CF8-6948-00-C
(20.32
mm)
(20.32
mm)
FORWARD
EDGE
OF
THE
FORWARD
EDGE
OF
THE
A-A
LEADING
GILL HOLE
CONVEX
(SUCTION)
SIDE
CONCAVE
(PRESSURE)
SIDE
TRAILING
EDGE
0.800
INCH
0.800
INCH
LEADING
GILL HOLE
LEADING
EDGE
FWD
INNER
FORWARD
FLANGE
OUTER
FORWARD
FLANGE
TRAILING
EDGE
SLOTS
A A
PLATFORM
INNER
NOSE
HOLES
GILL
HOLES
25350 S00061422719_V1
1st-Stage High Pressure Turbine Nozzle Vane Inspection
Figure 611/72-00-00-990-819-G00
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-00-00
NoC
Page 639
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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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