The IAR 813 is a two-seater light sports and training aircraft developed from the earlier IAR 811. The IAR 813 is a low-wing cantilever monoplane of wooden and composite construction powered by a Walter Minor 6-III six-cylinder in-line inverted air-cooled engine providing a top speed of 185km/h and a range of 500km.
|A three-view drawing (686 x 1022)|
| ENGINE||1 x Walter Minor 4-III, 77kW|
| Take-off weight||760 kg||1676 lb|
| Empty weight||520 kg||1146 lb|
| Wingspan||10.1 m||33 ft 2 in|
| Length||8.4 m||28 ft 7 in|
| Height||2.3 m||8 ft 7 in|
| Max. speed||190 km/h||118 mph|
| Cruise speed||175 km/h||109 mph|
| Ceiling||5500 m||18050 ft|
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