DG Aviation DG-1001E ↗
A tandem two-seat sailplane family used for training and cross-country soaring.
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A tandem two-seat sailplane family used for training and cross-country soaring.
Piper's two-seat trainer with fixed tricycle landing gear.
A two-seat amphibian with a flying-boat hull and a pusher engine above the cabin.
A six-engine flying boat created for long-distance passenger travel over water.
A midsize business jet developed by Bombardier’s Learjet division.
A very light twin jet developed from the Eclipse 500.
A two-seat training single with a high wing and fixed tricycle landing gear.
A very large single-engine biplane designed for practical work from modest airfields.
The second-generation Harrier, designed around vectored thrust and short-field operation.
A twin-turbine Huey descendant with a four-blade main rotor.
A high-wing utility turboprop designed for short-field passenger and cargo work.
An open, single-seat ultralight with its propeller behind the pilot.
The four-engine wide-body whose raised flight deck created one of aviation's most recognisable profiles.
A regional turboprop family whose short early versions and larger Q400 have different proportions and systems.
A simulated twin-turbine helicopter that explores no-tail-rotor anti-torque control.
A side-by-side touring motorglider used for both powered flying and soaring.
A twin-radial military transport with a rear ramp and short-field design priorities.
Pipistrel's streamlined four-seat composite-aircraft design.
A single-seat competition sailplane offered in Standard and 18-metre configurations.
A tandem two-seat sailplane designed for instruction and broader soaring use.
The tip-tanked turbofan Learjets, combining the classic compact airframe with longer range and careers in business, military and medical flying.
A European variable-sweep combat-aircraft family with distinct strike and interceptor versions.
A twin-turboprop family whose smaller conventional-tail and larger T-tail branches have distinct identities.
A push-pull twin with one engine at each end of the central fuselage.
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