DINFIA IA 46
IA 46 Ranquel / Super Ranquel and IA 51 Tehuelche | |
---|---|
Type: | Light aircraft |
Design country: | |
Manufacturer: | |
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
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
- IA 46 on airwar.ru accessed on March 15, 2016
- IA 46 at flap152.com. Retrieved March 15, 2016