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Boeing 767 - Page 371

Boeing 767
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TENSILE
CUSP
IS
ALLOWED
IN
THIS AREA
AREA
A
AREA
B
DIMENSION
A
DIMENSION
B
TIP
CHORD
DIMENSION
A
DIMENSION
B
LEADING
OR
TRAILING
TIP
CORNER
STAGE
1
HPC
BLADE
ALLOWABLE
MISSING
TIP
CORNER
NO
SHARP
CORNERS
AFTER
BLENDING,
MINIMUM
BLEND RADII
IS
0.5
INCH
(12.7
mm)
RADIUS
DIMENSIONS
ARE
IN
INCHES
(MILLIMETERS
ARE
IN
PARENTHESIS).
NOTE:
____
DIMENSION
INCH (mm)
TIP
CHORD
%
A
0.63
(16.00)
0.25
B
1.25
(31.75)
0.5
AREA
SQ. IN.
(SQ.
mm)
QTY.
OF
BLADES
A
0.40
(258.0)
ANY
NUMBER
B
1.23
(793.5)
FOUR
(4)
1257241-00-B
1862110 S00061423077_V1
STAGE 1 HPC Blade Blend Limits
Figure 809/72-35-00-990-817-G00 (Sheet 4 of 4)
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-35-00
NoC
Page 834
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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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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