Piper PA-28-236 Dakota ↗
The fixed-gear, six-cylinder touring branch of Piper's PA-28 family.
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The fixed-gear, six-cylinder touring branch of Piper's PA-28 family.
A wide-cabin business-jet family that developed from Canadair's original Challenger programme.
A specialised reconnaissance aircraft designed for very high altitude and sustained supersonic flight.
SOCATA's touring-aircraft family, including the Tobago and Trinidad.
A full-length double-deck airliner built for very high passenger capacity.
A three-engine airliner that became a mainstay of Soviet and Russian passenger transport.
Lockheed's wide-body TriStar, with three RB211 engines and a distinctive tail intake.
A tandem-seat utility aircraft whose light structure and high wing suit bush, towing and recreational work.
A four-bladed utility helicopter developed from the LongRanger lineage.
A cabin-class piston twin designed for commuter, cargo and utility work.
A rear-engined trijet built to bring jet service to shorter routes and smaller airports.
A stretched development of the DC-9 with rear-mounted engines and a five-abreast cabin.
A modern composite twin with a roomy cabin and two wing-mounted piston engines.
A compact regional turboprop with a pressurised cabin for up to 19 passengers.
A purpose-built agricultural aircraft that also became a single-engine air tanker.
Piper's two-seat trainer with fixed tricycle landing gear.
Epic's experimental light-jet project, represented in simulation by Aerobask.
A four-abreast regional-jet family spanning the E170, E175, E190 and E195.
A large twin-radial transport that carried heavy loads through wartime and post-war freight service.
An all-metal sport and touring aircraft from Bayerische Flugzeugwerke.
A compact utility helicopter distinguished by its enclosed Fenestron tail rotor.
An electric-powered educational glider concept inspired by the human-powered MIT Daedalus 88.
A twin-engine business jet designed to retain some of the utility flexibility associated with the PC-12.
A push-pull twin with one engine at each end of the central fuselage.
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