4-1.11 NO. 1 OR NO. 2 ENGINE HIGH PTIT

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 HIGH PTIT (Continued)

TM-55-1520-240-T-1 CH-47D Heilcopter Manual
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TM 55-1520-240-T 4-1.11 NO. 1 OR NO. 2 ENGINE HIGH PTIT 4-1.11 FAULT ISOLATION PROCEDURE References: INITIAL SETUP TM 55-1520-240-10 TM 55-1520-240-23 Applicable Configurations: TM 55-2840-254-23 Without 74 Equipment Condition: Tools: TM 55-1520-240-23: Powerplant Repairer's Tool Kit, Battery Connected NSN 5180-00-323-4944 Electrical Power On Materials: Hydraulic Power On None Personnel Required: Aircraft Powerplant Repairer Army Rotary Wing Aviator (2) GO TO NEXT PAGE 4-28 Change 17 Page 4-27 is a blank page.

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