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Cockpit of a BN-2 Islander. The Britten-Norman BN-2 Islander is a high-wing cantilever monoplane with a rectangular fuselage and two wing-mounted engines; early aircraft were equipped with a pair of piston engines while later production models may be alternatively fitted with turboprop engines in their place.
This brief developed into the BN-2 Islander, and the Britten-Norman company was formed to produce the aircraft, which first flew in 1965. During the 1960s, Britten-Norman were involved in the development of hovercraft via their subsidiary Cushioncraft Ltd; [6] their first craft, the CC1, was the world's second hovercraft.
Data from Jane's All The World's Aircraft 1976–77 General characteristics Crew: 1 or 2 Capacity: 16 or 17 passengers Length: 49 ft 3 in (15.01 m) Wingspan: 53 ft 0 in (16.15 m) Height: 14 ft 2 in (4.32 m) Wing area: 337.0 sq ft (31.31 m 2) Aspect ratio: 7.95:1 Airfoil: NACA 23012 Empty weight: 5,842 lb (2,650 kg) Max takeoff weight: 10,000 lb (4,536 kg) Fuel capacity: 154 imp gal (185 US gal ...
In 1951 Peter Gatrell, John Britten & Desmond Norman built and flew an ultra-light monoplane, their first aircraft, which made its first flight at Bembridge, Isle of Wight, on 16 May 1951. This machine crashed on an early flight, when the petrol supply to the 40 hp Aeronca-J.A.P. J-99 twin cylinder air-cooled engine faded out. [2]
The Harrier, informally referred to as the Harrier jump jet, is a family of jet-powered attack aircraft capable of vertical/short takeoff and landing operations (V/STOL). ). Named after the bird of prey, [1] it was originally developed by British manufacturer Hawker Siddeley in the 1
Q-2/Q-200 pilot controls included a central sidestick controlled by the right hand and a throttle controlled by the left hand. As the pitch and roll control linkages were via a pushrod, the aircraft was very responsive. Routine installations were the inclusion of an aileron reflexor and mid-fuselage belly-board speed brake.
Development of the Sling 2 commenced in 2006. The Sling is a two-seat, low wing, all metal aircraft with tricycle landing gear made from composites. The aircraft is powered by an 80 hp (60 kW) Rotax 912UL,100 hp (75 kW), a Rotax 912ULS, or a 912iS engine, or optionally a turbocharged 115 hp (86 kW) Rotax 914 UL, driving a 3-bladed Warp Drive Inc propeller.
The aircraft has a notably high useful load of 279 kg (615 lb). The landing gear is of tricycle configuration. [2] [4] [5] After 42 examples had been completed, the aircraft was introduced into the US market in September 2011 at the AOPA Summit. [2] By 31 December 2020, the company reported over 600 had been delivered. [1]