Beechcraft

King Air 65-90

The Beechcraft King Air 65‑90 series represents a versatile family of twin‑engine turboprop aircraft that has been in continuous production since the early 1970s. Originating from Beechcraft’s earlier Model 90 twin‑engine piston line, the King Air was introduced in 1974 as the Model 65 with a Pratt & Whitney PT6A‑21 engine, and later expanded to the 90‑series, featuring upgraded PT6A‑135 engines and increased maximum take‑off weight. Over the decades the aircraft has been refined with modern avionics, composite airframe components, and enhanced cabin pressurization, yet it retains the rugged, low‑maintenance design that made the original King Air popular with both civilian and military operators.

Key features include a spacious 19‑seat cabin, a high‑performance turboprop powerplant delivering cruise speeds of up to 312 kt, a service ceiling above 35 000 ft, and a short‑field capability that allows operation from runways as short as 2 800 ft. The King Air’s reliability and economic operating costs have secured its role in executive transport, regional airline service, air‑ambulance missions, and government surveillance. Its longevity and adaptability underscore the King Air’s significance as one of the most successful and enduring turboprop platforms in aviation history. Today, more than 2,500 King Air aircraft remain active worldwide, testifying to its lasting impact.

Production & History

Units Produced
112
First Flight
1965

Design & Classification

Country of Origin
Manufacturer
Beechcraft
Developer
Beechcraft
Engine
PT6A-6
Wikidata ID
Q15838789