S 424-018-C00
 (4)  Turn the quadrants clockwise until you can put the cable terminals in the grooves 2 and 3.
 (a)  
Put the cable terminals into their holes.

 (b)  
Bend the end of the retainers approximately 90 degrees to
 attach the cable terminals.

 S 424-019-C00
 (5)  
Turn the quadrants back to their initial position.

 S 424-020-C00

 (6)  
Install the two cable guards.

 S 424-021-C00

 (7)  
Push the torque switch mechanism up through the opening in the support structure.

 NOTE: The torque switch leads are in the aft direction.
____
 S 424-022-C00
 (8)  Engage the dowel pins in the support structure doubler.
 NOTE: Make sure the doubler is correctly installed.
____
 S 424-023-C00
 (9)  
Install the attach bolts and washers for the torque switch mechanism.

 S 424-025-C00

 (10)
 Make sure the T( )A cables engage the idler pulleys forward and aft of the torque switch mechanism.

 S 424-026-C00

 (11)
 Connect the leads of the torque switch to the adjacent terminal block.

 (12)
 Apply a thin layer of grease to the actuator output pinion.

 S 424-028-C00

 (13)
 Attach the actuator to the torque switch mechanism.

 S 914-027-C00
 (a)  Engage the actuator dowel pins with the holes in the torque
 switch mechanism.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(b)  Tighten the actuator attach screws.
 S 424-029-C00
 (14) Connect the T( )A and T( )B cables at the turnbuckles forward and aft of the torque switch mechanism.
 (a)  Apply a thin layer of the corrosion preventive compound to the internal and external threads of the turnbuckle.
 S 034-030-C00
 (15)
 Remove the cable clamps.

 S 734-031-C00

 (16)
 AIRPLANES WITHOUT THRUST REVERSER SYNC LOCKS;

 Install and adjust the throttle switches for the applicable engine. #
 (a)  
The throttle switches S139 and S283 for Engine No. 1 (AMM 27-62-04/401).

 (b)  
The throttle switches S133 and S140 for Engine No. 2 (AMM 27-62-04/401, AMM 31-26-11/401).

 S 734-039-C00
 (17) AIRPLANES WITH THRUST REVERSER SYNC LOCKS; Install and adjust the autothrottle assemblies for the applicable engine (AMM 27-62-04/401):
 (a)  
Engine No. 1, M1639

 (b)  
Engine No. 2, M1640

 S 734-032-C00
 (18)
 Adjust (rig) the thrust control cable forward and aft loops (AMM 76-11-00/501).

 S 724-033-C00

 (19)
 Do a test for the friction of the forward and reverse thrust control system (AMM 76-11-00/501).

 S 864-035-C00

 (20)
 Remove the DO-NOT-CLOSE tags and close these circuit breakers:

 (a)  P18-1 Panel
 1) AUTOTHROTTLE AC
 2) AUTOTHROTTLE DC

 (21)
 Do the BITE test for the autothrottle system (AMM 22-31-00/501).

 S 744-036-C00
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 76-11-03
 ALL  ú ú C02 Page 407 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
ENGINE CONTROL CABLES - MAINTENANCE PRACTICES
_____________________________________________
 1.  General
_______
 A.  The maintenance practices give the approximate location of the engine control cables in the fuselage, the wings and the strut.
 (1)  
This maintenance practices give the lengths and fittings of the engine control cables.
　
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