EasyManua.ls Logo

Boeing 737-600 - Page 2038

Boeing 737-600
2300 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
3
5
6
4
2
1
MOVE TWO WASHERS FROM [B] TO [A]
MOVE THREE WASHERS FROM [B] TO [A]
MOVE ONE WASHER FROM [G] TO [F]
ADD TWO SHIMS MAX (AS NECESSARY)
AT [H]
ADD THREE SHIMS MAX (AS NECESSARY)
AT [I]
MOVE ONE WASHER FROM [C] TO [D]
MOVE ONE WASHER FROM [D] TO [C]
MOVE ONE WASHER FROM [A] TO [B]
MOVE ONE WASHER FROM [B] TO [A]
MOVE ONE WASHER FROM [D] TO [E]
MOVE ONE WASHER FROM [E] TO [D]
REMOVE ONE SHIM AT [H]
REMOVE ONE SHIM AT [I]
CONTROL SHAFT ADJUSTMENT GAP LIMITS
TABLE A
0.022-0.086
0.025-0.054
THRUST LEVER
ENGINE 1
THRUST LEVER
ENGINE 2
ENGINE START
DETENT
ENGINE 2
ENGINE START
DETENT
ENGINE 1
0.0325-0.0540
< 0.022
> 0.086
< 0.0325
> 0.0540
< 0.036
> 0.090
< 0.025
0.036-0.090
0.030-0.060
SPEEDBRAKE
LEVER
0.060 MIN
> 0.054
< 0.030
0.060-0.080
0.080-0.100
> 0.100
FLAP LEVER
ADJUSTMENT NECESSARY
TO GET GAP LIMIT (REFER TO
TABLE B FOR SHIM QUANTITY)
< 0.060
ACTUAL
MEASUREMENT
GAP
LIMIT
GAP LOCATION
G11814 S0006583054_V2
Control Shaft Washer (Shim) Limits
Figure 408/76-11-01-990-810-F00 (Sheet 2 of 3)
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-01
Page 421
D633A101-ILF Oct 15/2017
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL

Table of Contents

Related product manuals