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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 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 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]
The aircraft is a single place, single engine gull-wing design with retractable conventional landing gear. The F4U was the second completed aircraft in the W.A.R. series, with the first example displayed at the EAA airshow in 1975. The aircraft featured folding wings. [3]
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 .
The ribs are made from aluminium sheet and the wing is covered in the same material. The fuselage is built from aluminium tubing, riveted together. A cockpit streamlined pod was optional. The design has folding wings and was intended for trailering from the onset. [2] [3] The standard engine for the A-10 is the 28 hp (21 kW) Rotax 277, but the ...
The Rand Robinson KR-1 is a single-seat, single-engine sport aircraft designed in the United States in the early 1970s and marketed for homebuilding. [1] [2] [3] A two-seat version is marketed as the KR-2. [1] [2] [3] It is a low-wing cantilever monoplane of conventional design with an enclosed cockpit and tailwheel undercarriage.