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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.
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.
Data from Manufacturer's website & Kitplanes General characteristics Crew: one Length: 16 ft 6 in (5.03 m) Wingspan: 30 ft 6 in (9.30 m) Height: 5 ft 0 in (1.52 m) Wing area: 120 sq ft (11 m 2) Empty weight: 254 lb (115 kg) Gross weight: 535 lb (243 kg) Fuel capacity: 5 US Gallons (19 litres) Powerplant: 1 × Hummel Half VW 1037 cc four-stroke, two-cylinder horizontally opposed aircraft engine ...
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 ...
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 Tuholer is a tandem two-seat, strut-braced, low-wing, open cockpit aircraft with conventional landing gear. The dual control aircraft can be flown solo from the rear cockpit only. The fuselage is welded steel tubing with wooden stringers and fabric covering. [3] The dual wing spars are wood, with wood ribs and fabric covering.
The Falconar AMF-S14 Maranda is a two-seat, light aircraft first flown in Canada in 1961 and originally marketed for amateur construction by Falconar Avia. [ 1 ] Since the winding up of business by Falconar Avia in 2019, the plans are now sold by Manna Aviation .