A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵1(79)

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 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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 27-14-00-200-001 Check of the Aileron Servo Control Oscillations. 29-10-00-863-001 Pressurize the Green Hydraulic System 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
 Power Supply 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow
 Hydraulic System through the PTU with the Electric Pump 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems
 after Operation of the PTU 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 27-14-00-991-001 Fig. 501 27-14-00-991-005 Fig. 502
 1EFF : ALL 1 27-14-00Page 505 1 1 Feb 01/05R 1 1 1CES 1

 3. Job Set-up__________
 Subtask 27-14-00-861-053
 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
 Subtask 27-14-00-865-053
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
R  -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/FCDC1/SPLY 20CE1 B10 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 121VU PTR/SPLY 6TW J21 121VU CFDS/CFDIU/SPLY 2TW J18 121VU FLIGHT CONTROLS/FCDC2/SPLY 20CE2 Q20 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20 
R  **ON A/C ALL 
R  Post SB  31-1163 For A/C 155-156,208-209, 
R  121VU CFDS/CFDIU/BACK/UP  8TW  J17 
R  **ON A/C ALL
 Subtask 27-14-00-860-064
 C. Aircraft Maintenance Configuration
 (1) On the panel 23VU, make sure that the FLT CTL/ELAC1 pushbutton switch is pushed (on this pushbutton switch, the OFF and FAULT legends are off).

 

 (2)
 On the panel 24VU, make sure that the FLT CTL/ELAC2 pushbutton switch is pushed (on this pushbutton switch, the OFF and FAULT legends are off).

 (3)
 Make sure that all the hydraulic systems are depressurized.

 (4)
 On the center pedestal, make sure that the flap and slat control lever is in the O position.

 (5)
 On the center pedestal, make sure that the speed brake control lever is in the RET position.

 (6)
 Pressurize the Green and Blue hydraulic systems (Ref. TASK 29-10-00-863-001) (Ref. TASK 29-10-00-863-003).

 (7)
 Operate the aileron ten times with the side stick to bleed the system.

 (8)
 On the panel 23 VU, release the FLT CTL/ELAC1 pushbutton switch (on this pushbutton switch, the OFF legend comes on).

 (9)
 Operate the aileron ten times with the side stick to bleed the system.

 (10)
 Put the side stick in the neutral position.

 (11)
 Install the PIN-SIDE STICK LOCKING (98D27903500000) on the side sticks.

 (12)
 Put the warning notices on the CAPT and F/O side sticks to tell persons not to operate the side sticks.

 (13)
 On the panel 23 VU, push the FLT CTL/ELAC1 pushbutton switch (on this pushbutton switch, the OFF legend goes off).

 (14) Depressurize the Green hydraulic system (Ref. TASK 29-23-00-864-001) Subtask 27-14-00-010-051
 D. Get Access
 (1)
 Put the access platform at the access door 822.

 (2)
 Open the access door 822.

 (3)
 Open the battery power center 105VU:

 -loosen the two screws and remove the protective cover.
 1EFF : ALL 1 27-14-00Page 507 1 1 Aug 01/01R 1 1 1CES 1

 (4)
 Put the access platform in position at zone:

 (a)
 575 for the left aileron,

 (b)
 675 for the right aileron.

 

 (5)
 Open the access door:

 (a)
 575KB for the left aileron,

 (b)
 675KB for the right aileron. NOTE : For an easier access for adjustment of the aileron

 

____ servocontrol, remove the rubbing strip seal, if necessary.
 4. Procedure
_________
 (Ref. Fig. 501/TASK 27-14-00-991-001, 502/TASK 27-14-00-991-005) Subtask 27-14-00-820-052
　
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