C. Shift one tooth between the gear just after the pitch-trim gearset unit and the chain/cable to the THS.
 D. Install the chain on the pinion.
 E. Adjust the trim control wheel (Ref. TASK 27-41-00-820-002).
 F. Adjust the tension of the cable (Ref. TASK 27-41-00-820-002).
 G. Make sure that you touch the stop of the THS actuator mechanical input before the stop of the pitch-trim control wheel.

 5.
 Close-up

________
 Subtask 27-41-00-860-055
 A. Put the aircraft back to its initial configuration.
 (1)
 Depressurize the Green and Yellow hydraulic systems (Ref. TASK 29-23-00-864-001) and (Ref. TASK 29-24-00-864-001).

 (2)
 Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).

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

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 (4)
 Remove the access platform(s).

 (5)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

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 TASK 27-41-00-730-001 System Test of the THS Actuator Electrical Control 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 FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______ NOTICES ARE IN POSITION.
 WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
 WARNING : MAKE SURE THAT THE CONTROLS AGREE WITH THE POSITION OF THE ITEMS THEY
_______ OPERATE BEFORE YOU PRESSURIZE A HYDRAULIC SYSTEM.
 1. Reason for the Job__________________ Self Explanatory
 2. Job Set-up Information______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific access platform 1.6 m (5 ft. 3 in.)
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 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
 29-10-00-863-003  Pressurize the Blue Hydraulic System with a Ground Power Supply
 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 27-41-00-860-050
 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/ELAC 1 and FLT CTL/SEC 1 pushbutton switches are pushed (On these pushbutton switches, the OFF and FAULT legends are off).

 (3)
 On the overhead panel 24VU:

 -make sure that the FLT CTL/ELAC 2 and FLT CTL/SEC 2 pushbutton switches are pushed (On these pushbutton switches, the OFF and FAULT legends are off).

 (4)
 Do the EIS start procedure (Ref. TASK 31-60-00-860-001).

 (5)
 On the center pedestal, on the ECAM control panel, push the F/CTL pushbutton switch. (On the lower ECAM display unit, the F/CTL page comes into view).

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 (6) Pressurize the Green, the Yellow and the Blue hydraulic systems. (Ref. TASK 29-23-00-863-001) (Ref. TASK 29-24-00-863-001) (Ref. TASK 29-10-00-863-003)
 Subtask 27-41-00-010-060
 B. Get Access
　
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