BEECHCRAFT 65-A80

The Beechcraft 65-A80 (also known as the A80 Queen Air) is a twin-engine piston aircraft with a maximum takeoff weight of 8,800 lbs and is powered by two 380 hp Lycoming IGSO-540-A1D engines. Its specifications include a cruise speed of around 191-200 KIAS, a service ceiling of approximately 28,500 ft, and a range of roughly 716 to 1,317 nautical miles. Key dimensions are a 50 ft 3 in wingspan and a 35 ft 6 in length.

General characteristics

• Crew: 1–2
• Capacity: 4–9 passengers
• Length: 35 ft 6 in (10.82 m)
• Wingspan: 50 ft 3 in (15.32 m)
• Height: 14 ft 2.5 in (4.33 m)
• Empty Weight: 5,277 lbs (2,394 kg)
• Max Takeoff Weight: 8,800 lbs (3,992 kg)
• Fuel Capacity: 214 US gallons (810 L) (normal)
• Powerplant: 2 × Lycoming IGSO-540-A1D supercharged, air-cooled flat-6 engines, 380 hp each
• Propellers: 3-bladed Hartzell constant speed