Boeing 767 - Page 83

B
SEE
A
B
SEE
SHROUD
____
0.100 INCH
SHADED AREAS EXCEPT ON THE
NO REPAIR IS PERMITTED IN THE
CIRCUMFERENTIAL FACES
SHROUD LOCK
NOTE:
LEADING AND TRAILING EDGES
(ANGLE WING)
SEAL LIP
PLATFORM
A
SKIRT
SURFACE
MATING
RADIUS
A A
ROOT
BLADE
SERRATIONS
RIB
SHROUD
SHROUD SEAL
SHROUD
SHANK
SERRATION
DOVETAIL
EDGE
SIDE
CONVEX
0.100 INCH
(2.54 mm)
A-A
LEADING
EDGE
TRAILING
CHORD
SIDE
CONCAVE
(2.54 mm)
25387 S00061422731_V1
Low Pressure Turbine Rotor Blade Inspection
Figure 620/72-00-00-990-831-G00
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-00-00
NoC
Page 650
D633T1B7 Aug 22/2017
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