(8)  
Adjust the aft loop of the thrust control cable (AMM 76-11-00/501).

 S 824-022-C00

 (9)  
Adjust the thrust control push-pull cable (AMM 76-11-00/501).

 S 824-023-C00

 (10)
 Adjust the feedback push-pull cables for the thrust reverser (AMM 78-34-02/201).

 S 414-024-C00

 (11)
 Install the access panel No. 6301 (engine No. 1) or 6401 (engine No. 2) on the upper aft surface of the nacelle strut (AMM 12-31-71/201).

 S 864-028-C00

 (12)
 Remove the leading edge flap locks and retract the flaps (AMM 27-81-00/201).

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 76-11-05
 ALL  ú ú C01 Page 405 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 864-026-C00
 (13) Do the activation procedure for the thrust reverser (AMM 78-31-00/201).
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 76-11-05
 ALL  ú ú C01 Page 406 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
FUEL SHUTOFF ASSEMBLY - REMOVAL/INSTALLATION
____________________________________________
 1.  General
_______
 A.  This procedure has two tasks. They are the removal and the installation
 of the fuel shutoff assembly.

 B.  This procedure applies to the left and right installations. Differences
 are written in the procedure.

 TASK 76-11-06-004-001-C00
 2.  Fuel Shutoff Assembly Removal (Fig. 401)
_____________________________
 A.  References
 (1)  
AMM 12-31-71/201, Wing Upper Surface Access Doors and Panels

 (2)  
AMM 27-81-00/201, Leading Edge Flaps and Slats

 (3)  
AMM 76-11-04/201, Engine Control Cables

 (4)  
AMM 78-31-00/201, Thrust Reverser System

 B.  Access
 (1)  
Location Zones
 504/604 Thrust Reverser - Left
 505/605 Thrust Reverser - Right
 507/607 Strut

 (2)  
Access Panel
 6301/6401 LE Access Panel

 C.  Procedure
 S 044-002-C00
 WARNING: MAKE SURE THAT YOU INSTALL THE LOCKPIN IN THE CONTROL VALVE
_______ MODULE OF THE THRUST REVERSER. THE THRUST REVERSER CAN EXTEND AND CAUSE INJURY TO PERSONS OR DAMAGE TO THE EQUIPMENT.
 (1)  Install the lockpin in the control valve module of the applicable thrust reverser (AMM 78-31-00/201).
 S 044-027-C00
 WARNING: REFER TO AMM 27-81-00/201 FOR THE LEADING EDGE FLAP LOCK
_______ PROCEDURE. FLAPS MOVE VERY QUICKLY AND CAN CAUSE INJURY TO PERSONS.
 (2)  
Extend the flaps and install the leading edge flap locks
 (AMM 27-81-00/201).

 S 014-004-C00

 (3)  
Remove the access panel No. 6301 (engine No. 1) or 6401 (engine No. 2) from the upper aft surface of the nacelle strut (AMM 12-31-71/201).

 S 824-005-C00

 (4)  
Adjust the turnbuckles to release the tension in the ESS( )A and ESS( )B cables for the applicable engine. See AMM 76-11-04/201 for turnbuckle locations.

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 76-11-06
 ALL  ú ú C02 Page 401 ú Nov 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 ////////////////////////
SEEA B
PUSH-PULL CABLE RETAINER PIN
ESS1A CABLE
ESS1B
CABLE
START CONTROL
PUSH-PULL CABLE

CABLE RETAINER
　
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