CF8-6205-00-A
270
˚
180
˚
90
˚
A
211
˚
1
A
280
˚
0
U
8.0
MILS
0
R
8.3
1
U
6.7
MILS
1
0
˚
X
48
˚
CCW
51798 S00061422872_V1
Example of Polar Plot to Find the Correction Balance Weight
Figure 508/72-31-00-990-817-G00
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-31-00
NoC
Page 518
D633T1B7 Dec 22/2016
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