McDonnell Douglas MD-80 / MD-82 ↗
A stretched development of the DC-9 with rear-mounted engines and a five-abreast cabin.
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A stretched development of the DC-9 with rear-mounted engines and a five-abreast cabin.
A twin-engine utility helicopter with roots in the BK 117 and EC145 families.
A heavy-lift helicopter built around an open frame and an external working load.
A cabin biplane with the lower wing placed ahead of the upper one.
An Italian light aircraft known for military training and aerobatic use.
A compact twin-engine helicopter widely used for medical, police and training work.
A purpose-built aerobatic monoplane family developed by pilot and designer Walter Extra.
A cabin-class piston twin designed for commuter, cargo and utility work.
A lightweight pusher family with an enclosed cabin and a high, braced wing.
A compact utility helicopter distinguished by its enclosed Fenestron tail rotor.
A compact twin-engine transport helicopter with retractable gear and a long development history.
A French two-seat aerobatic trainer with side-by-side seating and a distinctive curved wing outline.
A modern composite twin with a roomy cabin and two wing-mounted piston engines.
A shorter wide-body Airbus from the transition to two-pilot, electronic-instrument cockpits.
A five-seat composite single whose development led to the diesel DA50 RG.
A five-seat turbine helicopter developed from Robinson's smaller piston-helicopter line.
The fixed-gear, six-cylinder touring branch of Piper's PA-28 family.
Regional flying built around a high wing, two turboprops and short sectors.
A four-engine tactical transport built around a rear loading ramp and access to austere airfields.
An open, single-seat ultralight with its propeller behind the pilot.
A modern utility single whose family includes both tailwheel and nosewheel configurations.
A four-seat kit-built touring aircraft that expanded the RV family beyond two-seat designs.
A twin-radial military transport with a rear ramp and short-field design priorities.
A push-pull twin with one engine at each end of the central fuselage.
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