VU:

-release the FLT CTL/SEC1 pushbutton switch.
 4. Ground setting with the SEC2.
 A. On the center pedestal:
 -move the pitch trim control wheel to the 13.5.UP position.
 B. On the panel 24VU:
-push the FLT CTL/SEC2 pushbutton switch.
 NOTE : If the test fails (Ref.
____ TSM TASK 27-96-00-810-802).
The OFF legend of this pushbuttonswitch comes on.
The OFF legend of this pushbuttonswitch goes off.
 On the center pedestal:
 -the pitch trim control wheel goes back to 0.
The OFF legend of this pushbuttonswitch comes on.
The OFF legend of this pushbuttonswitch goes off.
 On the center pedestal:
 -the pitch trim control wheel goes back to 0.

 5. Close-up
________ Subtask 27-96-00-860-057
 A. Put the aircraft back to its initial configuration.
 (1)
 ON the panel 23VU:

 -Push the FLT CTL/ELAC1 , FLT CTL/SEC1 and the FLT CTL/SEC3 pushbutton switches.(on these pushbutton switches,the OFF legends go off).

 (2)
 ON the panel 24VU:

 -Push the FLT CTL/ELAC2 pushbutton switch.(on this pushbutton switch, the OFF legend goes off).

 (3)
 Depressurize the aircraft hydraulic systems (Ref. TASK 29-10-00-864-003) (Ref. TASK 29-23-00-864-001).

 (4)
 De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).

 

 Subtask 27-96-00-410-055
 B. Close Access
 (1)
 Install the protective cover on the battery power center 105VU.

 (2)
 Tighten the two screws.

 (3)
 Close the access door 822.

 (4)
 Remove the access platform(s).

 

 TASK 27-96-00-710-023
 Integrity Test of the Flight Control System
 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.
 1. Reason for the Job
__________________
 After maintenance operation on system electrical installation.
　
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