1978 Mitsubishi MU 2P Marquise

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Description

The Mitsubishi MU-2P Marquise is a twin-engine turboprop aircraft that was produced by the Japanese company Mitsubishi from 1977 to 1982. It is a pressurized cabin, high-wing aircraft with retractable tricycle landing gear. It was designed primarily to be used as a corporate transport and utility aircraft, but it was also used for private and charter operations. The MU-2P Marquise was the first pressurized Mitsubishi aircraft and was the predecessor to the later MU-2 Marquise and Solitaire. It is powered by two Garrett TPE331-10 engines. The MU-2P had a maximum cruise speed of 253 mph and a maximum range of 1,400 miles. The aircraft can seat up to seven passengers and has a maximum take-off weight of 8,500 pounds.

Features

  • Total Time: 4673
  • Engine 1 Time: 3963 SNEW
  • Engine 2 Time: 3963 SNEW
  • Prop 1 Time: 10 SOH
  • Prop 2 Time: 10 SOH
  • LH Engine: TPE-331-5-252M 3963 SNEW
  • RH Engine: TPE-331-5-252M 3963 SNEW
  • Avionics: Collins Pro Line
  • COM DUAL VHF-20A
  • NAV DUAL VIR-30A
  • ADF ADF-60A
  • DME DME-40A
  • RDR ALT Collins ALT-50
  • RMI DUAL COLLINS 332C-10
  • RADAR RDS81 Color Stabilized
  • TXPR GTX345R/GTX335R
  • ADSB In/Out
  • GPS GTN725
  • Roll Steering GAD42
  • A/P BENDIX M4D
  • F/D Collins 112V
  • Stormscope WX-1000 w/Checklist
  • Garmin FlightStream 510

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