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The BN-2B model involved several changes, including a redesigned cockpit and a reduction in cabin noise levels. [4] In 1980, it was decided to make available turboprop engines for the type, adopting twin Allison 250 -B17C engines; when the latter are installed, the aircraft is designated the BN-2T Turbine Islander .
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 ]
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 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 ...
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 ...
Model name First flight Number built Type Cessna Comet: 1917 1 Single piston engine monoplane sport plane Cessna Model A: 1927 70 Single piston engine monoplane utility airplane Cessna Model BW: 13 Single piston engine monoplane utility airplane Cessna CG-2: Glider Cessna CH-1: 1953 ~50 Single piston engine utility helicopter Cessna CH-4
Data from Pitts model 12.com General characteristics Capacity: 2 Length: 20 ft 6 in (6.25 m) Wingspan: 23 ft (7.0 m) Empty weight: 1,550 lb (703 kg) Gross weight: 2,250 lb (1,021 kg) Fuel capacity: 54 gal Powerplant: 1 × Vedeneyev M14P/PF, 360 hp (270 kW) Propellers: 3-bladed MT Propeller Performance Cruise speed: 150 kn (170 mph, 270 km/h) Stall speed: 56 kn (64 mph, 103 km/h) Range: 430 nmi ...