Tecnam P2010 ↗
Tecnam's four-seat high-wing single, built with metal and carbon-fibre components.
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Tecnam's four-seat high-wing single, built with metal and carbon-fibre components.
A compact regional turboprop with a pressurised cabin for up to 19 passengers.
An experimental twin-boom racing aircraft commissioned by Bob Pond and designed by Burt Rutan.
A large long-haul twin that introduced Boeing's first commercial fly-by-wire airliner flight controls.
A light two-seat helicopter with a side-by-side cabin and a semi-rigid main rotor.
An enclosed, two-seat autogyro with side-by-side seating and a pusher propeller.
A tandem-seat canard homebuilt with a pusher engine and distinctive winglets.
A two-seat touring motorglider with interchangeable wing tips.
A large twin-engine helicopter from the Super Puma line, used for offshore and public-service work.
A turbine-powered utility helicopter with a broad cabin and a long international service history.
A radial-engined utility aircraft closely associated with bush flying and float operations.
A compact aerobatic biplane family with both single-seat and tandem-seat branches.
A small two-seat piston helicopter with a two-bladed main rotor.
A fixed-gear twin turboprop with a long history in regional and remote-area transport.
A three-engine airliner that became a mainstay of Soviet and Russian passenger transport.
A two-seat amphibian with a flying-boat hull and a pusher engine above the cabin.
A purpose-built agricultural aircraft that also became a single-engine air tanker.
A narrow-body twin developed as a new generation of medium-range airliner.
A four-seat composite touring and training aircraft developed from Diamond's smaller two-seater.
A late-1930s cabin aircraft with metal construction and retractable landing gear.
Piper's two-seat trainer with fixed tricycle landing gear.
Cirrus's first type-certified aircraft, a composite piston single.
A four-seat, pressurised kit aircraft with a composite airframe and retractable landing gear.
A push-pull twin with one engine at each end of the central fuselage.
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