1978 Mitsubishi MU 2N
Description
The Mitsubishi MU-2N is a twin-engined light aircraft that was produced by Mitsubishi Heavy Industries in Japan. It was introduced in 1977 and remained in production until 1983. It was designed as a multi-purpose aircraft and was used for a variety of roles, including military, business, air ambulance, and private transport. The MU-2N is powered by two Garrett TPE331 turboprop engines and is equipped with retractable tricycle landing gear. It has a maximum speed of 310 mph and a range of 1,400 miles. The aircraft can accommodate up to seven passengers and has a maximum takeoff weight of 7,500 lbs.
Features
- Total Time: 7027
- Engines:
- TPE 331-5-252M (5400 Hours TBO)
- Engine 1 Time: 4806 Hours SOH
- Engine 2 Time: 3004 Hours SOH
- Prop:
- Hartzell 4 Blade HC-B4TN-5GL
- Left Hand Prop: TSO- 52 Hours SOH (1 Feb 2018)
- Right Hand Prop: TSO-52 Hours SOH (1 Feb 2018)
- Avionics / Equipment:
- GARMIN GNS-430W GPS/NAV/COMM/MAP
- GARMIN GNS-430W GPS/NAV/COMM/MAP
- GARMIN GA-56 GPS Antenna
- GARMIN GA-56 GPS Antenna
- AVIDYNE EX500 MULTI-FUNCTION DISPLAY
- GARMIN GMA-340 Audio Panel / Intercom
- GARMIN GTX-320 Transponder
- KING KFS-580B ADF Control
- KING KDA-692 RMI / ADF Adapter
- AIS ACF-328 Cooling Fan
- RCA DI-2007 Radar Indicator
- RCA RT-3002 Radar R/T
- RCA AP-3001 Radar Antenna
- Radar Altimeter
- Bendix M4D Autopilot
Location
