BEECHCRAFT 65-A90-4

The Beechcraft 65-A90-4 is a variant of the King Air A90 turboprop, featuring two Pratt & Whitney PT6A-20 engines, and specifications include a maximum takeoff weight of 9,300 lbs, a maximum speed of 223 knots, and a maximum range of 1160 nm. It has seating for a crew of 1-2 and up to 7 passengers. Other key specs include a service ceiling of 30,000 ft, a rate of climb of 1900 fpm, and dimensions of 14 ft 8 in (height) and 45 ft 11 in (wingspan).

Performance

• Maximum Speed: 223 knots
• Normal Cruise Speed: 216 knots
• Stall Speed: 77 knots
• Service Ceiling: 30,000 ft
• Rate of Climb: 1900 fpm
• Rate of Climb (One Engine Inop): 490 fpm
• Takeoff Distance: 1730 ft
• Landing Distance: 1250 ft

Dimensions

• Exterior Height: 14 ft 8 in
• Wingspan: 45 ft 11 in
• Length: 35 ft 6 in
• Cabin Height: 4 ft 10 in
• Cabin Width: 4 ft 6 in
• Cabin Length: 12 ft 4 in
• Cabin Volume: 227 cu ft

Weights

• Maximum Takeoff Weight: 9,300 lbs
• Empty Weight: 5,318 lbs
• Maximum Payload: 2,976 lbs

Powerplant

• Engines: 2
• Engine Manufacturer: Pratt & Whitney
• Engine Model: PT6A-20
• Horsepower: 550 HP

Capacity

• Crew: 1-2
• Passengers: Up to 7
• Internal Baggage: 54 cu ft
• Fuel Capacity: 384 gallons