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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 ...
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 ]
Hydrogen fuel could save £150,000–£300,000 annually over fossil fuel, maintenance costs should fall by 50% for the propulsion system, and 15% for the whole aircraft. [5] Rolls-Royce plc left the consortium, while engineering company Ricardo plc will integrate the two 250 kW (340 hp) fuel cells and Innovatus Technologies the composite ...
Aer Arann Islands was established as Aer Arann in 1970 by James Coen, Ralph Langan, and Colie Hernon [2] to provide an island-hopping air service between Galway and the Aran Islands off the west coast of Ireland. Operations, using a single Britten-Norman Islander, began in August 1970.
Data from Jane's All the World's Aircraft 1988-1989 General characteristics Crew: 2 Length: 8.33 m (27 ft 4 in) Wingspan: 7.92 m (26 ft 0 in) Height: 3.25 m (10 ft 8 in) Wing area: 11.89 m 2 (128.0 sq ft) Aspect ratio: 5.28:1 Airfoil: NACA 23012 Empty weight: 1,117 kg (2,463 lb) Max takeoff weight: 1,633 kg (3,600 lb) Fuel capacity: 405 L (89 imp gal; 107 US gal) internal fuel Powerplant: 1 × ...
With the military designation Bn.2 (2-seat night bomber) the aircraft were delivered to squadrons within 1e Groupe de Bombardement. Three escadrilles (S25, F114 and F119) had been equipped by the time of the Armistice in November 1918, with 45 F.50s in service. [ 1 ]
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