8X OR
GREATER
8X OR
GREATER
8X OR
GREATER,
OTHERWISE
BLEND
STRAIGHT
TO
BLADE
TIP
8X OR
GREATER
8X OR
GREATER
EXAMPLE
OF
BLENDING
NEAR
TIP
OF
BLADE
BLADE
TIP
X
DEPTH
OF
DAMAGE
BLADE
TIP
EXAMPLE
OF
BLENDING
BELOW
THE TIP
OF
BLADE
X
DEPTH
OF
DAMAGE
1.25X
1.25X
NOTE:
NO
SHARP
CORNERS
AFTER
BLENDING,
MINIMUM
BLEND
RADIUS
IS
R
0.5
INCH
(R
12.7
mm)
IS
RECOMMENDED.
1257257-00
F56904 S00061423097_V1
Blend Area Example
Figure 813/72-35-00-990-821-G00
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-35-00
NoC
Page 854
D633T1B7 Aug 22/2017
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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