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Download as PDF; Printable version; In other projects Wikidata item; Appearance. move to sidebar hide ... {Aircraft specs | ref = <!-- the reference for the data ...
Data from British Civil Aircraft since 1919 General characteristics Crew: 1 Capacity: 2 passengers Length: 23 ft 3 in (7.09 m) Wingspan: 36 ft 0 in (10.97 m) Height: 8 ft 11 in (2.72 m) Wing area: 184 sq ft (17.1 m 2) Aspect ratio: 7:1 Airfoil: NACA 23012 Empty weight: 1,600 lb (726 kg) Gross weight: 2,400 lb (1,089 kg) Fuel capacity: 23 imp gal (28 US gal; 100 L) Powerplant: 1 × de Havilland ...
The aircraft was certified for intentional spins. [3] While it is an all-metal design, the Skipper incorporated a number of innovative construction techniques, including tubular spars and aluminum honeycomb construction with metal-to-metal bonding, a technique inherited from the Musketeer family. [ 5 ]
The weight of the aircraft when unloaded—no crew, passengers, cargo, or fuel. {{{loaded weight main}}}, {{{loaded weight alt}}} The weight of the aircraft when loaded for a 'typical' mission. This statistic is cited for almost any aircraft, but it is relatively arbitrary, so only use statistics given in sources.
The MB-1 Colibri first flew in 1965 and served as a development aircraft for the definitive MB-2 Colibri 2 that flew in 1970. These aircraft had all-wooden framework with fabric-covered wings and plywood-covered fuselages. The pilot's seat was enclosed by an expansive bubble canopy. In 1976-77, Brügger built and flew an all-metal version as ...
The family had formed the Call Aircraft Company (known as Call-Air) to produce the aircraft. The prototype Model A was powered by a Continental A-80 engine but was redesignated the Model A-1 when re-engined with an Avco Lycoming O-235-A engine.
A higher-performance design revision was granted FAA approval as the 14-19 Cruisemaster on September 26, 1949. [2] The new model had structural upgrades, a 190 hp (142 kW) Lycoming O435-A engine, an increased gross weight of 2,600 lb (1,179 kg), hydraulically operated landing gear and flaps, and an improved interior. 99 of these airplanes were produced between 1949 and 1951.
The CAB GY-20 Minicab is a two-seat light aircraft designed by Yves Gardan and built in France by Construction Aeronautiques du Bearn (CAB) [2] in the years immediately following World War II. CAB was formed in 1948 by Yves Gardan, Max Lapoerte and M. Dubouts.
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