General Aviation
Beech 65-A90-1
Manufacturer: BEECH
The Beech 65-A90-1 is a twin‑turboprop aircraft from the King Air 90 family. It is an unpressurised, square‑windowed variant powered by two Pratt & Whitney Canada PT6A‑20 engines. The model was developed for the U.S. Army as the U‑21A utility aircraft and entered production in 1966, remaining in service until the 90‑series was retired in 2021.
Aircraft Facts
- Type Key
- beech-65-a90-1
- Class
- General Aviation
- Registry Count
- 90
- Example Registration
- N226DR
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
- 65-A90-1- 90 registrations - Example N226DR
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