1-82 INSPECT ENGINE SUBJECTED TO EXCESSIVE G-LOADS
Personnel Required:
INITIAL SETUP
68B10 Aircraft Powerplant Repairer
68B30 Aircraft Powerplant Inspector
Applicable Configurations:
All
References:
TM 55-1520-240-10
Tools:
Powerplant Mechanic's Tool Kit,
NSN 5180-00-323-4944
Task 8-23
Technical Inspection Tool Kit,
Task 8-27
NSN 5180-00-323-5114
Materials:
None
1. If it is suspected that excessive G-loads have
been imposed on engine, proceed as follows:
NOTE
G-load limits are defined in Operating
Instructions TM 55-1520-240-10. The
following inspections shall be made im-
mediately after the flight during which
the excessive G-loads occurred.
shall be no cracked flanges.
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