76-11-04
 ALL  ú ú C02 Page 202 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(2)  Extend the leading edge flaps and install the flap locks
 (AMM 27-81-00/201).

 NOTE: You must extend the leading edge flaps to get access to the
____ engine control cables between the fuselage and the strut.
 S 012-004-C00
 (3)  You can get access to the engine control cables and the components of the engine control system through the access doors and panels in the fuselage and the wing.
 (a)  
Open the access door, 1103L, to get to the thrust lever and the start lever drums that are below the control stand.

 (b)  
Open the access door, 1201L, to get access to the forward fuselage turnbuckles and the two autothrottle mechanisms that are above the electronic equipment shelves.

 (c)  
Go into the forward cargo compartment, through the forward cargo door, 4404R, to get access to the aft fuselage turnbuckles through the cargo compartment ceiling (AMM 25-52-65/401).

 (d)  
For the left wing, open the access panel 6301L, to get access to the left wing cables at the strut control box.

 (e)  
For the right wing, open the access panel 6401R, to get access to the right wing cables at the strut control box.

 (f)  
For the left wing, open the access panel 6302L, to get access to the left wing cables at the wing leading edge.

 (g)  
For the right wing, open the access panel 6402R, to get access to the right wing cables at the wing leading edge.

 S 212-005-C00
 (4)  If you must examine the control cables and the cable pulleys, do this procedure:
 (a)  Refer to AMM 20-20-31/601 for the procedure to examine the control cable and the control cable pulleys.
 S 022-006-C00
 (5) If you must replace the thrust control cables, do these procedures:
 (a)  
Refer to AMM 20-10-04/401, for the procedure to remove the control cable air seals 1) Remove Access panel 3478R to get access to the air seals.

 (b)  
Refer to AMM 20-10-41/401 for the procedure to remove the control cable grommets.

 (c)  
Refer to AMM 20-10-10/401 for the procedure to remove the locking clip on the control cable turnbuckles.

 (d)  
Refer to AMM 20-10-91/401 for the procedure to remove the thrust control cables.

 TASK 76-11-04-402-013-C00
 3. Install the Engine Control Cables
_________________________________
 A. References
 (1)  AMM 12-26-00/301, Cable Lubrication
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 76-11-04
 ALL  ú ú C03 Page 203 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(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

 (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
　
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