Mudry CAP 10 ↗
A French two-seat aerobatic trainer with side-by-side seating and a distinctive curved wing outline.
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A French two-seat aerobatic trainer with side-by-side seating and a distinctive curved wing outline.
A DC-10-derived tanker that combined aerial refuelling with passenger and cargo transport.
A five-seat composite single whose development led to the diesel DA50 RG.
A twin-turboprop utility aircraft developed by Reims Aviation with Cessna.
A compact Italian light twin with a shoulder wing and metal airframe.
Piper's PA-31 utility twin, used in commuter, cargo and corporate transport.
A four-seat high-wing single that spans generations of conventional instruments and glass cockpits.
An enlarged Velocity kit aircraft with a canard and rear-mounted pusher propeller.
TorqueSim's Pocket Rocket, a simulated PT6-powered light aircraft with two gear layouts.
A carbon-fibre aerobatic monoplane family with a dedicated air-racing branch.
An advanced trainer known around the world as the Texan, Harvard and SNJ.
The H130 utility helicopter, descended from the AS350 and fitted with a Fenestron.
A two-seat light amphibian with a compact boat hull and a pusher propeller.
A full-length double-deck airliner built for very high passenger capacity.
A super-midsize business jet with a swept wing, rear-mounted engines and an integrated glass cockpit.
A small two-seat piston helicopter with a two-bladed main rotor.
Piper's two-seat trainer with fixed tricycle landing gear.
A low-wing agricultural Cessna with a cockpit and hopper arranged around the job.
A large twin-radial transport that carried heavy loads through wartime and post-war freight service.
A two-seat composite trainer with a low wing and a large canopy.
A purpose-built aerobatic monoplane family developed by pilot and designer Walter Extra.
A long-range twin whose programme emphasised composite construction and more electrically powered systems.
A six-seat composite single turboprop with a pressurised cabin and retractable gear.
A push-pull twin with one engine at each end of the central fuselage.
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