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The wings are identical to the Bearhawk 4-Place Model B, employing the same Riblett 30-413.5 airfoil [5] and mounting flaps. [4] The aircraft's recommended engine power range is 250 to 315 hp (186 to 235 kW) and standard engines used include the 250 hp (186 kW) Lycoming O-540 , although the recommended engine is the 315 hp (235 kW) Lycoming IO ...
The Bearhawk was designed in the early 1990s [5] as a personal project by Barrows to carry aircraft engines for delivery as freight. It features a strut-braced high-wing, a four-seat enclosed cabin that is 42.5 in (108 cm) wide and accessed by doors, fixed conventional landing gear and a single engine in tractor configuration.
Bearhawk Model 5. Barrows is the designer of the Bearhawk Patrol, Companion, 4-Place, and Model 5 light aircraft, [3] as well as the Bearhawk LSA light-sport aircraft. [4]Prior to designing the first aircraft in the Bearhawk series, the 4-Place, Barrows designed and built a STOL high wing plane called the Grasshopper and an aerobatic biplane. [5]
A section of the rear fuselage from a Vickers Warwick showing the geodetic construction in duralumin. On exhibit at the Armstrong & Aviation Museum at Bamburgh Castle.. A geodetic airframe is a type of construction for the airframes of aircraft developed by British aeronautical engineer Barnes Wallis in the 1930s (who sometimes spelt it "geodesic").
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The aircraft involved was a Boeing 737-7H4 [b] with manufacturer's serial number 27880, fuselage line number 601, and registered as N772SW. [3] The aircraft had been in service with Southwest Airlines for nearly 18 years since its manufacture in 2000. [4] It was powered by two CFM International CFM56-7B24 engines. [2] [5]
Officials said an F-35 fighter jet crashed in Alaska on Tuesday after the pilot managed to safely eject from the aircraft – the latest mishap involving the U.S. military's most expensive weapon ...
Propeller broke apart; one of the blades punctured the fuselage, causing the forward section to break away 1967-06-23 Mohawk Airlines Flight 40: Pennsylvania, United States BAC One-Eleven 204AF: Mechanical failure 34 Valve in the auxiliary power unit suffered a complete failure, spreading fire to the tailplane and causing a loss of pitch control