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SA-11A with folded wings. The SA-11A is a single engine, side-by-side configuration seating, tricycle gear, strut-braced, low wing monoplane. The fuselage is welded steel tubing with aircraft fabric covering. [2] The wings have a quick release mechanism that allows them to fold and lock alongside the fuselage in 15–30 seconds.
The Grumman-patented Sto-Wing aftwards-folding wing folding system, pioneered on the Grumman F4F-4 Wildcat, has been used since World War II on a number of Grumman-designed carrier aircraft, [4] [5] a version of which is still in use in the 21st century on the Grumman E-2 Hawkeye shipboard airborne early warning (AEW) aircraft and its C-2 ...
The SA-5 is a mid-wing, tricycle landing gear design with folding wings. The aircraft was intended to be towed by a vehicle by the (lowered) tail on its main gear with wings folded along its sides. The cockpit can be open, or covered with a bubble canopy. The fuselage is constructed from welded steel tubing with aircraft fabric covering.
The Dyke Delta JD-2 is an American homebuilt aircraft designed in the United States in the 1960s and marketed for amateur construction. It is a monoplane with retractable tricycle undercarriage and seating for four. The wings can be folded for towing or storage and hinge upwards to lie flat above the fuselage, one atop the other. [1]
In reviewing the aircraft Andre Cliche said: The Twinstar Mk III is a very clean and aerodynamic design. lt looks fast and flies fast. With standard dual controls, it can be used as a trainer, but it is most often used as a cross-country cruiser. It is especially desirable for its folding wings. [3]
The wings are built from aluminium tube and ribs, feature flaps, and are folding or removable. [ 1 ] [ 2 ] [ 5 ] The present-day S-12XL is powered by the Rotax 503 of 50 hp (37 kW), with the Rotax 582 of 64 hp (48 kW), the Rotax 912UL of 80 hp (60 kW) and the Rotax 912UL of 100 hp (75 kW) available as options.
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. Production completed.
The aircraft was certified and put into production in Hungary for sale in Europe. In North America the Cuby II was sold for US$15,662.76, complete with propeller, 50 hp (37 kW) Rotax 503 powerplant, paint and fabric in 1988. Available options included folding wings, floats and an agricultural spray kit. [2] [3]
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