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The Skyfox is a high-wing braced monoplane with a conventional tailwheel landing gear with a fixed tailwheel. It has a welded steel fuselage with fabric covering. The wings can be folded when not in use along the side of the fuselage. Originally built to meet Australian ultralight regulations the latter CA-25 is built to JAR-VLA rules. [1]
Two seat side-by-side seating, high wing, US homebuilt development of the single seat Sparrow UL, with tricycle gear and an optional folding wing for transport or storage, powered by a 64 hp (48 kW) Rotax 582. Empty weight of 510 lb (231 kg) and gross weight 1,050 lb (476 kg). 60 were reported flying in 2004.
The aircraft has a 4130 steel tube frame fuselage and a wing constructed from aluminium tubing, all covered in doped fabric. The wings are equipped with slotted-style flaps and fold for transport or storage without a requirement to disconnect the flaps and ailerons. The landing gear is bungee suspended. The Sky Raider has a fully enclosed ...
The aircraft replaces the Spyder's two-stroke engine with a Yuneec Power Drive 20 20 kW (27 hp) electric motor and two 28 lb (13 kg) Lithium polymer battery packs which provide a 40-minute endurance. The aircraft is intended to be developed into a commercially available kit and forecast to be available for under US$25,000.
The aircraft is amateur-built and not type-certified. Over 4500 kits have been delivered in 42 countries. [1] A derivative of the Avid Flyer, [3] the Kitfox was an early kit plane to feature quickly-folding wings that greatly simplify carriage and storage. [4] The appeal of the aircraft was that it could be built in a two-car garage.
The horizontal stabilizer, tail fin and wings are also constructed of riveted aluminum tubing with all flying surfaces covered in doped aircraft fabric. The wings and horizontal tail are quick-folding for storage and ground transport. The Slingshot can be made ready to fly from trailering in 15 minutes. [1] [2] [3]
The aircraft has a very small wing for the US ultralight category with a wing area of only 95 sq ft (8.8 m 2) and a wingspan of 17.6 ft (5.4 m). The wing is equipped with flaps that give it a stall speed of 25 mph (40 km/h). The small wing gives the aircraft a high cruise speed and better resistance to turbulence than a lighter-loaded wing.
Two seat side-by-side configuration ultralight trainer, first flown in 1995, with first deliveries in February 1998. Folding wings were a factory option. Standard engine is the 50 hp (37 kW) Rotax 503 or 64 hp (48 kW) Rotax 582 as an option. [1] [2] [3] Phantom I Single seat ultralight aircraft with struts in place of cable-bracing.
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