Bellanca Aircraft - AviaBellanca Aircraft Corporation is an American aircraft design and manufacturer. Before 1983, it was called Bellanca Aircraft Corporation. The company was founded in 1927 by Giuseppe Mario Bellanca.
After Giuseppe Mario Bellanca, the first Italian aircraft designer and builder, came to the United States in 1911, he began designing aircraft for several companies, including the Maryland Press Steel Company, the Wright Aviation Company, and the Columbia Airplane Company. Bellanca founded his own company, Bellanca Aircraft Corporation of America, in 1927, locating first in Richmond Hill, New York, and moving in 1928 to New Castle (Wilmington), Delaware. In the 1920s and 1930s, Bellanca's self-designed aircraft were renowned for their efficiency and low operating costs, and achieved a reputation for breaking flight and distance records. The Bellanca WB-2 was Lindbergh's first choice for his flight from New York to Paris. Ryan was the result of the company's demand to select the "Lindberg" team.
Bellanca Aircraft
Bellanca remained president and chairman of the board from the company's founding on the last day of 1927 until he sold the company to L. Albert & Sons in 1954.
Bellanca 14 7
Since then, the Bellanca line has been part of a succession of companies that carry the lineage of the original Bellanca produced aircraft. The Bellanca 14-7 Junior and its successors were a family of light aircraft manufactured by the Bellanca Aircraft Company in the United States shortly before World War II.
Bellanca was already established in the 6-8 seater aircraft market, but he believed that he could also successfully sell smaller aircraft (3-4 seats). The first example flew in 1937.
The 14-7 was a low wing cantilever monoplane and the fuselage was intended to complement the lift design. Although the prototype flew with a fixed steering undercarriage, Version 14-9 was the first mass-produced American light aircraft with a retractable undercarriage; The main wheels rotated backwards, until they reached the wells in the wings.
In February 1938, the prototype 14-7 crashed during high-speed dive tests, killing Bellanca test pilot Cecil Hoffman (32), possibly due to wing flutter. This resulted in the redesign of the wing from being predominantly fabric covered to Bellanca's signature plywood covered wing. The second prototype, a 14-9 test pilot flown by Bellanca Holger Hoiriis, did not fare well from the spins. The iconic D stabilization plates solved the spin recovery problem. Bert "Fish" Hassel took the prototype 14-9 to the 1938 Chicago Air Show and because of the difficulty people were having getting into the plane, the upper fuselage cabin door trim was modified.
Aircraft Photo Of N9848b
Junior was 14-7 first. In 1939, when production began, the 14-9 Cruiser was renamed.
In 1940, Bellanca Aircraft gave two aircraft No. 14 to No. 9 on loan to the National Advisory Committee for Aeronautics (NACA), apparently to handle evaluations. One was at NACA in late June and the other in early July, and they stayed for 2-3 weeks.
Development ended in 1941 14-12-F3 [8], when production was halted to allow Bellanca to serve as a subcontractor for the duration of the war when an attempt to market a military version as a trainer failed. After the war, Bellanca returned to design to create the Bellanca 14-13 and its successors.
The main production version had a retractable undercarriage and 90 bhp (67 kW) LeBlond 5F or K-Royce 5G radial piston bearings.
Reflections Of Speed, 1960 Bellanca Aircraft Stock Photo
The photo shows a Smithsonian 14-10 equipped with a Lycoming O-350 6-cylinder horizontal piston engine rated at 150 horsepower (112 kW).
Military training version. Bellanca's documentation indicates that the T14-14 was to be fitted with a Franklin 6A4-150-B3 150 (112 kW) horizontal piston engine.
Indeed the surviving T14-14 is powered by a Franklin 6AC-298-F3 horizontal piston engine rated at 130 hp (97 kW) (prototype only). A retractable four-seat landing gear, manufactured in the United States in the 1960s and 1970s, the aircraft has undergone several modifications of classic designs by aviation pioneer Giuseppe Bellanca. A total of 1,356 Vikings were produced, with production peaking between 1968 and 1975 (1,019 aircraft).
Training with retractable tail wheel and triple tail. The larger and more powerful Cruisemaster series 14-13 Cruisers were introduced in the early 1950s. After the original Bellanca appeared, Downer Aircraft obtained type certification and built a Cruise Master 14-19-2 to marry the fuselage of the Continental O-470 230 hp. In 1958, Downer redesigned the aircraft with a nose wheel and a 260 hp IO-470 fuel injected engine, making it the "260".
Bellanca 28 92 Trimotor
The 14-19-2 260 retained the triple cable stayed tail of the 1962 model. After this year, the triple-tail design was changed to a single tail with the same additional surface area, and was built as the Model 260A. Later, the Vikings kept the enlarged vertical fin, which enhances the flight characteristics of the aircraft. The Model Viking was born from Downer's discussion of a larger version of the "Model 260" with at least 300 hp. The company was located in Minota and employed skilled craftsmen who made the Spruce wing, and the new 300-horsepower model was named "Viking" because of the many Vikings in the area.
It was equipped with the 300 hp Continental IO-520-K. In 1969, Viking was introduced with the 290 hp (later 300 hp) Lycoming IO-540, in regular (17-31) or turbocharged (17-31TC) versions.
Over the years, several improvements have been made to the aircraft. The original hydraulic landing gear and flap operating system were redesigned in 1968, when electric flaps were introduced. In 1969, the FAA issued the A18CE type certificate and the aircraft built to the design were named the "A" series "Super Viking". Along with improvements already made to the late model Viking 300, the power for the new Viking 300A (17-30A, 17-31A and 17-31 ATC) was increased to 1508.2kg. The original complex fuel system, with five tanks and two fuel selectors allowing eight possible selection combinations, was simplified to a left, right and auxiliary system in 1974. After several years of financial losses, Viking sales increased again. became profitable again in 1978.
The 1979 Continental powered Viking had a closed nose wheel due to a redesigned engine mount. This required the use of cooling flaps for the first time on board the Viking, but resulted in a speed increase of 19.3 km/h. In 1979, the production of the 17-31A equipped with the engine Lycoming co. In 1996, the Continental IO-550 engine became available as an option.
Three Days In A (really) Stinking Airplane
Since 2002, the company has been run by a group of six Bellanca enthusiasts who bought it from Minnota and created the Alexandria Aircraft Co. LLC. They provide technical and reputation support to owners and airframe and engine maintenance services on the ground. They sold a new aircraft built in 2005.
The fuselage is made of steel tubes covered with fabric, and the wings are made of spruce with a plywood cover.
Bill Cox, a well-known aviation journalist for Plane and Pilot magazine, said of the flying characteristics of Vikings, "They have long been known for a control and harmony that makes them almost psychic in nature." ",
He said, "Owners almost unanimously declare that the Viking is the best handling aircraft they have ever used."
Bellanca Cruisemaster & Cruisair: Covers, Plugs, Etc
Four-seat light aircraft, powered by a Continental IO-520-K piston engine rated at 300 hp (224 kW).
Four-seat light aircraft, powered by a Lycoming IO-540 piston engine rated at 300 hp.
Four-seat light aircraft, powered by a Lycoming IO-540 piston engine rated at 300 hp (224 kW), equipped with a turbocharger.
Four-seat light aircraft, powered by a Lycoming IO-540-K1 piston engine rated at 300 hp (224 kW).
Bellanca 7eca Citabria Light Aircraft Leaving Dalcross Airport, Inverness. Scottish Highlands. Xav 4875 457 Stock Photo
Four-seat light aircraft, powered by a Lycoming IO-540-K1 piston engine rated at 300 hp (224 kW), equipped with two Rajay turbochargers.
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