25.81 lbf.ft). Do not safety the lock nut (2) at this time.
 (f) Make sure that the adjustment does not change when you TORQUE the lock nut.

 (3)
 Make sure that you can easily engage and disengage the rigging pin into the elevator position transducer unit (1). (Ref. Fig. 502/TASK 27-34-00-991-009)

 (4)
 Set the servocontrol to the damping mode.

 FOR 34CE1, 34CE2
 -Release the FLT CTL/ELAC 2 pushbutton switch (on this pushbutton switch, the OFF legend comes on).
 -The FLT CTL/ELAC 1 pushbutton switch is pushed (on this pushbutton switch, the OFF and FAULT legends are off).
 FOR 34CE3, 34CE4
 -Push the FLT CTL/ELAC 2 pushbutton switch (on this pushbutton switch, the OFF legend goes off).
 (5)
 Make sure that the elevator trailing edge position has not changed. If you see a position variation, do the adjustment of the servocontrol again.

 (6)
 Safety the lock nut (2) with Lockwire-corrosion resistant steel dia

 0.8 mm (0.03 in.).

 (7)
 Preparation for the Test

 (a) FOR 34CE1, 34CE2
 -
Push the FLT CTL/ELAC 2 pushbutton switch (on this pushbutton switch, the OFF legend goes off).

 FOR 34CE3, 34CE4

 -
Push the FLT CTL/ELAC 1 pushbutton switch (on this pushbutton switch, the OFF legend goes off).

 (b)
 Remove the rigging pin from the CAPT and F/O side stick
 controllers.

 (c)
 Remove the rigging pin (5) from the screw jack of the THS
 actuator (6).

 1EFF : ALL 1 27-34-00Page 531 1 1 Aug 01/00R 1 1 1CES 1

 Subtask 27-34-00-710-055
 B. Test
 (1) Do the operational test of the elevators (Ref. TASK 27-34-00-710-001).
 5. Close-up
________
 Subtask 27-34-00-860-066

 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)
 Remove the warning notice(s).

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

 (4)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 Subtask 27-34-00-410-059
 B. Close Access
 (1) Close the access door 312AR.
R (2) Close the THS trailing edge access panels (Ref. TASK 55-13-11-400-R 001):
 (a)
 334CB, 334DB for the left elevator.

 (b)
 344CB, 344DB for the right elevator.

 (3)
 Install the protective cover on the battery power center 105VU.

 (4)
 Tighten the two screws.

 (5)
 Close the access door 822

 (6)
 Remove the access platform(s).

 TASK 27-34-00-820-003
 Adjustment of the Elevator and Hydraulic Actuation to 0.5 Degrees Nose-Up with the Gauge-Elevator Neutral Setting (98D27309006000)
 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 TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
 MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
 DAMAGE.

 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific threaded pins
 No specific warning notice
 No specific warning notices
 No specific access platform 1.6 m (5 ft. 3 in.)
 No specific access platform 2.8 m (9 ft. 2 in.)
 No specific access platform 5.35 m (17 ft. 7 in.)
 No specific Torque Wrench : range 0.20 to 3.60 m.daN

 (2.00 to 26.00 lbf.ft)
 0U190360 1 PIN - RIGGING R 98D27303000001 1 LOAD APPLICATION TOOL - ELEVATOR, AILERON, RUDDER R 98D27309006000 1 GAUGE-ELEVATOR NEUTRAL SETTING
 98D27903500000 2 PIN-SIDE STICK LOCKING B. Consumable Materials

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