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R  Cut the two rear cables by 75 mm (2.95 in.)
 (3) Use the measured clearance between the turnbuckles and the static fairleads to cut the rear cable junction by the calculated value.
 NOTE : Cut the two rear cables by the same value.____
 (4) Install the new turnbuckles on the cables (Ref. CFM Cable Fabrication Man).
 (5) Do the adjustment of the THS control-cables length (Ref. TASK 27-41-00-820-002).
 (6) Make sure that the clearances 'A' between the two turnbuckles and the fairleads is minimum 25.4 mm (1.00 in.) along the full travel range of the THS control.
 (7) Make sure that the distance 'B' between the ends of the turnbuckles in each THS control cable is minimum 90 mm (3.54 in.) in all the positions.
 (8) Make sure that the turnbuckles are in the adjustment range of 38.2 mm (1.50 in.).

 

 5. Close-up
________ Subtask 27-41-00-860-065
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Remove the special and standard tools and all other items.

 1EFF : ALL 1 27-41-00Page 543 1 1 May 01/04R 1 1 1CES 1

 TASK 27-41-00-820-004
 Cutting of the Rear Control Cable of the THS
 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.
 CAUTION : MAKE SURE THAT THE AIRCRAFT IS IN THE TEMPERATURE CONDITIONS (STABLE
_______ AMBIENT TEMPERATURE) SPECIFIED IN THE AIRCRAFT MAINTENANCE CONFIGURATION PARAGRAPH. CHANGES IN THE TEMPERATURE CAN CAUSE INCORRECT MEASUREMENTS.
 1. Reason for the Job
__________________
 Do this procedure when you install a new rear control cable on the THS.
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific thermometer No specific warning notice No specific access platforms 2.3 m (7 ft. 7 in.) 0U190360 1 PIN - RIGGING 98D27407532000 1 RIGGING PIN - THS MECHANICAL CONTROL
 1EFF : ALL 1 27-41-00Page 544 1 1 May 01/04R 1 1 1CES 1

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-33-21-618-001 Pre-conditioning through the LP Ground Connection CFM Cable Fabrication Man 27-41-00-991-006 Fig. 505

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 27-41-00-991-011 Fig. 509
 **ON A/C 301-399,

 27-41-00-991-011-A Fig. 509A
 **ON A/C ALL

 3. Job Set-up
__________
 Subtask 27-41-00-010-063

 A. Get Access
 (1)
 Make sure that the access platforms are in position at the cargo compartment doors 825 and 826.

 (2)
 Make sure that the cargo compartment doors 825 and 826 are open.

 (3)
 In the zone 241, make sure that the floor panels 241FF and 241BF are removed.

 (4)
 In the zone 131, make sure that the partition panel 131PW is removed.

 

 Subtask 27-41-00-860-068
 B. Aircraft Maintenance Configuration NOTE : Let the temperature in the aircraft become stable for three hours
____
 before you start this procedure.

 (1)
 Make sure that the air conditioning system does not operate (Ref. TASK 12-33-21-618-001).

 (2)
 Make sure that there is no neon light on, near the cable, in the cable routing zone.

 (3)
 Make sure that the pitch-trim control wheels are in the '0' position.

 (4)
 Put a warning notice in position in the cockpit to tell persons not to operate the pitch trim.

 (5)
 Make sure that the PIN - RIGGING (0U190360) (5) is in position on the mechanical input of the THS actuator (1).

 (6)
 Make sure that the RIGGING PIN - THS MECHANICAL CONTROL (98D27407532000) (11) is in position on the tension regulator (2).

 4. Procedure
_________ (Ref. Fig. 505/TASK 27-41-00-991-006) R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
　
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