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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 wings are strut-braced and utilize jury struts. The wings and tail surfaces are covered in pre-sewn Dacron envelopes, which reduces construction time. The wings have full-span ailerons, while the tail features conventional elevators and rudder. The landing gear is a tricycle gear arrangement with bungee suspension on the main wheels. The ...
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 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.
The aircraft is marketed in the United States as a Light Sport Aircraft, and as an ultralight in most of Europe. It is a high-wing design, mostly using engines from the Rotax 912 family. [1] It was developed from the similar Remos Gemini Ultra. The Mirage has the same layout, landing gear and structure but has a span reduced by 1.00 m (3 ft 3 ...
The Savannah is a two-seat aircraft of conventional configuration and metal semi-monocoque construction. The high wing is braced to the fuselage by V-struts. Most variants have a constant-chord wing with combined flaperons. Initial models were fitted with full-span leading edge slots. The cabin seats two side by side under the wing.
The Sadler SV-1 Vampire is a single-seat ultralight sport aircraft developed in the United States in the early 1980s. [1] It is uncharacteristic of ultralight designs in both its layout and its construction. The Vampire is a mid-wing cantilever monoplane of pod-and-boom configuration and twin booms joined by a common horizontal stabilizer. [1]
He modified the prototype Kitfox Lite to meet FAR 103 regulations requiring an ultralight aircraft to have an empty weight of less than 254 lb (115 kg). [1] [2] [3] [5] The fuselage is made from 4130 steel tubing. Flaperons and vortex generators are used to improve roll control and low speed flight. The wings are foldable for storage. [1] [2] [3]