CF8-6113-00-A
13
12
QUADRANT
II
QUADRANT
I
QUADRANT
III
QUADRANT
IV
38
37
36
35
34
33
32
31
30
29
28
27
26
25
24
23
22
21
20
19
18
17
16
15
14
11
WEIGHT
MOMENT
WEIGHT
MOMENT
POS
BLD
DIFF.
WEIGHT
WEIGHT
MOMENT
WEIGHT
MOMENT
POS
BLD
ENG
S/N_____
REPLACEMENT
BLADES
INITIAL
BLADES
REPLACEMENT
BLADES
INITIAL
BLADES
CODE
CL
CODE
CL
CODE
CL
CODE
CL
10
1
9
8
7
6
5
4
3
2
21665 S00061422916_V1
Blade Plot Form
Figure 804/72-31-02-990-809-G00 (Sheet 1 of 2)
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-31-02
NoC
Page 811
D633T1B7 Dec 22/2016
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ABX 001-007, 011, 012, 016-019, 021, 022, 025, 101,
109, 114, 115, 314-999
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