(3)
Remove the warning notice(s).
(4)
Remove the PIN-SIDE STICK LOCKING (98D27903500000) from the CAPT and F/O side sticks. Remove the F/O side sticks.
1EFF : ALL 1 27-34-00Page 624 1 1 Feb 01/05R 1 1 1CES 1
(5) Make sure that the work area is clean and clear of tool(s) and other items.
(6) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
Subtask 27-34-00-410-058
B. Close Access
R R (1) Close the THS trailing edge access panels 334DB, 344DB (Ref. TASK 55-13-11-400-001).
(2) Remove the access platform(s).
TASK 27-34-00-200-002
Check of the Elevator Servo Control Oscillations.
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 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 warning notices
No specific access platform 5.2 m (17 ft. 1 in.)
98D27303003001 1 CHECK TOOL - AILERON, ELEVATOR, RUDDER
R 98D27303022000 1 CHECK TOOL (ORAP) - AILERON, ELEVATOR, RUDDER 98D27903500000 2 PIN-SIDE STICK LOCKING
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 27-34-51-000-008 Removal of the Elevator Servo Control Actuator Servo Valve 27-34-51-400-003 Installation of the Elevator Servo Control Actuator Servo Valve 29-10-00-863-001 Pressurize the Green Hydraulic System
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground Power Supply 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 27-93-34-000-001 Removal of the ELAC (2CE1,2CE2) (for corrective
action) 27-93-34-400-001 Installation of the ELAC (2CE1,2CE2) (for corrective action)
3. Job Set-up
__________
Subtask 27-34-00-860-058
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
(2)
Put the PIN-SIDE STICK LOCKING (98D27903500000) on the CAPT and F/O side sticks.
(3)
Put the warning notices on the CAPT and F/O side sticks to tell persons not to touch the side sticks.
(4)
Put the warning notices on the center pedestal, to tell persons not to touch the pitch-trim control wheel.
(5)
On the panel 23VU:
-make sure that the FLT CTL/ELAC 1 pushbutton switch is pushed (on this pushbutton switch, the OFF and FAULT legends are off).
(6)
On the panel 24VU:
-make sure that the FLT CTL/ELAC 2 pushbutton switch is pushed (on this pushbutton switch, the OFF and FAULT legends are off).
(7)
Pressurize the Green hydraulic system
(Ref. TASK 29-10-00-863-001).
1EFF : ALL 1 27-34-00Page 627 1 1 May 01/04R 1 1 1CES 1
Subtask 27-34-00-480-053
B. Installation of the Tools
(1) Put the access platform at the zone 334, 344.
R R R R (2) Install the CHECK TOOL - AILERON, ELEVATOR, RUDDER (98D27303003001) or CHECK TOOL (ORAP) - AILERON, ELEVATOR, RUDDER (98D27303022000) on the rear cone, near the trailing edge of the elevator (left or right side).
R R R (3) Put the pointer of the CHECK TOOL - AILERON, ELEVATOR, RUDDER (98D27303003001) or CHECK TOOL (ORAP) - AILERON, ELEVATOR, RUDDER (98D27303022000) at the trailing edge of the elevator.
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 FLIGHT CONTROLS 飞行操纵3(46)
