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The CAC Boomerang is a fighter aircraft designed and manufactured in Australia by the Commonwealth Aircraft Corporation between 1942 and 1945. Approved for production shortly following the Empire of Japan's entry into the Second World War, the Boomerang was rapidly designed as to meet the urgent demands for fighter aircraft to equip the Royal Australian Air Force (RAAF).
The Rutan Model 202 Boomerang is an aircraft designed and built by Burt Rutan, with the first prototype taking flight in 1996. [1] The design was intended to be a multi-engine aircraft that in the event of failure of a single engine would not become dangerously difficult to control due to asymmetric thrust .
The Whitney Boomerang DW200 is a two-seat, fixed tricycle gear general aviation airplane, originally designed for flight training, touring and personal use. It can be seen in active service at Darwin International , Brisbane's Archerfield and Perth's Jandakot general aviation airports.
Aircraft with ventral fins under the fuselage for stability which had to be folded for takeoff and landing include the Mikoyan-Gurevich MiG-23, the MiG-27, and the Vought XF8U-3 Crusader III. An example of aircraft using folding wingtips other than stowage/hangar space such as aerodynamics and flight handling was the North American XB-70 ...
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Faulty repair after same plane suffered a tailstrike: the rear bulkhead failed which caused the tail fin to fall off and rupture all four hydraulic systems. The crash remains the deadliest single-aircraft accident in aviation history. 1987-11-28 South African Airways Flight 295: Indian Ocean, 134 nautical miles (248 km) north-east of Mauritius,
Two Icon employees were killed in the accident: lead engineer and chief company test pilot Jon Karkow, who was the pilot in command, and Cagri Sever, Icon's director of engineering, who was a passenger on the flight. Karkow had been involved in the design of the A5's folding wings as well as parts of the aircraft's control systems.
The vertical stabilizer is the fixed vertical surface of the empennage. A vertical stabilizer or tail fin [1] [2] is the static part of the vertical tail of an aircraft. [1] The term is commonly applied to the assembly of both this fixed surface and one or more movable rudders hinged to it.