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
- 124
- 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- 124 registrations - Example N111KC
Related Aircraft
- Beech A36 - 1,907 registrations
- Beech F33a - 978 registrations
- Beech V35b - 913 registrations
- Beech 95-B55 (T42a) - 775 registrations
- Beech 58 - 723 registrations
- Beech S35 - 459 registrations
- Beech C23 - 456 registrations
- Beech V35 - 425 registrations
Machine-Readable Resources
Sources
- https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=111KC
- https://www.faa.gov/licenses_certificates/aircraft_certification/aircraft_registry/releasable_aircraft_download
- https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=117C
- https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=119SA
- https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=120RP
- https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=1212W
- https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=127MU
- https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=127ZW
- https://en.wikipedia.org/wiki/Beechcraft_King_Air