0.0
(0.0)
0.5
(12.7)
1.0
(25.4)
1.5
(38.1)
1.6
(40.6)
0.24
(6.1)
0.20
(5.1)
0.15
(3.8)
0.11
(2.8)
0.10
(2.5)
0.00
(0.0)
0.03
(0.8)
0.06
(1.5)
0.09
(2.3)
0.10
(2.5)
0.12
(3.0)
0.11
(2.8)
0.11
(2.8)
0.10
(2.5)
0.10
(2.5)
1.00
(25.4)
0.12
(3.0)
0.11
(2.8)
0.11
(2.8)
0.10
(2.5)
0.10
(2.5)
0.0
(0.0)
0.5
(12.7)
1.0
(25.4)
1.5
(38.1)
1.6
(40.6)
1.00
(25.4)
0.33
(8.3)
NO
BLENDING
ALLOWED
0.33
(8.3)
NO
BLENDING
ALLOWED
0.10
(2.5)
BOTH
SIDES
0.30
(7.6)
0.5
(12.7) RADIUS
AREA
C
BLENDING
ONE
EDGE
(LEADING
OR
TRAILING)
DIMENSION
FROM
TIP
AXIAL BLEND DEPTH
BLADE
TIP
AXIAL BLEND DEPTH
DOVETAIL
0.10
(2.5)
BOTH
SIDES
0.30
(7.6)
PLATFORM
AREA
C
DIMENSION
FROM
TIP
AXIAL BLEND DEPTH
BLADE
TIP
AXIAL BLEND DEPTH
DOVETAIL
STAGE
8
HPC
BLADE
DIMENSIONS
ARE
IN
INCHES
(MILLIMETERS
IN
PARENTHESIS).
NOTE:
____
1257250-00-B
BLENDING
BOTH
EDGES
(LEADING
OR
TRAILING)
PLATFORM
1862150 S00061423087_V1
Stage 2-14 HPC Blade Blend Limits
Figure 811/72-35-00-990-819-G00 (Sheet 9 of 16)
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-35-00
NoC
Page 844
D633T1B7 Apr 22/2020
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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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