Boeing 767 - Page 249

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CF8-6112-00-
REPLACEMENT BLADE THAT IS DIRECTLY OPPOSITE IN THE LEFT QUADRANT
SHOWS THE REPLACEMENT BLADE IN THE RIGHT QUADRANT IS HEAVIER THAN THE
BLADE THAT IS DIRECTLY OPPOSITE IN THE RIGHT QUADRANT
SHOWS THE REPLACEMENT BLADE IN THE LEFT QUADRANT IS HEAVIER THAN THE
EXAMPLE
IF YOU SWITCH BLADE POSITIONS, USE BLADES THAT ARE DIRECTLY OPPOSITE.
BLADES
REPLACEMENT
CODE
CL
DIFF.
WEIGHT
WEIGHT
MOMENT
CODE
CL
POS
BLD
CODE
CL
WEIGHT
MOMENT
WEIGHT
MOMENT
CODE
CL
POS
BLD
BLADES
REPLACEMENT INITIAL
BLADES
ENG S/N
123722
QUADRANT
II
QUADRANT
I
QUADRANT
III
QUADRANT
IV
1115686
88
98
109
140
148
149
151
120
106
95
87
65
60
53
33
34
55
62
76
123122
122730
122076
120508
120145
120052
119971
121502
122228
123170
124296
124548
124857
125874
125811
124791
124441
1092334
122784
1241294
201
182
367
696
97
611
424
110
83
46
213
502
62
253
175
638
50
55
265 1 79
70
57
123457
122718
124496
61
124919
124622
124328
123833
123259
123210
123077
124017
124421
1260027
124666
125015
125643
126256
126732
126919
126857
126467
126030
125442
52
58
64
74
85
86
89
62
50
38
25
16
12
13
21
30
42
38
37
36
35
34
33
32
31
30
29
28
27
26
25
24
23
22
21
20
92
100
116
126
162
143
103
104
94
83
75
58
48
30
47
56
63
54
60
66
71
83
96
75
70
54
49
61
24
15
9
14
23
34
42
19
18
17
16
15
14
12
11
10
9
8
7
6
5
4
3
2
1092163
122921
122548
121709
121204
120242
119441
120395
121392
122311
1243533
122830
123383
123794
124610
125110
126049
125173
124741
124386
1115963
124838
124542
124207
123988
123382
123776
124016
1260027
124815
125071
125491
126313
126785
127084
126846
126361
125850
125411
WEIGHT
MOMENT
RIGHT QUADRANTS
LEFT QUADRANTS
BLADES
INITIAL
21610 S00061422917_V1
Blade Plot Form
Figure 804/72-31-02-990-809-G00 (Sheet 2 of 2)
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-31-02
NoC
Page 812
D633T1B7 Dec 22/2016
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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109, 114, 115, 314-999