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The aluminum block Viking 110 has electronic ignition and multi-port fuel injection. It was introduced in 2009 and is based upon the 2009 model Honda Fit automotive engine. It produces 110 hp (82 kW) through a mechanical gear reduction drive with helical gears, with a reduction ratio of 2.33:1. A Warp Drive Inc propeller is recommended.
The Aircraft Bluebook Price Digest is a quarterly print publication by Informa (also available on CD-ROM) that was established in the 1950s. It identifies and prices more than 3,000 used general aviation aircraft and helicopter make and model-years available in the United States. Prices reflect historical data and cannot, therefore, take into ...
The earliest versions, developed in 1965, had a sea-level thrust of about 190 kN. By 1971, the thrust had improved to 540 kN, with resulting engine named Viking 1 and adopted for the Ariane program. The engine first flown on the Ariane 1 rocket in 1979 was Viking 2, with thrust further improved to 611 kN.
The cockpit is 39 in (99 cm) wide and has a baggage compartment with a limit of 70 lb (32 kg), located behind the seats. The aircraft's recommended engine power range is 60 to 82 hp (45 to 61 kW) and standard engines used include the 82 hp (61 kW) Volkswagen four-stroke powerplant. Construction time from the supplied kit is estimated as 1700 ...
Developed by GE Aircraft Engines during the late 1960s, the original engine comprises a single stage fan, driven by a 4-stage low pressure (LP) turbine, supercharging a 14-stage high pressure (HP) compressor, driven by a 2-stage HP turbine. An annular combustor is featured.
[17] [18] During 2008, Bombardier and Viking Air reached an arrangement under which the former sold the design documents and all intellectual property rights of all out-of-production de Havilland aircraft from the DHC-1 Chipmunk through the DASH-7 50 passenger STOL regional airliner to Viking. [19] [20] Its unit cost in 2014 was 36.9 million US ...
The Dragonfly is a two-seater aircraft that features a tandem wing layout with a forward wing mounted low and the other behind the cockpit in a shoulder position, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed landing gear and a single engine in tractor configuration. The cockpit is 43 in (109 cm) wide [3]
It is commonly registered as a light-sport aircraft in the United States and as an ultralight in some other jurisdictions and is considered a microlight aircraft in New Zealand. Manufacture (both ready to fly and kits) is done in the ICP premises located in Castelnuovo Don Bosco ( Piedmont , Italy ), where the firm moved on September 10, 2009 ...