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时间:2011-04-08 12:04来源:蓝天飞行翻译 作者:航空
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F14020
 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 409 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
A

A
FWD
STABILIZER LEFT STABILIZER
TRIM CHAIN
TRIM CONTROL GUARDNO. 1
WHEEL NO. 2
THRUST STARTSTABILIZER BEARING LEVER LEVER
TRIM SPLINED (3 LOCATIONS)
CONTROL SHAFT NO. 1 NO. 2

BUSHINGSPACER
START THRUST (4 LOCATIONS)
LEVER LEVER
//////////////////////// / /
CFM56 ENGINES
/ / ////////////////////////
RIGHT STABILIZER
STABILIZER TRIM WHEEL
TRIM CHAIN
SPROCKET CONTROL STAND FRAME
FLAP LEVER
AND CABLE
DRUM

SHIM  SHIM 
SHAFT CONTROL LONG BUSHING  (2 LOCATIONS) SHIM A-A SHIM STAND CONTROL FRAME FRAME STAND CONTROL (3 PLACES) SHIM FRAME STAND CONTROL SHIM WASHER NUT AND CUP CONTROL SHAFT LONG SHAFT CONTROL SHORT  BUSHING  NUT AND CUP CONTROL SHAFT SHORT WASHER 
Figure 404 (Sheet 2) Control Shaft Components Installation 

F14051
 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 410 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////

Control Shaft Components Installation Figure 404 (Sheet 3)
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 411 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
F14025
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
GAP LOCATION  GAP REQUIREMENT  ACTUAL MEASUREMENT  TO OBTAIN GAP REQUIREMENT ADJUSTMENT NECESSARY 
1  FLAP LEVER  0.060 MIN  LESS THAN 0.060  RELOCATE ONE WASHER FROM TO7 6 
2  SPEEDBRAKE LEVER  0.030-0.060  GREATER THAN 0.100  RELOCATE THREE WASHERS FROM TO2 1 
0.080-0.100  RELOCATE TWO WASHERS FROM TO 12 
0.060-0.080  RELOCATE ONE WASHER FROM TO 12 
LESS THAN 0.030  RELOCATE ONE WASHER FROM TO1 2 
3  THRUST LEVER ENGINE NUMBER 1  0.025-0.054  GREATER THAN 0.054  RELOCATE ONE WASHER FROM TO4 3 
LESS THAN 0.025  RELOCATE ONE WASHER FROM TO3 4 
4  ENGINE START DETENT ENGINE NUMBER 1  0.036-0.090  GREATER THAN 0.090  ADD TWO SHIMS MAX (AS REQUIRED) AT 8 
LESS THAN 0.036  REMOVE ONE SHIM AT 8 
5  ENGINE NUMBER 2 THRUST LEVER 0.0325-0.0540  GREATER THAN 0.0540  RELOCATE ONE WASHER FROM TO4 5 
LESS THAN 0.0325  RELOCATE ONE WASHER FROM TO5 4 
6  ENGINE NUMBER 2 ENGINE START DETENT 0.022-0.086  GREATER THAN 0.086  ADD THREE SHIMS MAX (AS REQUIRED) AT 9 
LESS THAN 0.022  REMOVE ONE SHIM AT 9 

CONTROL SHAFT ADJUSTMENT GAP REQUIREMENTS
TABLE A

LOCATION  QUANTITY OF WASHERS/SHIMS 
MAX  MIN 
1 4  0 
2  4  0 
3  2  0 
4  4  1 
5  2  0 
6  1  0 
7  1  0 
8  3  0 
9  4  0 

CONTROL SHAFT ADJUSTMENT SHIM REQUIREMENTS
TABLE B

Control Shaft Components Installation
Figure 404 (Sheet 4)

F14023
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS-REINFORCED CONTROL ú
 
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