The Whisper X350 Generation II is a South African amateur-built aircraft, designed in 2015 and produced by Whisper Aircraft of Mossel Bay. The aircraft was developed from the 2004-designed Whisper Aircraft Whisper motorglider. The X350 Generation II is supplied as a kit for amateur construction. The X350 Generation II designation indicates a design top speed goal of 350 km/h (189 kn), with the larger engine fitted. The aircraft features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit that is 47.2 in (119.9 cm) wide, under an acrylic plastic articulated lift-up bubble canopy. It has fixed optionally tricycle landing gear or conventional landing gear and a single engine in tractor configuration. The aircraft is predominately made from vacuum-bagged, post-cured carbon fibre composites, with E-glass used for non-structural parts, including the engine cowling, aircraft fairings, wing and tail tips. The structure is 10% anodized aluminum and cadmium-plated steel, with the landing gear legs made from steel. The design's 26.17 ft (8.0 m) span wing has an area of 122 sq ft (11.3 m2) and mounts plain flaps and features a cruciform tail. The aircraft's recommended engine power range is 160 to 200 hp (119 to 149 kW) and standard engines used include the 160 hp (119 kW) Lycoming O-320, the 180 hp (134 kW) Lycoming O-360, the 200 hp (149 kW) Lycoming IO-390, or the 180 to 200 hp (134 to 149 kW) ULPower UL520i four-stroke powerplants. The fuel capacity is 32 U.S. gallons (120 L; 27 imp gal) in two fuselage tanks, although future production kits will have 63 U.S. gallons (240 L; 52 imp gal) in a wet wing. The design has a single centre console-mounted side-stick or optional individual centre stick controls. The ailerons are actuated via push rods, while the elevator has push rods to the tailcone and then cables. The rudder is cable-actuated. There is no elevator trim tab system, but it may be included as a future factory option. Evaluation flights indicated neutral longitudinal stability, however, reducing the need for one. The left seat is equipped with toe-brakes. The 51% compliant kit includes a mated fuselage and pre-closed wing structures. The aircraft can be constructed in a two-car garage. Construction time from the supplied kit is estimated by the manufacturer as 500 hours. The design as load factors of +6/-4 g, but is not designed for aerobatics. The instrument panel is made from aluminum. The seats and rudder pedals are independently adjustable. There are optional rear fuselage windows for improved visibility, LED navigation lights and strobe lights on the wing tips and tail. Lightning protection is a factory option. Tricycle gear variant.
