(b)  
Adjust the Thrust Control Push-Pull Cables.

 (c)  
Adjust the Start Control Push-pull Cables.

 (d)  
Put the Airplane Back to Its Usual Condition.

 (2)
Engine Control-Cables Tension Adjustment which consists of:

 (a)  
Prepare for the Adjustment.

 (b)  
Adjust the Tension of the Thrust Control Cables.

 (c)  
Adjust the Tension of the Start Control Cables.

 (d)  
Put the Airplane Back to Its Usual Condition.

 B.  The third task is a system test which includes:
 (1)  Friction Test for the Engine Control System.
 TASK 76-11-00-835-001-C00
 2.  Engine Control System Rigging (Travel Adjustment)
_________________________________________________
 A.  General
 (1)  This procedure describes the adjustment (rigging) of the thrust and start control push-pull cables. You must do this adjustment after you replace the engine or the push-pull cables.
 B.  Equipment
 (1)  Kit - Rig Pin, F70207-93
 (a)  
Rig Pin - F70207-8 Optional: MS20392-4C pin (or equivalent 0.311 (+0.000/-0.0011 -inch diameter, 3-inch long rod or bolt)

 (b)  
Rig Pin - F70207-23 (2 required). Optional: MS20392-3C pin (or equivalent 0.248 (+0.00/-0.002)-inch diameter, 3-inch long rod or bolt).

 ú (2) Rig Pin - C76001-9
 (3)  
Protractor - 4MIT65B80307-1 or F52485-500

 (4)  
Set - Forward Thrust Lever Protractor/Adapter,
 F72952-15

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ////////////////////////
C. References
 (1)  
AMM 12-31-11/201, Body Section 41 Access Doors and Panels

 (2)  
AMM 12-31-71/201, Wing Upper Surface Access Doors and Panels

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

 (4)  
AMM 52-61-00/001, Forward Airstair

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

 (6)  
AMM 76-11-09/401, Start Control Push-Pull Cable

 (7)  
AMM 78-31-00/201, Thrust Reverser System

 (8)  
AMM 78-34-02/201, Feedback Push-Pull Cables

 D. Access
 (1)  
Location Zones
 101/102 Control Cabin, Left and Right
 205 Electronic Compartment
 208 Forward Cargo Compartment
 502/602 Fan Cowl - Left
 503/603 Fan Cowl - Right
 504/604 Thrust Reverser - Left
 505/605 Thrust Reverser - Right
 507/607 Strut Area

 (2)  
Access Panels
 4404 Forward Cargo Door
 6301/6401 Leading Edge Access Panel

 E. Prepare for the Adjustment
 S 045-094-C00
 WARNING: DO THE DEACTIVATION PROCEDURE 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
 (AMM 78-31-00/201).

 S 865-003-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 CAUSE INJURY TO PERSONS AND DAMAGE TO THE EQUIPMENT.
 (2)  AIRPLANES WITHOUT THROTTLE CONTROL CABLE TURNBUCKLES IN THE FUSELAGE; AIRPLANES PRE-SB 76-1023; Extend the leading edge flaps and install the flap locks (AMM 27-81-00/201).
 NOTE: Extend the leading edge flaps to get access to the
____
 control cable turnbuckles.

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