1257238-00-B
SEE
A
A
PLATFORM,
DOVETAIL
DOVETAIL
ROOT
FILLET
RADII
(ALL
AROUND)
LEADING
EDGE
DENT
DEPTH
DENT
WIDTH
NORMAL
LEADING
EDGE
CONTOUR
EDGE
EROSION
EDGE
EROSION
TIP
CURL
OR
TIP
FOLD,
IGV
CONTACT
MID-SPAN
SHROUD
WEAR PAD,
CARBOLOY
TRAILING
EDGE
CENTER
PANEL
AXIAL CRACK
OR
TEAR
NICK
DEPTH
NICK
RADIAL
TIP
CRACK
TIP
CORNER
MISSING
OR
CORNER
EROSION
DENT
TIP
CURL
DEPTH
RADIAL
TIP
CLANG
NOTE:
NO
SHARP
CORNERS
AFTER
BLENDING,
MINIMUM
BLEND RADII
IS
0.5
INCH
(12.7
mm)
RADIUS.
____
CHORD
LENGTH
CHORD
PERCENT
DENT
LENGTH
F56896 S00061423074_V2
STAGE 1 HPC Blade Blend Limits
Figure 809/72-35-00-990-817-G00 (Sheet 1 of 4)
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-35-00
NoC
Page 831
D633T1B7 Aug 22/2017
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ABX 001-007, 011, 012, 016-019, 021, 022, 025, 101,
109, 114, 115, 314-999
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