Kestrel KL-1
Kestrel Aircraft Company · United States · first flew 1995 · light aircraft
The Kestrel KL-1 is an American single-engined four-seat utility aircraft designed and built in the 1990s by the Kestrel Aircraft Company of Norman, Oklahoma. It was designed to meet the utility and normal categories of Part 23.
Recognition (WEFT)
| W — Wings | High-mounted, straight |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | Composite fuselage with a four-seat cabin |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Cantilever high-wing cabin monoplane
- Composite fuselage with a four-seat cabin
- Fixed tricycle landing gear
Look for a composite high-wing four-seater with fixed tricycle gear. The wingspan is 11.2 m.
Specifications
- The Kestrel KL-1 has a length of 8.15 m (27 ft).
- It has a wingspan of 11.2 m (37 ft).
- Typical crew: 1.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
The prototype KL-1A, registered N960KA, first flew on 19 November 1995 with a 160 hp Lycoming O-320-D2G piston engine. The programme was abandoned while the prototype was test flying for certification.
Variants
Proposed variants included a KL-1B de-luxe model, a KL-1C high-performance version, a six-seat KL-1D and a retractable-gear KL-1R. An armed observation version, the K250A, was also proposed.
Where you'll see it
Three aircraft were built, and none entered service.
Related aircraft
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