1978 Mitsubishi MU 2P Marquise
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