DINFIA IA 46

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IA 46 Ranquel / Super Ranquel and IA 51 Tehuelche
An IA 46 Super Ranquel in 1975 in Buenos Aires
Type: Light aircraft
Design country:

ArgentinaArgentina Argentina

Manufacturer:

DINFIA

First flight:

December 23, 1957

Commissioning:

1958

Number of pieces:

132 IA-46, 1 IA-51

The DINFIA IA 46 Ranquel, IA 46 Super Ranquel and IA 51 Tehuelche were single-engine multi-purpose aircraft from the Argentine manufacturer DINFIA .

History and construction

The IA 46 was developed for the Argentine flying clubs and for use as an agricultural aircraft in agriculture. It was designed as a strutted shoulder wing with a non-retractable tail wheel landing gear . The fuselage consisted of a welded tubular steel construction and, like the wings, was covered with fabric. There was room for a pilot and two passengers on a bench behind him. The wings of the further development IA 51 Tehuelche were clad with metal, had larger landing flaps and an increased fuel capacity from 140 to 172 liters. When used as an agricultural aircraft, instead of 400 liters of fertilizer or chemicals, 500 liters could now be carried.

Many machines are still used today by the Argentine aviation clubs. Some machines were purchased from Fuerza Aérea Argentina for the towing of gliders.

Versions

  • IA 46 Ranquel - first production version with Lycoming O-320 -A2B engine, a prototype and 115 production aircraft built
    • IA 46 Super Ranquel - version with Lycoming O-360 -A1A engine, 16 built.
  • IA 51 Tehuelche - Version with metal-clad wings, larger landing flaps and increased spray capacity of 500 liters. Only one copy was built. First flight on March 16, 1963.

Military use

ArgentinaArgentina Argentina

Technical specifications

Parameter Data from IA 46
values ​​for use as an agricultural aircraft in brackets
crew 1
Passengers 2 or spray equipment
length 7.45 m
span 11.60 m
height 2.15 m
Wing area 18 m²
payload 400 liters of chemicals instead of the passengers as a spray plane
Empty mass 630 kg (690 kg)
Max. Takeoff mass 1000 kg (1160 kg)
Cruising speed 162 km / h
Top speed 180 km / h
Service ceiling 4000 m
Range 650 km
Engine 1 × Lycoming O-320 -A2B boxer engine with 112 kW

See also

literature

  • Taylor, John WR (1965). Jane's All The World's Aircraft 1965-66. London: Sampson Low, Marston & Company.
  • Taylor, Michael JH (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. P. 326.
  • Simpson, RW (1995). Airlife's General Aviation. Shrewsbury: Airlife Publishing. P. 413.

Web links

Commons : DINFIA IA 46  - collection of images, videos and audio files

Individual evidence

  1. Jane's 1965, p. 5
  2. Data from Jane's All The World's Aircraft 1965–66, p. 4