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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.
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 ...
The BN-2T-4S Defender 4000 is an enhanced version of the BN-2T Defender intended for the aerial surveillance role. Compared to earlier Defenders, it has a stretched fuselage, the enlarged wing from the Trislander , a new nose structure capable of accommodating an EO/IR sensor and radar , and an increased payload. [ 2 ]
Data from Jane's All the World's Aircraft 1992-93 General characteristics Capacity: 2 Length: 5.30 m (17 ft 5 in) Wingspan: 7.80 m (25 ft 7 in) Height: 1.47 m (4 ft 10 in) Wing area: 9.80 m 2 (105.5 sq ft) Empty weight: 282 kg (622 lb) Max takeoff weight: 500 kg (1,102 lb) Powerplant: 1 × Limbach L2000 4-cylinder horizontally opposed, with water-cooled piston heads, 60 kW (80 hp) Performance ...
Data from Jane's All the World's Aircraft 1988–89 General characteristics Crew: one Length: 13 ft 9 in (4.19 m) Wingspan: 16 ft 8 in (5.08 m) Height: 4 ft 6 in (1.37 m) Wing area: 86.0 sq ft (7.99 m 2) Empty weight: 475 lb (215 kg) Gross weight: 850 lb (386 kg) Fuel capacity: 12 US gal (10.0 imp gal; 45 L) Powerplant: 1 × Continental A-80 Horizontally opposed piston, 80 hp (60 kW ...
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 2si 460 is a family of in-line twin-cylinder, two-stroke, single ignition, aircraft engines that were designed for ultralight aircraft. [1]The basic engine was originally designed and produced by ILO-Motorenwerke of Germany and was later acquired by the AMW Cuyuna Engine Company of Beaufort, South Carolina and marketed under the Cuyuna brand name.
The prototype Fly Baby first flew in 1962, becoming the winner of the Experimental Aircraft Association's 1962 design competition. [1] [2]Variants include a biplane version called the Bowers Bi-Baby or Fly Baby 1-B, [1] [2] a floatplane version, [1] and several dual-cockpit designs by various builders. [2]