(3)
 Install the PITCH TRIM CONTROL LOCKING (98D27403500000) (7) on the center pedestal.

 Locking Tool - Pitch-Trim Control
 Figure 201/TASK 27-00-00-991-001
 1EFF :  ALL  1  27-00-00 Page 202 
1  1  Feb 01/98
 1  1
 1CES  1

 NOTE : The wheel (5) must be between the grooves of the two side
____
 plates (4).

 (4)
 Tighten the two nuts (3) until the two side plates (4) lock the wheel (5).

 (5)
 With the two screws (2), put the two stops (6) against the center pedestal so that the assembly cannot move.

 (6)
 Lower the cover (1).

 TASK 27-00-00-080-001
 Removal of the Pitch-Trim Control Locking Tool (98D27403500000)

 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-00-00-991-001 Fig. 201
 3. Job Set-up
__________ (Ref. Fig. 201/TASK 27-00-00-991-001) Subtask 27-00-00-860-050
 A. Not applicable
 4. Procedure
_________ Subtask 27-00-00-080-050
 A. Removal of the Pitch-Trim Control Locking Tool
 (1)
 Lift the cover (1).

 (2)
 Loosen the two screws (2).

 (3)
 Fully loosen the two nuts (3).

 (4)
 Remove the PITCH TRIM CONTROL LOCKING (98D27403500000) (7).

 TASK 27-00-00-480-002
 Installation of the Flap/Slat Control-Lever Locking Tool (98D27803000000)

 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-00-00-991-002 Fig. 202
 3. Job Set-up
__________ (Ref. Fig. 202/TASK 27-00-00-991-002) Subtask 27-00-00-860-052
 A. Not applicable
 4. Procedure
_________ Subtask 27-00-00-480-051
 A. Installation of the Flap/Slat Control-Lever Locking Tool
 (1)
 Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000)

 (2) on the flap/slat control lever (1).

 (2)
 Lock the locking tool with the pin (3).
 (Ref. Fig. 202/TASK 27-00-00-991-002)

 Flap/Slat Control-Lever Locking Tool
 Figure 202/TASK 27-00-00-991-002
 1EFF :  ALL  1  27-00-00 Page 206 
1  1  Feb 01/98
 1  1
 1CES  1

 TASK 27-00-00-080-002
 Removal of the Flap/Slat Control-Lever Locking Tool (98D27803000000)
 1. Reason for the Job__________________
 Self Explanatory
 2. Job Set-up Information______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
98D27803000000  1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER 
R  B. Referenced Information 
R R R  -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R  27-00-00-991-002  Fig. 202
 3. Job Set-up__________
 Subtask 27-00-00-860-051
 A. Not applicable
 4. Procedure_________
 Subtask 27-00-00-080-051
R  A. Removal of the Flap/Slat Control-Lever Locking Tool (Ref. Fig. 202/TASK 27-00-00-991-002)
 (1) Remove the pin (3) from the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) (2).
 (2) Remove the locking tool (2) from the flap/slat control lever (1).
　
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1(73)