Boeing 767 - Page 356

1
THE BLADE CHORD LENGTH.
1 DIMENSION A TO BE A MAXIMUM OF
0.1 INCH (2.50 mm) OR 5% OF
OF NICKS AND DENTS
LEADING AND TRAILING EDGE BLEND REPAIR
A
BLADE EDGE
MINIMUM BLEND RADIUS
AFTER BLEND REPAIR
CONTOUR OF THE BLADE
8A8A
DIMENSION
A
OF THE BLADE
INITIAL CONTOUR
SEE
A
LEADING EDGE NICK
(OPEN)
VBV DOOR
ACOUSTIC LINER
BORESCOPE
1020570-00
E98141 S00061423066_V1
Stage 1 Blade Repair - Repair of the HPC Blades
Figure 806/72-35-00-990-814-G00
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-35-00
NoC
Page 819
D633T1B7 Dec 22/2016
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