76-11-07
 ALL  ú ú C01 Page 405 ú Jul 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 864-010-C00
 (9)  
Install the F70207-23 rig pin through the R rig pin hole into gear in the main engine control (MEC) control box.

 S 024-011-C00

 (10)
 Remove the push-pull cable.

 (a)  
Disconnect the push-pull cable from the strut drum control box. 1) Remove the disconnect clamp at the strut drum control box. 2) Remove the push-pull cable core from the control box rack.

 (b)  
Open the clamp blocks in the strut structure and the fan cowl support beam to release the push-pull cable.

 (c)  
Remove the clamp from the push-pull cable in the fan cowl support beam.

 (d)  
Remove the penetration fitting from the fan cowl support beam.

 (e)  
Open the five quick-release clamps on the engine brackets to remove the push-pull cable.

 (f)  
Remove the push-pull cable from the fuel control box on the main engine control (MEC). 1) Remove the disconnect clamp at the MEC fuel control box.

 (g)  
Remove the push-pull cable from the control box rack.

 (h)  
Pull the push-pull cable down from the opening in the fan cowl support beam.

 TASK 76-11-07-404-012-C00
 3. Install the Thrust Control Push-Pull Cable
__________________________________________
 A. Equipment
 (1)  
Rig Pin - F70207-8
 Component of Rig Pin Kit F70207-93.
 Optional: MS20392-4C pin or equivalent 0.311
 (+0.000/-0.002)-inch diameter,
 3-inch long rod or bolt

 (2)  
Rig Pin Assembly - F70207-23.
 Component of Rig Pin Kit F70207-93.
 Optional: MS20392-3C pin (or equivalent 0.248
 (+0.000/-0.002)-inch diameter, 3-inch long rod
 or bolt)

 B. Consumable Materials
 (1)  Sealant - DC93-006-1 (AMM 70-10-01/201)
 C. References
 (1)  
AMM 12-31-71/201, Wing Upper Surface Access Doors and Panels

 (2)  
AMM 12-31-91/201, Nacelle and Engine-To-Wing Access Doors and Panels

 (3)  
AMM 27-81-00/201, Leading Edge Flap and Slat Control System

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 76-11-07
 ALL  ú ú C01 Page 406 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(4)  
AMM 54-32-01/401, Forward Fairing

 (5)  
AMM 71-11-02/201, Fan Cowl Panels

 (6)  
AMM 78-31-00/201, Thrust Reverser System

 D.  Access
 (1)  
Location Zones
 5700, Engine No. 1 (Left)
 5800, Engine No. 2 (Right)

 (2)  
Access Panels
 5726L, Strut Access Door, Eng. No. 1 - left
 5727L, Strut Access Door, Eng. No. 1 - top
 5728L, Strut Access Door, Eng. No. 1 - top
 5729L, Strut Access Door, Eng. No. 1 - top
 5731L, Strut Access Door, Eng. No. 1 - right
 5746L, Fan Cowl Panel, Eng. No. 1 - left
 5826R, Strut Access Door, Eng. No. 2 - left
 5827R, Strut Access Door, Eng. No. 2 - top
 5828R, Strut Access Door, Eng. No. 2 - top
 5829R, Strut Access Door, Eng. No. 2 - top
 5831R, Strut Access Door, Eng. No. 2 - right
 5846R, Fan Cowl Panel, Eng. No. 2 - right

 E.  Install the thrust control push-pull cable.
 S 424-013-C00
 (1)  Install the push-pull cable (Fig. 401).
 (a)  
Install the upper end of the push-pull cable up through the opening in the fan cowl support beam.

 (b)  
Push the cable aft through the fan cowl support beam and the strut structure to the strut drum control box.

 (c)  
Connect the push-pull cable to the strut drum control box. 1) Connect the push-pull cable to the rack of the strut drum control box. 2) Install the disconnect clamp on the push-pull cable and the

 control box rack. 3) Install the lockwire on the clamp screws.
　
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