(2)  
Access Panels
 1103L Forward Access Door
 1201L Forward Equipment Access Door
 4404R Forward Cargo Door

 D.  Prepare for the Removal
 S 864-002-C01
 (1)  
Remove pressure from the A and B hydraulic systems and reserviors (AMM 29-15-00/201).

 S 864-003-C01

 (2)  
Set the thrust levers to the IDLE position.

 (a)  Put a clamp on the cable.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH NON-REINFORCED CONTROL ú

 76-11-02
 STANDS  ú CONFIG 1 ú C01 Page 401 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 864-004-C01
 (3)  Set the start levers to the CUTOFF position.
 (a)  Put a clamp on the cables.
 S 864-005-C01
 (4)  
Loosen the turnbuckles in the lower nose compartment to remove the tension on the flap control cables WFA and WFB (AMM 27-09-14/201 for the location of the turnbuckles).

 S 494-006-C01

 (5)  
Install the rig pin through the control drum for the forward speed brake into the structure (Fig. 401).

 S 864-007-C01

 (6)  
Adjust the forward and aft support links to lift the forward mechanism (Fig. 402).

 NOTE: This will remove the tension on the stabilizer trim chain
____
 assembly.

 S 864-008-C01
 (7)  
Loosen the turnbuckles in the electronic equipment center to remove the tension on the thrust control cables T1A, T1B, T2A, T2B (AMM 76-11-04/201 for the location of the turnbuckle).

 S 864-009-C01

 (8)  
Loosen the turnbuckles in the forward cargo compartment to remove the tension on the engine start control cables (AMM 76-11-04/201 for the location the the turnbuckles).

 (a)  
Disconnect the cables for the start drums, as applicable to the start lever to be removed.

 (b)  
Attach a tag to the cables.

 E. Remove the Start Lever
 S 024-010-C01
 (1)  Do these steps to remove the start lever:
 (a)  Remove the tie rod nut on the trim control wheel for the left stabilizer (7, Fig. 403).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH NON-REINFORCED CONTROL ú

 76-11-02
 STANDS  ú CONFIG 1 ú C01 Page 402 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SPEED BRAKE ASSEMBLY
SEE A
FORWARD DRUM OF THE SPEED BRAKE ASSEMBLY
FLOOR
RIG PIN BOTTOM CONTROL ROD
LEVER FOR THE SPEED BRAKE CONTROL
TOP CONTROL ROD
IDLER
LINK
CHECK NUT
SPEED BRAKE ASSEMBLY
A

Speed Brake Control Lever Adjustment

Figure 401

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH NON-REINFORCED CONTROL ú

 76-11-02
 STANDS  ú CONFIG 1 ú C01 Page 403 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
CONTROL WHEELS OF STABILIZER
THE STABILIZER TRIM POSITION INDICATOR
CONNECTOR LINK SEE B
IDLER SPROCKET  IDLER 
CRANK  SPROCKET 
STABILIZER  AFT SUPPORT 
TRIM BRAKE  LINK 
STABILIZER  INDICATOR 
TRIM CHAIN  FLEXIBLE SHAFT 
FORCE POINT CHAIN DEFLECTION  DEFLECTION 5-POUND  CHAIN DEFLECTION 
　
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