4-1.10 ROTOR RPM CHANGES MORE THAN +0 OR -2 PERCENT OR ENGINE TORQUE SPLIT EXCEEDS 6 PERCENT DURING HOVER

NO. 1 OR NO. 2 ENGINE OIL TEMP HIGH (Continued)

TM-55-1520-240-T-1 CH-47D Heilcopter Manual
Page Navigation
212

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

Privacy Statement
Press Release
Contact