Boeing 767 - Page 58

LEADING
EDGE
A
MAXIMUM
2.0 INCHES
(50.8 mm)
0.75 INCH
(19.1 mm)
MAXIMUM
IGV
CONTACT
DAMAGE
A
SEE
EXAMPLE OF
TIP CONTACT
CONVEX SIDE)
TIP (FROM THE
BENT AT THE
CONVEX SIDE)
TIP (FROM THE
BENT AT THE
LEADING
EDGE
2/3 CHORD
TRAILING
EDGE
TIP CLANG MARK
(EXAMPLE)
A
A
A-A
FWD
25348 S00061422705_V1
Tip Clang Marks for the Compressor Rotor Blade
Figure 602/72-00-00-990-805-G00
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-00-00
NoC
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D633T1B7 Aug 22/2017
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