Boeing 767 - Page 200

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
U
(EXTENDED)
CCW
X = 48 ˚
0 ˚
TRANSPOSED
R1
47810 S00061422873_V1
Example of How to Find Angle X By Transposition
Figure 509/72-31-00-990-818-G00
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-31-00
NoC
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