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The all-metal aircraft is made from sheet aluminum. Its 18.40 ft (5.6 m) span wing lacks flaps and has a wing area of 63.00 sq ft (5.853 m 2). The cabin width is 22 in (56 cm). The acceptable power range is 70 to 100 hp (52 to 75 kW) and the standard powerplant is the 70 hp (52 kW) Volkswagen air-cooled engine.
It is made from 7075-T6 aluminum tubing, with the control bar and kingpost made from 6061-T6 aluminum. The single-surface wing is covered in Dacron sailcloth. Its 39.0 ft (11.9 m) span wing is cable braced from a single kingpost. The nose angle is 115°, wing area is 330 sq ft (30.7 m 2) and the aspect ratio is 5:1. Pilot hook-in weight range ...
The aluminum structure wing, covered in flush riveted aluminum sheet, ... The aircraft was designed for a maximum gross weight of 1,500 lb (680 kg) in the utility ...
He modified the prototype Kitfox Lite to meet FAR 103 regulations requiring an ultralight aircraft to have an empty weight of less than 254 lb (115 kg). [1] [2] [3] [5] The fuselage is made from 4130 steel tubing. Flaperons and vortex generators are used to improve roll control and low speed flight. The wings are foldable for storage. [1] [2] [3]
The Panther is a single seat, low wing aircraft, built of aluminum with a bubble canopy. The forward fuselage is constructed from welded 4130 steel tubing, with the aft fuselage, tail and wings made from 2024-T3 aluminum sheet. The landing gear can be assembled in either tricycle or conventional gear arrangements. The wings are designed to be ...
Its wing has an area of 195 sq ft (18.1 m 2). [3] Falcon 3 Tandem Tandem model for flight training, introduced in 2009. [3] Falcon 4 145 Small-sized model for lighter pilots, HGMA certified in 2015. Its wing has a span of 28 ft (8.5 m), wing area is 145 sq ft (13.5 m 2) and the aspect ratio is 5.4:1. The pilot hook-in weight range is 120 to 190 ...
The B-10's fuselage is made from aluminum tubing while the wing has a birch plywood D-cell leading edge and foam ribs, covered with Dacron sailcloth or doped aircraft fabric. The tailless wing is common to all three variants. [2] It is of tapered and lightly-swept form, employing a NACA 23015 airfoil. It has a span of 36 ft (11.0 m) span wing ...
Data from Ultralight News, Pilot Mix. General characteristics Crew: one Capacity: one (ultralight configuration) Length: 17 ft 3 in (5.26 m) Wingspan: 27 ft 5 in (8.36 m) Height: 5 ft 0 in (1.52 m) varies by main landing gear wheel diameter Wing area: 123 sq ft (11.4 m 2) Empty weight: 254 lb (115 kg) Gross weight: 540 lb (245 kg) Fuel capacity: 5 US gallons (19 litres) Powerplant: 1 × Rotax ...