TM 55-1520-240-T
4-1.10 ROTOR RPM CHANGES MORE THAN +0 OR -2 PERCENT OR ENGINE TORQUE SPLIT EXCEEDS 6 PERCENT DURING HOVER
4-1.10
FAULT ISOLATION PROCEDURE
Personnel Required:
INITIAL SETUP
Aircraft Powerplant Repairer
Applicable Configurations:
References:
TM 55-1520-240-23
Without 74
Tools:
Equipment Condition:
Powerplant Repairer's Tool Kit,
TM 55-1520-240-23:
NSN 5180-00-323-4944
Battery Connected
Electrical Power On
Materials:
Hydraulic Power On
None
END OF TASK
4-26 Change 17
