Boeing 737-600 - Page 2090

1
2
4
6
5
3
ADD THREE SHIMS MAX (AS NECESSARY)
AT [I]
ADD TWO SHIMS MAX (AS NECESSARY)
AT [H]
MOVE ONE WASHER FROM [G] TO [F]
MOVE THREE WASHERS FROM [B] TO [A]
MOVE TWO WASHERS FROM [B] TO [A]
MOVE ONE WASHER FROM [B] TO [A]
MOVE ONE WASHER FROM [A] TO [B]
MOVE ONE WASHER FROM [D] TO [C]
MOVE ONE WASHER FROM [C] TO [D]
REMOVE ONE SHIM AT [H]
MOVE ONE WASHER FROM [D] TO [E]
MOVE ONE WASHER FROM [E] TO [D]
REMOVE ONE SHIM AT [I]
GAP LOCATION
GAP
LIMIT
ACTUAL
MEASUREMENT
< 0.060
ADJUSTMENT NECESSARY
TO GET GAP LIMIT (REFER TO
TABLE B FOR SHIM QUANTITY)
FLAP LEVER
> 0.100
0.080-0.100
0.060-0.080
< 0.030
> 0.054
0.060 MIN
SPEEDBRAKE
LEVER
0.030-0.060
0.036-0.090
< 0.025
> 0.090
< 0.036
> 0.0540
< 0.0325
> 0.086
< 0.022
0.0325-0.0540
ENGINE START
DETENT
ENGINE 1
ENGINE START
DETENT
ENGINE 2
THRUST LEVER
ENGINE 2
THRUST LEVER
ENGINE 1
0.025-0.054
0.022-0.086
CONTROL SHAFT ADJUSTMENT GAP LIMITS
TABLE A
G42261 S0006583071_V2
Control Shaft Washer (Shim) Limits
Figure 406/76-11-02-990-805-F00 (Sheet 2 of 3)
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-02
Page 435
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
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