BRAZED
CLOSED, TYPICAL
BOTH
SIDES
MANUFACTURING
ACCESS
HOLES
SEE
C
C
VENT SLOT
REPAIR
TIP
2.00
INCHES
(50.8
mm)
AREA
B
AREA
A
FACE
PRESSURE
PLATFORM
BOWED
AND
CRACKED
PLATFORM
B
CF8-A6003-00-C
SEE
A
TIP
AREA
BLADE
TIP CAP
ABOVE
THE
LAST
VENT HOLE
1-1/2
HOLE
SPACES
B
SEE
VENT
HOLES
COOLING
AIR
VENT SLOT
BLADE
PLATFORM
(BOTH
SIDES)
SEAL
LIP
TIP CAP LIP
TIP
CAVITY
SHELF
0.25 INCH
(6.4
mm)
SIDE
SIDE
FORWARD
TIP
CAP
HOLE
0.25 INCH (6.4
mm)
CAP
HOLE
AFT TIP
TIP CAP
CONCAVE
A-A
A
A
A
CONVEX
TIP
HOLES
TRAILING
EDGE
LEADING
EDGE
26110 S00061422723_V1
2nd-Stage High Pressure Turbine Rotor Blade Inspection
Figure 614/72-00-00-990-823-G00
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-00-00
NoC
Page 643
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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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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