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Engine or Fuselage Fire Flight

TM-1-1520-240-CL Army CH-47D Heilcopter (EIC:RCD) Manual
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TM 1-1520-240-CL E-7 Engine power is not required: 1.  EMER ENG SHUTDOWN. 2.  Land as soon as practicable. 712 Torque Measuring System Malfunctions 1.  AC and DC Torque circuit breakers — In. 2.    N1s — Monitor when power changes are made, insuring power outputs are matched. 3.  Fuel flow indicator — Monitor for matched fuel flows. 714A  Torque Measuring System Malfunctions N1 and PTIT indicators — Check. N1s and PTITs not matched 1-2. 1.  LOAD SHARE switch — PTIT 2.  PTIT indicators — Check. PTITs not matched Land as soon as practicable. N1s and PTITs are matched AC   and   DC   Torque   and   Engine   circuit breakers — IN. FIRE Engine Hot Start ABORT START. Residual Fire During Shutdown 1.  ABORT START. 2.  FIRE PULL handle (affected engine) — Pull. Auxiliary Power Unit (APU) Fire 1.  APU switch — OFF. 2.  ABORT START.







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