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Quicksilver MX Quicksilver MX II Sprint two seater Quicksilver Sport 2S, showing its struts, in place of wire bracing Quicksilver C The C model was the earliest powered version and consisted of the Quicksilver hang glider, including the weight-shift sling seat, with a McCulloch MAC 101 powerplant of 12 hp (9 kW), a V-belt reduction drive and a 1.7 US gal (6 L) fuel tank.
Quicksilver Aircraft is an American manufacturer of ultralight and light aircraft.Founded in 1972 as Eipper Formance and later Eipper Aircraft, [1] the company today claims to be the leading manufacturer of ultralight aircraft in the United States, [2] with the Quicksilver type ultralight being used to train more ultralight pilots than any other type.
Data from Cliche and M-Squared General characteristics Crew: one Capacity: one passenger Length: 19 ft 0 in (5.79 m) Wingspan: 32 ft 9 in (9.98 m) Height: 7 ft 10 in (2.39 m) Wing area: 180 sq ft (17 m 2) Empty weight: 475 lb (215 kg) Gross weight: 1,400 lb (635 kg) Fuel capacity: 8 US gallons (30 litres) Powerplant: 1 × Rotax 582, 64 hp (48 kW) Propellers: 2-bladed, 5 ft 8 in (1.73 m ...
[1] [2] [9] ASAP at one time owned GSC Propellers who made a line of wooden blade, aluminum hub, ground adjustable propellers for the ultralight aircraft market. Founded in 1984 GSC Propellers initially operated from the ASAP Vernon facility. The company was sold in 2000 and, while still located in Vernon, changed its name to GSC Systems in 2004.
Data from OPERATORS MANUAL FOR ENGINE TYPES 447, 503 & 582 General characteristics Type: two-stroke air-cooled aeroengine Bore: 72 mm (2.84 in) Stroke: 61 mm (2.4 in) Displacement: 496.7 cc (30.31 cu in) Dry weight: 31.4 kg (69 lb) (dry, no exhaust system) Components Valvetrain: piston ports Fuel system: pneumatic pump pressurized Fuel type: regular autofuel Oil system: premixed in the fuel at ...
The aircraft closely resembles the contemporary Quicksilver MX. [1] [2] The aircraft is made from bolted-together aluminum tubing, with the wings and tail surfaces covered in Dacron sailcloth. Its 32 ft (9.8 m) span wing is cable-braced from a single tube kingpost. The landing gear does not incorporate suspension.
Data from Cliche and the Virtual Ultralight Museum General characteristics Crew: one Wingspan: 33 ft (10 m) Wing area: 165 sq ft (15.3 m 2) Empty weight: 238 lb (108 kg) Gross weight: 518 lb (235 kg) Fuel capacity: 5 U.S. gallons (19 L; 4.2 imp gal) Powerplant: 1 × Cuyuna UL II twin cylinder, Two-stroke aircraft engine, 35 hp (26 kW) Performance Maximum speed: 55 mph (89 km/h, 48 kn) Cruise ...
American Aerolights Falcon. American Aerolights Inc. was an American aircraft manufacturer founded by Larry Newman.The company specialized in the design and manufacture of ultralight aircraft in the form of kits for amateur construction and ready-to-fly aircraft under the US FAR 103 Ultralight Vehicles rules.