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Encyclopedia > Fokker Universal
Fokker Universal
G-CAJD from Western Canada Airways, c.1928
Type Airliner, Utility aircraft
Manufacturer Fokker Aircraft Company (Atlantic Aircraft Corporation)
Designed by Robert B.C. Noorduyn
Introduced 1926
Produced 1926-1931
Number built 44
Unit cost 1926 $14,200 (USD) [1]

The Fokker Universal of "Standard" was the first aircraft built in the United States that was based on the designs of Dutch-born Anthony Fokker, who had designed aircraft for the Germans during the First World War. About half of the 44 Universals that were built between 1926 and 1931 in the United States were used in Canada. Among the famous pilots who flew the Fokker Universal were Punch Dickins and Walter Gilbert. Image File history File linksMetadata Size of this preview: 800 × 407 pixels Full resolution (2159 × 1099 pixel, file size: 1,007 KB, MIME type: image/jpeg) I, the creator of this work, hereby release it into the public domain. ... An Airbus A340 airliner operated by Air Jamaica An airliner is a large fixed-wing aircraft with the primary function of transporting paying passengers. ... An aerospace manufacturer is a company or individual involved in the various aspects of designing, building, testing, selling, and maintaining aircraft, aircraft parts, missiles, rockets, and/or spacecraft. ... Fokkers first airplane, the Spin (1910) Fokker was a Dutch aircraft manufacturer named after its founder, Anthony Fokker. ... Robert B.C. Noorduyn (6 April 1893 in Nimwegen, the Netherlands - 22 February 1959 in South Burlington, Vermont) was an aircraft designer and manufacturer. ... Look up aircraft in Wiktionary, the free dictionary. ... Anton Herman Gerard Anthony Fokker (April 6, 1890 – December 23, 1939), was born in Kediri (Dutch East Indies, now Indonesia) and became a Dutch aircraft manufacturer. ... Ypres, 1917, in the vicinity of the Battle of Passchendaele. ... Clennell Haggerston Punch Dickins OBE,DFC (January 12, 1899 - August 3, 1995) was a pioneering aviator and bush pilot. ...

Contents

Design and development

Anthony Fokker established the Atlantic Aircraft Corporation at the Teterboro Airport of Hasbrouck Heights, New Jersey. One of his first ventures for the new company was building other aircraft under license. In 1926, he formulated plans to create an original aircraft designed for utility and air transport. The design was spearheaded by Robert Noorduyn and based on conventional Fokker designs. The mixed-material construction featured a welded steel tube frame for the fuselage and tail surfaces that were covered in fabric as well as a large wing constructed of wood with a wingspan of 14.55 metres, mounted above the fuselage. Although the overall design was quite "clean," all cables, horns and attachments were mounted externally, adding considerably to the drag. FAA diagram of Teterboro Airport (TEB) Main article: Transportation in New York City Teterboro Airport (IATA: TEB, ICAO: KTEB) is a general aviation reliever airport located in the Boroughs of Teterboro, Moonachie, and Hasbrouck Heights in Bergen County, New Jersey[1]. It is operated by the Port Authority of New... Map highlighting Hasbrouck Heights location within Bergen County. ... It has been suggested that this article be split into multiple articles. ... Robert B.C. Noorduyn (6 April 1893 in Nimwegen, the Netherlands - 22 February 1959 in South Burlington, Vermont) was an aircraft designer and manufacturer. ... Fokkers first airplane, the Spin (1910) Fokker was a Dutch aircraft manufacturer named after its founder, Anthony Fokker. ... The fuselage can be short, and seemingly unaerodynamic, as in this Christen Eagle 2 The fuselage (from the French fuselé spindle-shaped) is an aircrafts main body section that holds crew and passengers or cargo. ... Empennage is an aviation term used to describe the tail portion of an aircraft. ... A Laughing Gull with its wings extended in a gull wing profile Aircraft wing planform shapes: a swept wing KC-10 Extender (top) refuels a trapezoid-wing F/A-22 Raptor A wing is a surface used to produce lift and therefore flight, for travel in the air or another...


When the Fokker Universal was first developed in 1925, it had a 200 hp Wright J-4 or a 220 hp J-5 engine. Later models of the aircraft were powered by 330 hp J-6 engines. Two gas tanks were mounted in the wings near the forward edge. As typical of the era, the pilot sat in an open cockpit forward to the wing’s leading edge. The enclosed cabin below and to the rear of the pilot held four to six passengers or could be fitted for cargo hauling. Cargo capacity was estimated to be approximately 427 kg (940 lb); fuel capacity was at 280 litres / 213 kg (78 US Gal / 468 lb) hp, see HP (disambiguation) The horsepower (hp) is the name of several non-metric units of power. ... A cockpit was a pit used for cockfighting, where owners would pit fighting birds against each other for the purpose of gambling. ...


They were sold new at the factory in 1927 for $14,200.


