C
TIP
NOTCH
FOR
IDENTIFICATION)
TIP
NOTCH (USED
USUAL
0.2
INCH (5.1
mm)
LEADING
EDGE
0.25 INCH (6.4
mm)
USUAL
TIP CAP
(NOT
PERMITTED)
TIP CAP CAN
BE
SEEN
B
SIDE
CONVEX
OR
CONCAVE
BLADE
TIP
142039 S00061422722_V1
1st-Stage High Pressure Turbine Rotor Blade Inspection
Figure 613/72-00-00-990-821-G00 (Sheet 2 of 2)
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-00-00
NoC
Page 642
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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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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