(2)  
The cable references are from end fitting to end fitting.

 (3)  
The T1A and T2A cables control the increase of the forward thrust.

 (4)  
The T1B and T2B cables control the decrease of the forward thrust.

 (5)  
The ESS1A and ESS2A cables control the engine start and the fuel to the run position.

 (6)  
The ESS1B and ESS2B cables control the engine shutdown and fuel to the cutoff position.

 B.  There are two sets of thrust control and start control cables.
 (1)  
The optional control cables will put the turnbuckles for the thrust control cables and the engine start cables behind the wing leading edge.

 (a)  
The following cables are installed on these airplanes. 1) Line no. 1001 - 1999 have the optional start control cables. 2) Line no. 2000 and on has the recommended start control cables. 3) Line no. 1001 - 1998 has the optional thrust control cables.

 4)  Line no. 1999 and on has the recommended thrust control cables.

 (b)  
The airplanes without SB 76-1023 or SL 76-15 have the optional control cables.

 (2)  
The recommended control cables will move the turnbuckles for the thrust control cables and the engine start cables from the wing to the fuselage.

 (a)  
The airplanes with SB 76-1023 have the recommended T1A/T2A/T1B/T2B control cables.

 (b)  
The airplanes with SL 76-15 have the recommended ESS1A/ESS1B/ESS2A/ESS2B control cables.

 TASK 76-11-04-002-001-C00
 2.  Remove the Engine Control Cables
________________________________
 A.  References
 (1)  
AMM 12-26-00/301, Cable Lubrication

 (2)  
AMM 12-31-11/201, Body Section 41 Access Doors and Panels

 (3)  
AMM 12-31-21/201, Body Section 43 Access Doors and Panels

 (4)  
AMM 12-31-61/201, Wing Lower Surface Access Doors and Panels

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 76-11-04
 ALL  ú ú C01 Page 201 ú Mar 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(5)  
AMM 12-31-91/201, Nacelle and Engine-to-Wing Fairing Access Doors and Panels

 (6)  
AMM 20-10-04/401, Control Cable Air Seal

 (7)  
AMM 20-10-10/401, Turnbuckle Locking Clips

 (8)  
AMM 20-10-41/401, Control Cable Grommet

 (9)  
AMM 20-10-91/401, Control Cables

 (10)
 AMM 20-20-31/601, Control Cables

 (11)
 AMM 25-52-65/401, Cargo Compartment Ceiling Lining

 (12)
 AMM 27-81-00/201, Leading Edge Flaps and Slats Control System

 (13)
 AMM 76-11-00/501, Engine Control System

 (14)
 AMM 78-31-00/201, Thrust Reverser System

 B. Access
 (1)  
Location Zones
 203 Lower Nose Compartment
 205 Electronic Compartment
 208 Forward Cargo Compartment
 209 Forward Cargo Door
 303/403 Wing Leading Edge
 507/607 Strut Area

 (2)  
Access Panels
 1103L Forward Access Door
 1201L Electronic Equipment Access Door
 4404R Forward Cargo Door
 6301L Leading Edge Access Door
 6401R Leading Edge Access Door
 6302L Front Spar Access Panel
 6402R Front Spar Access Panel

 C. Remove the Engine Control Cables
 S 042-002-C00
 WARNING: DO THE DEACTIVATION PROCEDURE FOR THE THRUST REVERSER TO
_______ PREVENT THE OPERATION OF THE THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO THE EQUIPMENT.
 (1)  Do the deactivation procedure for the thrust reverser for ground maintenance (AMM 78-31-00/201).
 S 042-015-C00
 WARNING: REFER TO AMM 27-81-00/201 FOR THE INSTALLATION OF THE LOCK FOR
_______ THE LEADING EDGE FLAP. THE FLAPS CAN MOVE QUICKLY AND CAN CAUSE INJURY TO PERSONS AND DAMAGE TO THE EQUIPMENT.
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