MIDSPAN SHROUDS
OF
THE
ADJACENT
BLADES
LEADING
EDGE
NO
AIRFOIL
DENTS
PERMITTED
APPROVED
AREA
FOR
AIRFOIL
DENTS
CAUSED
BY
THE
(15.24
mm)
0.6
INCH
C81025 S00061422711_V1
Midspan Shroud Inspection of the 1st-Stage Blades
Figure 606/72-00-00-990-811-G00 (Sheet 1 of 2)
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-00-00
NoC
Page 631
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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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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