QUADRANT
MAP
(VIEW
IN
THE AFT
DIRECTION)
III
QUADRANT
IV
QUADRANT
II
QUADRANT
I
QUADRANT
35
34
33
32
31
27
26
25
24
23
22
21
20
19
18
17
16
15
14
13
12
11
10
9
8
7
6
5
4
38
37
36
3
2
1
30
29
28
BALANCE
COMPARISON
MOMENT WEIGHT
DIFF.
SWITCHED
CHANGED
BLADES
IV
II
III
I
QUADRANT
NEW
TOTAL
MOMENT WEIGHT
DIFFERENCE
(II-IV)
DIFFERENCE
(I-III)
TOTAL
MOMENT WEIGHT
OF
QUADRANT
IV
TOTAL
MOMENT WEIGHT
OF
QUADRANT
III
__________________
__________________
__________________
__________________
__________________
__________________
TOTAL
MOMENT WEIGHT
OF
QUADRANT
II
TOTAL
MOMENT WEIGHT
OF
QUADRANT
I
__________________
__________________
__________________
__________________
__________________
__________________
INITIAL
BLADES
REPLACEMENT
BLADES
21622 S00061422918_V1
Balance Comparison Form
Figure 805/72-31-02-990-810-G00 (Sheet 1 of 2)
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-31-02
NoC
Page 813
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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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,
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