Boeing 767 - Page 441

1.0
1.5
2.0
2.5
3.0
3.5
0.5 163
325
488
650
100
201
302
402
503
603
704
--
--
--
BALANCE CORRECTION WEIGHT TABLE
(U)
VIBRATION
BALANCE CORRECTION WEIGHT (GRAM INCHES)
(MILLS)
3200 (RPM)
3439 (RPM)
GM IN 4 40
X
X
X
X
X
X
X
X
X
X
X
X
X
1
X
X
X
X
2 3
X
X
1
X
X
X
X
X
2
X
X
X
3
X
X - INDICATES LOCATION TO PLACE
BALANCE CLIP IN RELATION TO
THE CENTER BLADE
LPT BALANCE CLIP DISTRIBUTION TABLE
NO.
OF
CLIPS
BLADE
CENTER
1
2
3
4
5
6
7
95
190
285
379
473
567
660
750382 S00061423152_V1
Balance Correction Weight and Location
Figure 507/72-52-00-990-807-G00
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-52-00
NoC
Page 515
D633T1B7 Aug 22/2017
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