OF
BRADELLOY
FALLOUT
CELL
IS
OPEN
BECAUSE
SURFACE
SEAL
EROSION
CRACK
CRACK
60899 S00061422726_V1
2nd-Stage High Pressure Turbine Shroud Segment
Figure 616/72-00-00-990-826-G00
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-00-00
NoC
Page 646
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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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