Fanaero-Chile Chincol

Last updated
Chincol
Role Trainer aircraft
Manufacturer Fanaero-Chile
First flight 14 December 1955

The Fanaero-Chile Chincol (named for a South American sparrow) was a prototype trainer aircraft developed in Chile in 1955 for air force use. It was a conventional, low-wing cantilever monoplane of mixed construction, with fabric covered wooden wings and tail surfaces (making extensive use of Mañío, an indigenous wood). It was fitted with a fixed tailwheel undercarriage and was powered by a single 215 horsepower (160 kW) Continental O-470 air-cooled horizontally-opposed piston engine. The pilot and instructor sat in tandem, and were enclosed under a long canopy. The prototype Chincol made its maiden flight on 14 December 1955. The Chilean Air Force responded positively to the design, and placed an order for 50 machines. [1] However, technical problems significantly delayed manufacture, and the order was cancelled before the aircraft were produced.

Trainer aircraft Aircraft designed for training of pilots and aircrew

A trainer is a class of aircraft designed specifically to facilitate flight training of pilots and aircrews. The use of a dedicated trainer aircraft with additional safety features—such as tandem flight controls, forgiving flight characteristics and a simplified cockpit arrangement—allows pilots-in-training to safely advance their real-time piloting, navigation and warfighting skills without the danger of overextending their abilities alone in a fully featured aircraft.

Chile republic in South America

Chile, officially the Republic of Chile, is a South American country occupying a long, narrow strip of land between the Andes to the east and the Pacific Ocean to the west. It borders Peru to the north, Bolivia to the northeast, Argentina to the east, and the Drake Passage in the far south. Chilean territory includes the Pacific islands of Juan Fernández, Salas y Gómez, Desventuradas, and Easter Island in Oceania. Chile also claims about 1,250,000 square kilometres (480,000 sq mi) of Antarctica, although all claims are suspended under the Antarctic Treaty.

Cantilever beam anchored at only one end

A cantilever is a rigid structural element, such as a beam or a plate, anchored at one end to a support from which it protrudes; this connection could also be perpendicular to a flat, vertical surface such as a wall. Cantilevers can also be constructed with trusses or slabs. When subjected to a structural load, the cantilever carries the load to the support where it is forced against by a moment and shear stress.

Contents

Specifications

Data from Jane's All The World's Aircraft 1956–57 [1]

General characteristics

Airfoil

An airfoil or aerofoil is the cross-sectional shape of a wing, blade, or sail.

Continental O-470 flat six piston aircraft engine family

The Continental O-470 engine is a family of carbureted and fuel-injected six-cylinder, horizontally opposed, air-cooled aircraft engines that was developed especially for use in light aircraft by Continental Motors. Engines designated "IO" are fuel-injected.

Performance

  • Maximum speed: 210 km/h (130 mph; 113 kn) at sea level
  • Cruise speed: 185 km/h (115 mph; 100 kn)
  • Stall speed: 90 km/h (56 mph; 49 kn)
  • Range: 650 km (404 mi; 351 nmi) (cruising radius)
  • Service ceiling: 5,400 m (17,700 ft)
  • Rate of climb: 4.09 m/s (805 ft/min)
  • Take-off distance to 15 m (50 ft): 240 m (790 ft)
  • Landing distance from 15 m (50 ft): 650 m (2,130 ft)

Related Research Articles

The Aerauto PL.5C was a roadable aircraft developed in Italy in the early 1950s. It was a high-wing two-seat monoplane whose wings could be folded to quickly transform it into an automobile. It was different from many such projects in that it used its pusher propeller for propulsion not only in the air, but on the road as well. Development was abandoned in 1953.

The Aero Boero AB-210 is an Argentine civil utility aircraft, a development of the AB-180 with improved performance delivered by a fuel-injected engine. Unlike previous aircraft by this manufacturer, it also featured tricycle undercarriage, but retained the same general high-wing configuration. Only a single prototype was built, first flying on 22 April 1971.

SAI KZ III

The SAI KZ III Laerke was a Danish light utility aircraft used by the Danish Air Ambulance Service and Danish Air Force.

