MU-2B-26

The MU-2B-26 is a twin-engine turboprop aircraft with a maximum takeoff weight of 10,470 lbs. Its key specifications include a service ceiling of about 29,750 ft, a maximum speed of around 314 knots, and a maximum range of 972 nm. It has a crew of two and can carry up to five passengers. The MU-2B-26 is powered by two Honeywell TPE331-5-252M engines.

Performance and dimensions

• Maximum speed: 314 kts
• Normal range: 757 nm
• Maximum range: 972 nm
• Service ceiling: 29,750 ft
• Rate of climb: 2,000 fpm
• Rate of climb (one engine inop): 500 fpm

Weights and fuel

• Max takeoff weight: 10,470 lbs
• Max landing weight: 9,955 lbs
• Operating weight: 7,400 lbs
• Fuel capacity: 2,439 lbs (approx. 364 gal)

Capacity

• Crew: 2
• Passengers: 5
• Cabin volume: 142 cubic ft

Engines

• Engines: 2 x Honeywell TPE331-5-252M turboprops
• Horsepower: 665 hp each (or 715 shp