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THE FLIGHT CONTROLS
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THE FLIGHT CONTROL SURFACES
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THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
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GEAR.
1. Reason for the Job
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Refer to the MPD TASK: 271400-02
2. Job Set-up Information
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A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notices No specific access platform 4.2 m (13 ft. 9 in.) 97A27003000000 1 GAGE ASSY - PUSH-PULL 97A27003000001 1 GAGE ASSY - PUSH-PULL 97A27902016000 1 SPRING SCALE ASSY 98D27303000001 1 LOAD APPLICATION TOOL - ELEVATOR, AILERON, RUDDER 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
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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. 27-14-41-200-001 Inspection/Check of the Aileron
R 27-14-51-000-001 Removal of the Aileron Servo Control 27-14-51-200-001 Check of the Aileron Servo Control
R 27-14-51-400-001 Installation of the Aileron Servo Control 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 27-14-00-991-004 Fig. 601
3. Job Set-up
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Subtask 27-14-00-865-050
A. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
Subtask 27-14-00-860-050
B. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
On the center pedestal, make sure that the flap and slat control lever is in the O position.
(3)
On the center pedestal, make sure that the speedbrake control lever is in the RET position.
(4)
On the overhead panel 23VU, make sure that the FLT CTL/ELAC 1 pushbutton switch is pushed (on this pushbutton switch, the FAULT and OFF legends are off).
Subtask 27-14-00-010-055
C. Get Access
(Ref. Fig. 601/TASK 27-14-00-991-004)
(1)
Put the access platform in position at zone 575 for the left aileron.
(2)
Open the access doors 575KB, 575MB, 590AB, 590BB.
(3)
Put the access platform in position at zone 675 for the right aileron.
(4) Open the access doors 675KB, 675MB, 690AB, 690BB.
Subtask 27-14-00-480-050
D. Installation of the tools.
(1)
Lock the 2 side stick controllers with the PIN-SIDE STICK LOCKING (98D27903500000).
(2)
Put the warning notices on the CAPT and F/O side sticks to tell persons not to touch the side sticks.
(3)
Install the LOAD APPLICATION TOOL - ELEVATOR, AILERON, RUDDER (98D27303000001) as follow:
-at the trailing edge of the aileron
-between the two servo controls.
R (4) Install the CHECK TOOL - AILERON, ELEVATOR, RUDDER (98D27303003001) R or CHECK TOOL (ORAP) - AILERON, ELEVATOR, RUDDER (98D27303022000) on R the trailing edge of the aileron.
(Ref. Fig. 601/TASK 27-14-00-991-004)
Adjust the spindle of the dial indicator to its mid travel.
Subtask 27-14-00-863-062
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