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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 發動機控制 ENGINE CONTROLS(30)
