34
35
37
38
(RPM) (RPM) (RPM) (RPM)
(99.1%)
3400 3200
(93.2%)
3400
(99.1%)
3200
(93.2%)
CF8-6162-04-A
AMPLITUDE
U
(MILS)
BALANCE
WEIGHT
QUANTITY
(W)
PHASE ANGLE
(A)
(DEGREES) (DEGREES)
PHASE ANGLE
(A)
HOLE
NUMBERS
HOLE
NUMBERS
SPINNER
HOLE
LOCATION
3
4
5
6
7
8
9
10
11
25
24
23
22
21
20
19
18
17
16
15
14
13
12
11
28
27
26
25
24
23
22
21
20
19
18
17
16
15
14
13
12
11
10
9
8
3400
(RPM)
(99.1%)
3200
(RPM)
(93.2%)
194-203
204-212
213-222
223-231
232-241
242-250
251-260
261-269
270-279
280-288
289-298
299-307
308-317
318-326
327-336
337-345
346-355
356-3
4-13
14-22
23-32
33-41
42-51
52-60
61-70
71-79
80-89
90-98
99-108
109-117
118-127
128-136
137-146
147-155
156-165
166-174
175-184
185-193
7
6
5
4
3
2
1
38
37
36
35
34
33
32
31
30
29
28
27
26
10
9
8
7
6
5
4
3
2
1
33
32
31
30
29
36
22.5
GRAMS
30.0
GRAMS
37.5
GRAMS
45.0
GRAMS
52.5
GRAMS
60.0
GRAMS
67.5
GRAMS
75.0
GRAMS
82.5
GRAMS
33.0
GRAMS
41.7
GRAMS
50.4
GRAMS
59.1
GRAMS
67.8
GRAMS
76.5
GRAMS
85.2
GRAMS
93.9
GRAMS
24.3
GRAMS
23437 S00061422866_V1
Trim Balance Matrix
Figure 503/72-31-00-990-812-G00
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-31-00
NoC
Page 512
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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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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