Search results
Results from the WOW.Com Content Network
The Diehl AeroNautical XTC Hydrolight is an American amphibious flying boat ultralight aircraft that was designed and produced by Diehl AeroNautical in the 1980s. [1] The prototype first flew in March 1982, with production of kits commencing the following year. [2]
The Spratt Controlwing 107 was an unorthodox controlwing flying boat designed in the United States in the 1960s and marketed for home building in the 1970s. [2] The aircraft featured a flat, speedboat-like [3] hull with a square bow and with tailfins blended into each side. [4] [5] The fins were angled to form a butterfly tail and included no ...
The aircraft is made from a combination of metal tubing, with its flying surfaces covered in Dacron sailcloth doped aircraft fabric and a reinforced fiberglass hull. Its 30.83 ft (9.4 m) span wing has a wing area of 150.0 sq ft (13.94 m 2 ) and is supported by a central pylon behind the cockpit, "V" struts and jury struts .
It was a large high-wing flying boat with Allison T40 engines driving six-bladed contra-rotating propellers. It had a sleek body with a single-step hull and a slender high-lift wing with fixed floats. The Navy ordered two prototypes on 27 May 1946. Designated XP5Y-1, the first aircraft first flew on 18 April 1950 at San Diego. In August the ...
Data from Jane's All the World's Aircraft 1982–83 General characteristics Crew: 1 Capacity: 1 passenger Length: 23 ft 6 in (7.16 m) Wingspan: 36 ft 1 in (11.00 m) Height: 8 ft 0 in (2.44 m) Empty weight: 1,032 lb (468 kg) Max takeoff weight: 1,600 lb (726 kg) Fuel capacity: 20 US gal (17 imp gal; 76 L) Powerplant: 1 × Lycoming O-235 four-cylinder horizontally-opposed engine, 115 hp (86 kW ...
The 11.15 m (36.6 ft) span wing is supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar. The powerplant is a twin cylinder, liquid-cooled, two-stroke , dual-ignition 64 hp (48 kW) Rotax 582 engine.
Get AOL Mail for FREE! Manage your email like never before with travel, photo & document views. Personalize your inbox with themes & tabs. You've Got Mail!
Data from Jane's All the World's Aircraft 1958-59 General characteristics Crew: 2 Capacity: 3 Length: 10.8 m (35 ft 5 in) Wingspan: 13.53 m (44 ft 5 in) Height: 3.83 m (12 ft 7 in) Wing area: 25.1 m 2 (270 sq ft) Aspect ratio: 7.4 Airfoil: NACA 230 series Empty weight: 2,110 kg (4,652 lb) Gross weight: 2,994 kg (6,601 lb) Fuel capacity: 730 L (193 US gal; 161 imp gal) in two hull tanks ...