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Summary of aircraft built by Medway Microlights; Model name First flight Number built Type Hybred 44XL [5] 1978 ultralight trike: HybredR: 1982 ultralight trike Raven [5] 1982 ultralight trike Rebel SS [5] 1988 ultralight trike EclipseR: 1989 ultralight trike Av8R: 2003 ultralight trike SLA100 Executive [3] 2003 fixed wing microlight: SLA 80 ...
The Medway SLA100 Executive, also called the Medway SLA 100 Executive, is a British ultralight aircraft designed and produced by Medway Microlights, of Rochester, Kent. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.
The Tiger Cub Developments (TCD) Sherwood Ranger is a single engine, tandem two seat biplane microlight designed and built in the United Kingdom in the early 1990s. Kits were originally produced by TCD; later, design rights were acquired by The Light Aircraft Company Ltd (TLAC) who resumed kit production in 2009.
The British Microlight Aircraft Association (BMAA) is an organisation that governs microlight aircraft in the UK.; [1] it is a member organisation that exists to benefit its members with respect to flying and operating microlight aircraft in the United Kingdom. Its aims are listed in the Articles of Association.
The aircraft complies with the Fédération Aéronautique Internationale microlight rules and UK certified under BCAR Section "S". It features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit accessed via doors, fixed tricycle landing gear or conventional landing gear and a single engine in tractor configuration.
Data from Bertrand, Bayerl and Medway General characteristics Crew: one Capacity: one passenger Wingspan: 11.0 m (36 ft 1 in) Wing area: 15.0 m 2 (161 sq ft) Aspect ratio: 8:1 Empty weight: 208 kg (459 lb) Gross weight: 415 kg (915 lb) Fuel capacity: 42 litres (9.2 imp gal; 11 US gal) Powerplant: 1 × Rotax 912UL four-stroke, four-cylinder aircraft engine, 60 kW (80 hp) Performance Maximum ...
Ultralight aviation (called microlight aviation in some countries) is the flying of lightweight, 1- or 2-seat fixed-wing aircraft. Some countries differentiate between weight-shift control and conventional three-axis control aircraft with ailerons , elevator and rudder , calling the former "microlight" and the latter "ultralight".
Summary of aircraft built by Thruster Air Services; Model name First flight Number built Type Thruster T600 Sprint: mid-1990s Two-seat microlight aircraft
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