Tecnam P2008 ↗
A two-seat Tecnam high-wing aircraft combining composite and metal construction.
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A two-seat Tecnam high-wing aircraft combining composite and metal construction.
A midsize business jet developed by Bombardier’s Learjet division.
Avro's delta-wing bomber, developed for Britain's postwar strategic force.
The H130 utility helicopter, descended from the AS350 and fitted with a Fenestron.
A pressurised single turboprop with a large cargo door and a broad range of working roles.
A tandem-seat light aircraft with a streamlined low-wing layout.
A tandem two-seat sailplane designed for instruction and broader soaring use.
Diamond's four-seat light twin, developed with diesel-powered versions.
A low-wing piston twin that carries the Beechcraft touring-aircraft lineage into two-engine flying.
Airbus's first production aircraft, built around a twin-engine wide-body layout.
A streamlined twin-engine helicopter with a Fenestron tail rotor and retractable landing gear.
A long-range fighter whose different engine and canopy developments produced several distinct forms.
A purpose-built aerobatic monoplane family developed by pilot and designer Walter Extra.
A long-haul twin whose family spans passenger, freight and specialist transport roles.
Cirrus's first type-certified aircraft, a composite piston single.
SOCATA's touring-aircraft family, including the Tobago and Trinidad.
A two-seat composite light-aircraft family with a high wing and a compact enclosed cabin.
A long-range strategic bomber with a swept wing and eight jet engines in paired pods.
A long-running touring single, familiar in both V-tail and conventional-tail forms.
A two-seat composite trainer with a low wing and a large canopy.
A tandem-seat utility aircraft whose light structure and high wing suit bush, towing and recreational work.
A high-wing utility aircraft known for short-field work and a broad choice of working configurations.
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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