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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 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 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 ...
The IO-520 series engines normally produce 285 to 310 horsepower (210 to 230 kW) and are used in numerous aircraft such as certain models of the Bellanca Viking 300 and Super Viking, the Beech Bonanza and Baron, and Cessna 185- 206-, 210-, 310-, and 400-series aircraft. The IO-520 remained in production in 2019.
In 2003 it was reported that 298 engines had been sold to RV builders. [ 3 ] In 2010 Eggenfellner founded a new company to produce the Viking 110 light-sport aircraft engine, Viking Aircraft Engines .
Data from Jane's All the World's Aircraft 1976–77 General characteristics Crew: 1 Capacity: 3 passengers Length: 26 ft 4 in (8.03 m) Wingspan: 34 ft 2 in (10.41 m) Height: 7 ft 4 in (2.24 m) Wing area: 161.5 sq ft (15.00 m 2) Airfoil: Bellanca B Empty weight: 2,217 lb (1,006 kg) Max takeoff weight: 3,325 lb (1,508 kg) Fuel capacity: 60 US gal (50 imp gal; 230 L) usable fuel (normal), 75 US ...
This is an accepted version of this page This is the latest accepted revision, reviewed on 9 November 2024. British airliner with 2 piston engines, 1945 This article is about the post-World War II airliner. For the earlier single-engined amphibian, see Vickers Viking. This article includes a list of general references, but it lacks sufficient corresponding inline citations. Please help to ...
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.