Operational service

Powered by the newly developed, air-cooled Pratt & Whitney radial engine which proved to be reliable, the Universal became widely-regarded as a good choice for small air carriers and operators. The rugged utility aircraft proved it could haul cargo or passengers and its unique shock absorber system comprised of bungee cords enabled it to land on bumpy and uneven landing strips. Configurations could be readily changed from landplane to seaplane equipped with floats or if fitted with skis, the Universal could be used on rough ice and snow surfaces. An order for 12 Universals was placed by Western Canada Airways when its owner, James Armstrong Richardson, Sr. judged that the Standard Universal was the best available transport for use in the northern regions of Canada [2]. Bungee cord is an elastic cord composed of one or more elastic strands forming a core, covered in a woven sheath usually of nylon or cotton. ... James Armstrong Richardson (Sr. ...


While not specifically designed for long-distance flights, the Universal was suitable for pioneering work. Charles Lindbergh had wanted to fly a Universal on his transatlantic flight but officials at the Atlantic Aircraft Corporation who reviewed his request in 1926, thought that Lindbergh's plans were too risky. More concerned about the company's reputation rather than the pilot's well-being, they would not sell him an aircraft. For Charles Augustus Lindbergh, Junior, see Lindbergh kidnapping. ...


The Universal provided steady if unspectacular service with more than half of the Universals utilized for bush flying while more than a dozen United States, Canadian and foreign airlines flew it as a passenger/cargo transport. A further development, the "Super Universal" was larger and more refined with a fully-enclosed cockpit. The follow-up design soon supplanted the Universal on the Atlantic Aircraft Corporation's production lines.


Universals continued to fly well into the 1930s but were primarily relegated to cargo work.


The Ghost of Charron Lake

Fokker Standard Universal G-CAJD is also known as "The Ghost of Charron Lake". It was lost in a snow storm on 10 December 1931. After a 30-year search for the rare bush plane, it was discovered in 2005. A Western Canada Aviation Museum search team (the Fokker Aircraft Recovery Team, F.A.R.T.), using sophisticated side scan sonar technology, finally located the aircraft literally "parked" on the lake bottom. In July 2006, the Ghost's engine was returned to Winnipeg, along with several artifacts. In October, the underwater archaeology team returned to the recovery site and towed the tail section to shallower waters. A further expedition will be undertaken in 2007 to recover more of the Fokker for future display at the museum. December 10 is the 344th day (345th in leap years) of the year in the Gregorian calendar, 21 days before the next year. ... 1931 (MCMXXXI) was a common year starting on Thursday (link is to a full 1931 calendar). ... The Western Canada Aviation Museum is a museum in Winnipeg, Manitoba, Canada. ...


Specifications (Fokker Universal)

General characteristics

  • Crew: One
  • Length: 33 ft 3 in (m)
  • Wingspan: 47 ft 9 in (m)
  • Height: 8 ft 9 in (m)
  • Wing area: 341 ft² ()
  • Empty weight: 2192 lb (996 kg)
  • Loaded weight: 4,000 lb (1818 kg)
  • Powerplant: 1× Wright J-6, Hamilton metal propeller, 330 hp (kW)

Performance

References

  1. ^ Fokker Universal NC3317
  2. ^ Molson 1974, p. 20.
  • Dierikx, Marc. Fokker: A Transatlantic Biography. Washington, DC: Smithsonian Institution Press, 1997. ISBN 1-56098-735-9.
  • Molson, K.M. Pioneering in Canadian Air Transport. Winnipeg: James Richardson & Sons, Ltd., 1974. ISBN 0-919212-39-5.
  • Nevin, David. The Pathfinders (The Epic of Flight Series). Alexandria, Virginia: Time-Life Books, 1980. ISBN 0-8094-3256-0.
  • Postma, Thijs. Fokker: Aircraft Builders to the World. London: Jane's, 1979. ISBN 0-531-03708-0.
  • Seagrave, Sterling. The Bush Pilots (The Epic of Flight Series). Alexandria, Virginia: Time-Life Books, 1983. ISBN 0-8094-3312-5.

The or meter (see spelling differences) is a measure of length. ... The distance AB is the wing span of this Aer Lingus Airbus A320. ... A square metre (US spelling: square meter) is by definition the area enclosed by a square with sides each 1 metre long. ... The U.S. National Prototype Kilogram, which currently serves as the primary standard for measuring mass in the U.S. It was assigned to the United States in 1889 and is periodically recertified and traceable to the primary international standard, The Kilogram, held at the Bureau International des Poids et... VNO of an aircraft is the V speed which refers to the velocity of normal operation. ... Kilometre per hour (American spelling: kilometer per hour) is a unit of both speed (scalar) and velocity (vector). ... Airspeed Indicator in a light aircraft The VC of an aircraft is the V speed which refers to the velocity of cruising. ... Kilometre per hour (American spelling: kilometer per hour) is a unit of both speed (scalar) and velocity (vector). ... Stall speed is an aerodynamic term. ... The maximal total range is the distance an aircraft can fly between takeoff and landing as limited by its fuel capacity. ... In aeronautics, the service ceiling is the maximum density altitude where the best rate of climb airspeed will produce a 100 feet per minute climb(twin engine) and 50 feet(single engine) at maximum weight while in a clean configuration with maximum continuous power. ... This page is a candidate to be moved to Wiktionary. ... In aerodynamics, the lift-to-drag ratio, or L/D ratio (ell-over-dee, as opposed to ell-dee), is the amount of lift generated by a wing, compared to the drag it creates by moving through the air. ...

External links

  • Fokker Universal
  • Fokker Universal NC3317
  • The Ghost of Charron Lake


 
 

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