1981 Mitsubishi MU2 Solitaire
Description
The Mitsubishi MU2 Solitaire is a twin-engine turboprop aircraft produced by Mitsubishi Heavy Industries of Japan between 1965 and 1986. The MU2 is a light-weight, high-performance aircraft designed for executive, business, and light cargo transport. It has a pressurized cabin, retractable landing gear, and is able to land on short runways. It is powered by two Garrett TPE-331-5-252G engines, each producing 750 shp (560 kW), and has a maximum speed of 260 knots (480 km/h). The MU2 Solitaire is capable of carrying up to eight passengers and has a range of 1,290 nautical miles (2,400 km).
Features
- Total Time: 5937
- Engines / Prop:
- TPE 331-10-511M
- ENGINE TIME: 599/599 Since Overhaul
- PROP TIME: 352/352 SPOH May 2016
- Garmin 750/750 WAAS and TAWS/G600 with GAD 43
- COMS: Garmin 750/750
- HSI: Sperry RD 44 Co-Pilot
- NAVS: Garmin 750/750
- RADAR: Sperry 300 Slimline
- A/P: Sperry SPZ-500 FD System w/GPS Roll Steer
- DME: Collins 40
- GPS: Garmin 750/Garmin 750
- TXPR: Dual GTX-33es
- RADIO ALT: Collins 55
- STORMSCOPE: WX500 W/ GPS Input
- MFD: Garmin 600
- MOVING MAP: Garmin 750 /G600
- EFIS: G600
- ADSB: GDL-88 ADSB
- NEXRAD: Garmin GDL 69A
- TRAFFIC: GTX-800 traffic
Location
