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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 ...
The Falconar SAL Mustang, also called the 2/3 Mustang and the SAL P-51D Mustang is a Canadian amateur-built aircraft, originally produced by Falconar Avia and introduced in 1969. The aircraft is a 2 ⁄ 3 scale replica of the North American P-51 Mustang and is supplied as a kit or as plans for amateur construction.
Glasair Sportsman 2+2 Diesel A Thielert Centurion 2.0s powered variant. Carbon Sportsman A variant with the fuselage constructed of carbon fiber rather than fiberglass.The weight savings of carbon fiber are negated by heavier duty cage, wing struts, and wing skins; both variants have the same empty weight, but the carbon variant gross weight is increased by 150 lb. [6]
Yes, a flight manual is the ultimate reference for specs I suppose but some editors will check the references. I think 'reliable third party sources' is one of the criteria for references. As far as the level of detail in the specs goes, the fields are laid out using a standard aircraft template which can be filled out as required.
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 ...