(a) Remove the cotter pin (8) and discard it.
 1EFF : ALL 1 27-22-00Page 507 1 1 May 01/05R 1 1 1CES 1

 (b)
 Remove the nut (9) and the washer (10).

 (c)
 Remove the bolt (11).

 (3)
 Connect the artificial feel spring rod (1) to the mixer (3). To do this:

 (a)
 Install the bolt (11). If you cannot install the bolt (11) easily or if you cannot install the rigging pin (4) during the operation before, do these steps:

 (b)
 Install the washer (10), the nut (9) and the new cotter pin (8).

 (4)
 Remove the rigging pins (4), (5) and (7). (Ref. Fig. 501/TASK 27-22-00-991-001, 502/TASK 27-22-00-991-002)

 (5)
 Install the blanking plug (12) on the rigging hole of the trim actuator (2). (Ref. Fig. 502/TASK 27-22-00-991-002)

 1_ Remove the trim actuator (2) (Ref. TASK 27-22-51-000-001).
 2_ Turn the gimbal joint of the artificial-feel spring rod (1)
 until you can install and remove the rigging pin (4) and the
 bolt (11) easily.
 3_ Install the trim actuator (2) (Ref. TASK 27-22-51-400-001).

 Subtask 27-22-00-720-051
 B. Do the operational test of the rudder trim (Ref. TASK 27-22-00-710-002).
 5. Close-up
________ Subtask 27-22-00-860-057
 A. Put the aircraft back to its initial configuration.
 (1)
 Depressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-24-00-864-001) (Ref. TASK 29-10-00-864-003).

 (2)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 (3)
 Make sure that the work area is clean and clear of tool(s) and other items.

 1EFF : ALL 1 27-22-00Page 508 1 1 May 01/05R 1 1 1CES 1

 Subtask 27-22-00-410-050
 B. Close Access
 (1)
 Close the access doors 325BL, 325BR.

 (2)
 Remove the access platform(s).

 1EFF : ALL 1 27-22-00Page 509 1 1 Feb 01/03R 1 1 1CES 1

 TASK 27-22-00-710-001
 Operational Test of the Reset Function
 1. Reason for the Job
__________________
 Refer to the MPD TASK: 272100-01
 2. Job Set-up Information
______________________
 A. 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 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 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the
 Electric Pump 29-24-00-864-001 Depressurize the Yellow Hydraulic System 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure
 3. Job Set-up
__________
 Subtask 27-22-00-860-053
 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).

 (2)
 On the overhead panel 23VU, make sure that the FLT CTL/FAC 1 pushbutton switch is pushed (on this pushbutton switch, the FAULT and OFF legends are off).

 1EFF : ALL 1 27-22-00Page 510 1 1 Feb 01/03R 1 1 1CES 1

 (3) On the overhead panel 24VU, make sure that the FLT CTL/FAC 2

 pushbutton switch is pushed (on this pushbutton switch, the FAULT and

 OFF legends are off).
 (4)
 On the panel 110VU, make sure that the rudder trim is in the zero position.

 (5)
 Do the EIS start procedure (Ref. TASK 31-60-00-860-001).

 (6)
 Pressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-863-001) (Ref. TASK 29-24-00-863-001) (Ref. TASK 29-10-00-863-003).

 (7)
 On the center pedestal, on the ECAM control panel, push the F/CTL key (on the lower ECAM display unit, the F/CTL page comes into view).

 Subtask 27-22-00-865-051
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU AUTO FLT/FAC2/26VAC 14CC2 M18
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM FLIGHT CONTROLS 飛行操縱2(75)