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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 |
| WEIGHTS |
| Take-off weight | 760 kg | 1676 lb |
| Empty weight | 520 kg | 1146 lb |
| DIMENSIONS |
| Wingspan | 10.1 m | 33 ft 2 in |
| Length | 8.4 m | 27 ft 7 in |
| Height | 2.3 m | 7 ft 7 in |
| PERFORMANCE |
| Max. speed | 190 km/h | 118 mph |
| Cruise speed | 175 km/h | 109 mph |
| Ceiling | 5500 m | 18050 ft |
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