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Engine Fluctuations without FADEC 1/2 Light
ROTOR, TRANSMISSION, AND DRIVE SYSTEMS

TM-1-1520-240-CL Army CH-47D Heilcopter (EIC:RCD) Manual
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TM 1-1520-240-CL E-4 Engine Shutdown — Complete Electrical Failure F 1.   FUEL VALVE #1 and #2 ENGINE — CLOSE. 2.  Normal shutdown — Perform. Engine Shutdown — Condition Lever Failure 1.  FIRE PULL handle (affected engine) — Pull. 2.  Normal shutdown — Perform. Engine   Shutdown   With   APU   or   APU   Generator Inoperative 1.  No. 2 Engine — Perform a normal shutdown. 2.  All   unnecessary   electrical   switches   (except BATT switch) — OFF. 3.  GEN 1 and 2 switches — OFF. 4.  ENG  COND  1  lever  —  GND.  Wait  until  PTIT decreases  and  then  begins  to  increase;  then move the ENG COND 1 lever to STOP. 5.  ENG 1 START switch — MTR until rotors stop or PTIT is below 260_C. 6.  Normal shutdown — Perform. Engine Oil — Low Quantity/High Temperature/High or Low Pressure 1.  If engine power is required for flight: Land as soon as possible. 2.  If engine power is NOT required for flight: a.   EMER  ENGINE  SHUTDOWN—  (affected engine). b.   Land as soon as practicable. Engine Chip Detector Caution Light ON 1.  If engine power is required for flight: Land as soon as possible. 2.  If engine power is not required: a.   EMER ENGINE SHUTDOWN — (affected engine). b.   Land as soon as practicable.







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