(13)
 Turn the srew (28) to increase the tension of the chain (22).

 (14)
 Attach the dynamometer to item (24).

 (15)
 With the dynamometer, apply a force of 1.1 daN (2.4728 lbf) in the up direction at 90 degrees to the chain section and make sure that the end of item (24) is in the range of item (25) (Ref. detail D).

 (16)
 Turn the screw (28) to adjust the chain tension if necessary.

R (17) Remove the dynamometer and items (24) and (25) of the CHECKING TOOL -R CHAIN TENSION, PITCH TRIM CTL WHEEL (98D27403002002).
 (18)
 Tighten the nut (27). Make sure that the screw (28) does not turn.

 (19)
 Safety the nut (27) and the screw (28) with lockwire corrosion resistant steel dia 0.8 mm (0.03 in.).

 (20)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (21)
 Install the lateral panel.

 (22)
 Install the radio management panel (1RG1) (Ref. TASK 23-13-13-400-001), the audio control panel (2RN1) (Ref. TASK 23-51-12-400-001), the panel 111VU (Ref. TASK 31-10-00-700-001) and the weather radar control unit (3SQ) (Ref. TASK 34-41-12-400-001).

 Subtask 27-41-43-720-050
 C. Test
 (1)
 Remove the HOLDING TOOL-TRIM CTL LOWER SHAFT (98D27403000000) from the drive shaft (23).

 (2)
 Remove the standard locking bolt from the chain (1). (Ref. Fig. 401/TASK 27-41-43-991-002)

 (3)
 Remove the PITCH TRIM CONTROL LOCKING (98D27403500000) from the pitch-trim control wheels.

 (4)
 Do the functional test of the THS-actuator overfull travel with reference to the mechanical indicator (Ref. TASK 27-41-00-720-001).

 5. Close-up
________
 Subtask 27-41-43-942-050

 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Close the access door 811.

 (3)
 Remove the access platform(s).

 CABLES - THS CONTROL - REMOVAL/INSTALLATION
___________________________________________
 TASK 27-41-44-000-001
 Removal of the THS Control Cables
 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 warning notices
 No specific access platform 1.5 m (4 ft. 11 in.)
 No specific access platform 1.6 m (5 ft. 3 in.)
 No specific access platform 2.8 m (9 ft. 2 in.)
 0U190360 1 PIN - RIGGING
 98D27403500000 1 PITCH TRIM CONTROL LOCKING

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-54-12-000-002 25-55-11-000-002 25-55-12-000-002 29-23-00-863-001 29-23-00-864-001 29-24-00-863-001 29-24-00-864-001 53-12-11-000-001  Removal of the Ceiling Panels in the FWD Cargo CompartmentRemoval of the Ceiling Panels in the AFT Cargo Compartment - FR47/FR59Removal of the Ceiling Panels in the AFT Cargo Compartment - FR59/FR65Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric PumpDepressurize the Green and Yellow Hydraulic Systems after Operation of the PTUPressurize the Yellow Hydraulic System with the Electric PumpDepressurize the Yellow Hydraulic SystemRemoval of the Cockpit Floor Panels from FR1 Thru FR12
 53-12-12-000-001  Removal of the Cabin Floor Panels from FR12 thru FR24
 53-22-12-000-001  Removal of the Cabin Floor Panels
 53-32-12-000-002  Removal of the Cabin Floor Panels

 **ON A/C 001-049, 051-099, 101-149, 201-299, 27-41-44-991-001 Fig. 401

R **ON A/C 151-199, 401-499,
 27-41-44-991-001-A Fig. 401A
 **ON A/C 301-399,
　
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