1972 Mitsubishi MU 2J
Description
The Mitsubishi MU-2J is a high-performance business airplane produced by the Japanese aircraft manufacturer Mitsubishi Heavy Industries. First introduced in 1977, the MU-2J is a pressurized, twin-engine turboprop aircraft with the capacity for up to nine passengers. It is powered by two Pratt & Whitney Canada PT6A-135A turboprop engines, each producing 800 horsepower. The aircraft has a maximum speed of 250 knots, a range of 1,250 nautical miles, and a service ceiling of 25,000 feet. The MU-2J is known for its reliability, performance, and efficiency, making it an ideal business aircraft.
Features
- Total Time: 7107
- Engine(s):
- Left:
- 3630.6 Hours Since Overhaul
- 1809.3 Hours Since Hot Section
- Right
- 3447.3 Hours Since Overhaul
- 1743.8 Hours Since Hot Section
- Prop(s):
- Left:
- 162.4 Hours Since Overhaul
- Right:
- 162.4 Hours Since Overhaul
- Avionics:
- Collins VHF-20 Com Radios
- Collins 618 Nav Radios
- Bendix M4D Auto-Pilot with Capability to Operate on Left/Right Gyros
- Pilot & Co-Pilot RMI's
- Dual Wilcox Transponders
- Bendix Weather Radar
- Collins DME-40
- King KDF-600 ADF
- USB Charging Port
- Sigtronics SPA-400 Intercom
- NorthStar GPS-60 GPS
- Additional Equipment:
- Cleveland Wheels & Brakes
- Tip Tank Taxi Lights
- Aft Toilet with Privacy Dividers
- Aft Baggage Compartment
- Aft Club Leather Seating with tables
- Pilot's Heated Windshield
- Lead Acid Battery STC
- Dual PC-17-3 A/C Inverters
- Woodward Engine Fuel Controls
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