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 76-11-01 STANDS WITH A STABLIZER TRIM SHAFT WITH ú CONFIG 3 A SELF-LOCKING INSERT-AND-BOLT ú C01 Page 401
 ú  Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 864-006-C03
 (5)  Put a protective cover on the Aft Electronics Panel, P8.
 NOTE: This will prevent damage to the switches and the glass
____
 surfaces of the indicators and the displays.

 S 014-007-C03
 (6)  
Remove the Captain and First Officer seats.

 S 014-008-C03

 (7)  
Open the access door to the lower nose compartment.

 S 864-009-C03

 (8)  
Release the tension on the flap control cables, WFA and WFB:

 (a)  Loosen the turnbuckles in the lower nose compartment
 (AMM 27-09-14/201 for turnbuckle location).

 S 864-010-C03
 (9)  
Install a rig pin through the control drum of the forward speed brake and into the structure (Fig. 401).

 S 864-011-C03

 (10)
 Turn the trim wheel for the left stabilizer until you can get access to the connector link in the stabilizer trim chain in the lower nose compartment.

 S 864-012-C03

 (11)
 Release the tension on the chain assembly:

 (a)  Adjust the forward support link to lift the forward mechanism in the lower nose compartment (Fig. 402).
 S 014-014-C03
 (12) Open the electronic equipment access door No. 1201 (AMM 12-31-11/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS-REINFORCED CONTROL ú
 76-11-01 STANDS WITH A STABLIZER TRIM SHAFT WITH ú CONFIG 3 A SELF-LOCKING INSERT-AND-BOLT ú C02 Page 402
 ú  Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SEE A
SPEED BRAKE CONTROL LEVER
UPPER CONTROL ROD
LOWER CONTROL ROD
IDLER
LINK
CHECK NUT
FLOOR
SPEED BRAKE FORWARD DRUM
A
RIG PIN
Speed Brake Control Lever Adjustment
Figure 401

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS-REINFORCED CONTROL ú

 76-11-01
 STANDS WITH A STABLIZER TRIM SHAFT WITH ú CONFIG 3 A SELF-LOCKING INSERT-AND-BOLT ú C01 Page 403 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
F13995
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
STABILIZER TRIM
CONTROL WHEELS

STABILIZER
POSITION
INDICATOR

STABILIZER TRIM INDICATOR LINKAGE
CONNECTOR LINK ARM SEE B
IDLERIDLER SPROCKET STABILIZER TRIM
SPROCKET INDICATOR CRANK
AFT SUPPORT
STABILIZER
LINK

TRIM BRAKE
INDICATOR
STABILIZER TRIM
FLEXIBLE SHAFT
CHAIN ASSEMBLY 5-POUNDCHAIN DEFLECTION
CHAIN DEFLECTION FORCE POINT
DEFLECTION
0.25(|0.07) INCHFORCESEE A
A
FORWARD TRIM
MECHANISM

4.5
SPROCKET
(|1.0)
INCHES
FORWARD

A
SUPPORT LINK

FWD
TURNBUCKLE
FORWARD TRIM MECHANISM SPROCKET
PIN
A
LINK
CONNECTOR LINK
B

Stabilizer Trim Chain Assembly Adjustment
Figure 402

F13996
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS-REINFORCED CONTROL ú

 76-11-01
 STANDS WITH A STABLIZER TRIM SHAFT WITH ú CONFIG 3 A SELF-LOCKING INSERT-AND-BOLT ú C01 Page 404 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
　
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