1997 McDonnell Douglas 600N

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The McDonnell Douglas 600N is a medium-lift, twin-engine, turbine-powered helicopter which was produced by the American aerospace manufacturer McDonnell Douglas. It was introduced in the early 1990s, with the first customer delivery taking place in 1991. It is powered by two Pratt & Whitney Canada PW206B engines and has a maximum cruise speed of 150 knots. The 600N can accommodate up to six passengers and has a range of approximately 450 nautical miles. It is primarily used in corporate and executive transport roles, as well as in search and rescue operations, law enforcement, and medical evacuation.


  • Total Time: 1836 hrs
  • Rolls Royce 250-C47M
  • Engine #1: TTSN: 1,836 Hours CSN: 3,604 Cycles
  • Turbine Module TSN: 1,124 Hours
  • Compressor Impeller TSN: 614 Hours
  • Compressor Module OH on Condition
  • 856 Hrs Remaining to OH
  • 6,990 Hrs Remaining to OH
  • Avionics
  • ADS-B Compliant
  • Garmin GTN 650 NAV/COMM/GPS/WAAS
  • Garmin GNS 430 NAV/COMM/GPS/WAAS
  • Garmin GMA 350H Audio Panel
  • Garmin GTX 34S Transponders
  • KI525A Pictorial NAV Indicator
  • Shading Fuel Management Indicator
  • Kannard 406Mz ELT
  • Features/Options
  • FDC Particle Separator
  • Slant Panel
  • Dual Controls
  • Bristol Wire Strike Kit
  • Life-Limited Parts:
  • Main Rotor Blades TT: 817Hrs
  • -Remaining to Retire: 2,383 Hours
  • Main Rotor Hub TT: 1,836Hrs
  • -Remaining to OH: 888.5 Hours
  • Main Rotor Transmission TT: 1,836Hrs
  • -Remaining to OH: 1,156 Hours
  • Main Rotor Swashplate TT: 1,836Hrs
  • -Remaining to OH: 934 Hours
  • Interconnecting Shaft Remaining 6+ Years
  • Tension – Torsion Straps Remaining 3+ Years

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