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 S 024-009-C00
 (4)  Loosen the actuator attachment screws and remove the actuator. (a) Hang the actuator from the support structure with a cord.
 S 034-010-C00
 (5)  AIRPLANES WITHOUT THRUST REVERSER SYNC LOCKS; Remove these throttle switches for the applicable engine. (a) The throttle switches S139 and S283 for Engine No. 1 (AMM 31-26-11/401, 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 034-040-C00
 (6)  AIRPLANES WITH THRUST REVERSER SYNC LOCKS; Remove the autothrottle assemblies for the applicable engine (AMM 27-62-04/401): (a) Engine No. 1, M1639 (b) Engine No. 2, M1640
 S 024-011-C00
 (7)  Remove the attachment bolts for the torque switch mechanism. (a) Lower the torque switch mechanism and the attached cables from the support structure. (b) Remove the cable guards from the torque switch mechanism.
 S 024-012-C00
 (8)  With your hand, turn the cable quadrants to get access to the cable terminals in grooves 1 and 4. (a) Bend the ends of the cable terminal retainers approximately 90 degrees to loosen the cable terminals. (b) Remove the cable terminals from the terminal holes and remove the cables from the quadrants.

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 76-11-03
 ALL  ú ú C02 Page 404 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 024-013-C00
 (9)  With your hand, turn the cable quadrants to get access to the cable terminals in grooves 2 and 3.
 (a)  
Bend the ends of the cable terminal retainers approximately 90 degrees to loosen the cable terminals.

 (b)  
Remove the cable terminals from the terminal holes and remove the cables from the quadrants.

 TASK 76-11-03-424-002-C00
 3.  Install the Autothrottle Torque Switch Mechanism________________________________________________
 A. Consumable Materials
 (1)  
Corrosion Preventive Compound - MIL-C-16173,
 Grade 2 (AMM 70-10-01/201)

 (2)  
Grease - MIL-G-81322 (AMM 70-10-01/201)

 B. References
 (1)  
AMM 12-31-11/201, Body Section Doors and Panels

 (2)  
AMM 22-31-00/501, Autothrottle System

 (3)  
AMM 27-62-04/401, Engine Throttle Switches

 (4)  
AMM 31-26-11/401, Thrust Lever Actuated Landing Gear Warning Switches

 (5)  
AMM 76-11-00/501, Engine Control System

 C. Access
 (1)  
Location Zone
 205 Electronic Compartment

 (2)  
Access Panel
 1201 Electronic Equipment Access Door

 

 D. Prepare to Install the Torque Switch Mechanism
 S 034-014-C00
 (1)  
Remove the cover from the actuator mounting face on the torque switch mechanism.

 S 034-015-C00

 (2)  
Remove the cable guards from the torque switch mechanism.

 E. Install the Torque Switch Mechanism
 S 424-037-C00
 (1)  
Turn the quadrants of the torque switch mechanism to get access to the cable terminal holes.

 S 424-038-C00

 (2)  
Install a new cable terminal retainer in each of the terminal holes in the quadrants.

 (a)  Use corrosion preventive compound to hold the retainers in the correct position.
 S 424-017-C00
 (3)  Turn the quadrants counterclockwise until you can put the cable terminals in the grooves 1 and 4.
 (a)  Put the cable terminals into their holes.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 76-11-03
 ALL  ú ú C01 Page 405 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(b)  Bend the end of the retainers approximately 90 degrees to
 attach the cable terminals.
　
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本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊 發(fā)動機(jī)控制 ENGINE CONTROLS(53)