Ambrosini S.1001 light sport aircraft

The Ambrosini S.1001 Grifo ("Griffin") was an Italian light airplane that appeared shortly after the end of World War II. The first plane built by SAI Ambrosini postwar, the prototype flew in 1947 and was derived from the pre-war SAI.2S. It was a four-seat monoplane with spatted fixed undercarriage. A small series was produced for the Italian aeroclubs with an Alfa Romeo 110-ter engine of 97 kW (130 hp). Three examples were even bought by the Italian Aeronautica Militare (AMI), which used them between 1948 and 1950.

The Auster Avis was a four-seat light aircraft developed from the Auster Autocrat. It featured a redesigned fuselage incorporating four doors and a circular cross-section towards the tail, new undercarriage, and new wing flaps. It was planned in two versions, the Mk 1 for civil use, and the Mk 2 for military and air ambulance duties. However, only two prototypes were built, and Auster abandoned the project in favour of the Auster J-5 Autocar.

The Breda-Pittoni B.P.471 was an Italian twin-engine airliner/military transport produced by Breda.

The Piper PA-6 Sky Sedan was a 1940s American four-seat light aircraft designed and built in prototype form by Piper Aircraft at its Lock Haven, Pennsylvania, factory.

The Fletcher FL-23 was an American two-seat liaison or observation aircraft designed and built by the California-based Fletcher Aviation Corporation. It was entered into a competition and lost against the Cessna 305A as a liaison or observation aircraft for the United States Army.

DINFIA IA 53 agricultural aircraft by DINFIA

The DINFIA IA 53 Mamboretá was an agricultural aircraft developed in Argentina by DINFIA in the 1960s.

The PZL M-17 "Duduś Kudłacz" was a Polish twin-boom pusher general aviation and trainer aircraft of 1977, which remained a prototype.

LWD Żuraw aircraft

The LWD Żuraw was a Polish utility and liaison aircraft prototype of 1951, high-wing monoplane with single engine, that did not enter production. The name means crane.

The Mráz M-3 Bonzo was a light aircraft built in Czechoslovakia in 1948 as a further development in the family of light aircraft that had commenced with the M-1 Sokol. The Bonzo was based on the Sokol airframe, but with a redesigned wing and substantial changes to the fuselage. These included lengthening it to allow for the addition of a fourth seat, reducing the height of the rear fuselage to allow for a new cabin with all-around visibility, and the addition of a semi-retractable nosewheel in place of a tailwheel.

The Taylorcraft Model 20 Ranch Wagon was a four-seat cabin monoplane designed and built by Taylorcraft Aircraft as a development of the earlier experimental Model 18. The Model 20 was constructed of moulded fibreglass over a tubular framework. It had a conventional landing gear and a nose-mounted 225 hp (168 kW) Continental O-470-J engine.

Custer CCW-5

The Custer CCW-5 was a twin-engined, 5-seat aircraft of pusher configuration, which used a channel wing claimed to enable low speed flight and short take-offs. Two CCW-5s flew, eleven years apart, but the type never entered production.

Aero-Service Puma

The Aero-Service Puma is a Polish ultralight aircraft, designed and produced by Aero-Service Jacek Skopiński of Warsaw. The aircraft is supplied complete and ready-to-fly.

The Temco 58 was a low wing single engine, tandem seat propeller driven trainer, designed for sale to overseas air forces. It did not reach production.

Kawasaki KAT-1

The Kawasaki KAT-1 is a Japanese primary trainer, seating two in tandem, designed to compete for a Japanese Air Defense Force (JADF) contract in the mid-1950s. Only two were completed.

The SIPA S.70 was a late 1940s French eight-passenger light transport aircraft prototype built by Société Industrielle Pour l’Aéronautique (SIPA).

CSS-12 prototype Polish twin-engined feederliner of the 1950s

The CSS-12 was a prototype Polish twin-engined feederliner of the 1950s. A single example was built and flown in 1950, but no production followed.

The Maestranza Central de Aviación Triciclo-Experimental was a prototype Chilean light aircraft of the 1940s.

References

  1. 1 2 Bridgman 1956, p. 120.