General Aviation
Beech C90a
Manufacturer: BEECH
The Beechcraft C90A is a twin‑turboprop utility aircraft in the King Air 90 family. It was produced by Beechcraft from the early 1980s until 1992, with a maximum take‑off weight of 10,100 lb and powered by two Pratt & Whitney PT6A‑21 engines. The C90A is a refined version of the earlier C90, featuring redesigned engine cowlings, improved landing‑gear retraction, and upgraded electrical and pressurization systems.
Aircraft Facts
- Type Key
- beech-c90a
- Class
- General Aviation
- Registry Count
- 126
- Example Registration
- N111KC
Specifications
- Wingspan
- 15.32 m / 50.25 ft
- Length
- 10.82 m / 35.5 ft
- Height
- 4.34 m / 14.25 ft
- Max Speed
- 500 km/h / 270 kn
- Cruise Speed
- 416 km/h / 226 kn
- Range
- 2446 km / 1321 nmi
- Ceiling
- 9144 m / 30000 ft
- First Flight
- 1963-05-15
- Production Start
- 1963
- Production End
- 2021
- Total Built
- 3370
Variants
- C90A- 126 registrations - Example N111KC
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