IAe.22 DL

The I.Ae. 22 "DL" was an Argentine advanced training aircraft designed by the Instituto Aerotecnico (AeroTechnical Institute) in 1943. It had a wooden structure, and a 9-cylinder 450 HP radial engine (Ae 16 "El Gaucho") with a Hamilton Standard 2M-D-30 metallic propeller. The prototype flew the 8 August 1944, although some sources give a different date.fact|date=December 2007 Approximately 200 aircraft were built. A version with an Armstrong Siddeley "Cheetah" 25 engine (radial 7 cylinder, 475 HP) and a Rotol constant speed propeller was designated I.Ae. 22- C.

Operators

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pecifications

General characteristics
*Wingspan 12,60 m;
*length 9,20 m;
*height 2,82 m;
*wing surface 23,19 m2;
*empty weight 1.520 kg;
*total weight 2.220 kg;
*wing load 96 kg/m2;
*weight-power ratio 5,28 kg/HP.Performance
*Maximum speed 290 km/h at 450 m;
*cruise speed 260 km/h;
*landing speed 110 km/h;
*service ceiling 5.200 m;
*absolute ceiling 6000 m;
*range 1.100 km / 4 hours 15 min.

Armament
*2 x 7,65 mm fixed machine guns (450 rounds each)
*3 x 50 kg bombs, or 9 x 15 kg, or 6 x 11 kg rockets.

ee also

*North American T-6 Texan trainer, a comparable aircraft

References

*Article on the 50th anniversary of the "Fabrica Militar de Aviones" listing all the aircraft developed and manufactured there since 1927, Aerospacio, Buenos Aires, 1977. (in Spanish)

*cite web |url=http://www.aeroespacio.com.ar/site/anteriores/538-550/549/SITE/sumario549.htm |title=Los 75 años de la Fábrica Militar de Aviones |author=Antonio C. Burgos |accessdate=2007-12-05 (in Spanish)

External links

* [http://www.geocities.com/bacosistemas01/IAe22.html Development and Specifications] (in Spanish)