Boeing 767 - Page 230

SEE C
D
CB
CHORD WIDTH OF
DISTORTION
LEADING EDGE
LENGTH
DISTORTION
(DISPLACEMENT
FROM LEADING
EDGE)
MEASURE FROM A
STRAIGHT EDGE
HELD
ON THE
LEADING EDGE.
LEADING EDGE
2ND-THRU 5TH-STAGE BLADES
ROOT
AREA
A
AREA B
0.75 INCH
(19.1 mm)
STAGE ONE FAN BLADE
DISTORTION ON LEADING EDGE
(DUE
TO FOD)
1330077 S00061422901_V1
Fan Rotor Blade Inspection
Figure 601/72-31-02-990-804-G00 (Sheet 2 of 2)
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-31-02
NoC
Page 606
D633T1B7 Dec 22/2016
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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