MU-2B-30

The MU-2B-30 is a specific model of the Mitsubishi MU-2 turboprop, also known as the MU-2G, which features a stretched fuselage and was powered by two Garrett TPE331-1-151A engines producing 665 shp each. Its specifications include a max takeoff weight of 11,575 lb (5,250 kg), a cruise speed of up to 547 km/h (340 mph), and a service ceiling of 29,590 ft (9,020 m).

Performance and weights

• Cruise speed: 547 km/h (340 mph, 295 kn) at 4,575 m (15,010 ft)
• Economical cruise speed: 483 km/h (300 mph, 261 kn) at 7,620 m (25,000 ft)
• Stall speed: 185 km/h (115 mph, 100 kn) with flaps down
• Rate of climb: 12.0 m/s (2,360 ft/min) at sea level
• Range: 2,334 km (1,450 mi, 1,260 nmi) with reserves
• Service ceiling: 9,020 m (29,590 ft)
• Takeoff run: 661 m (2,169 ft) over a 15 m (50 ft) obstacle
• Landing run: 573 m (1,880 ft) from a 15 m (50 ft) obstacle
• Max takeoff weight: 5,250 kg (11,575 lb)
• Empty weight: 3,433 kg (7,570 lb)

Dimensions

• Wingspan: 11.94 m (39 ft 2 in)
• Length: 12.01 m (39 ft 5 in)
• Height: 4.17 m (13 ft 8 in)

Powerplant

• Engines: 2 x Garrett TPE331-1-151A turboprops
• Horsepower: 665 shp each