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Support aircraftIn production
Light Sport Aircraft
Evektor SportStar is a light Sport Aircraft originating in Czech Republic. It was built by Evektor-Aerotechnik.
Light Sport Aircraft
Czech Republic
Evektor-Aerotechnik
In production
1997–present
Evektor EPOS
one
one passenger
5.98 m (19 ft 7 in)
8.645 m (28 ft 4 in)
2.475 m (8 ft 1 in)
10.6 m 2 (114 sq ft)
NACA 2315 mod
309 kg (681 lb)
600 kg (1,323 lb)
118 L (31 US gal; 26 imp gal) usable / 85 kg (187 lb) max fuel weight
1 × Rotax 912ULS four-cylinder air and liquid-cooled, horizontally-opposed, piston engine, 73.4 kW (98.4 hp)
3-bladed VZLU V230C ground adjustable propeller
213 km/h (132 mph, 115 kn)
204 km/h (127 mph, 110 kn) at 75% power
83 km/h (52 mph, 45 kn) power off flaps up
270 km/h (170 mph, 150 kn)
1,300 km (810 mi, 700 nmi) with max fuel
8 hours 30 minutes
4,720 m (15,490 ft)
+6/-3
5.2 m/s (1,020 ft/min)
56.6 kg/m 2 (11.6 lb/sq ft)
0.128 kW/kg (0.078 hp/lb)
190 m (623 ft)
365 m (1,198 ft)
180 m (591 ft)
Reference text from Wikipedia contributors, used under CC BY-SA 4.0.
True scale
Sourced dimensions beside a 1.75 m human reference.
Points represent sourced observations, including revisions. Revisions on the same effective date are not separate inventory events. Ranges appear in the table and are not plotted as exact points.
| Observation / report period | Value | Source | Claim state |
|---|---|---|---|
| 29 Sept 2026 | 5.98 m | Wikipedia contributors | superseded |
| 29 Sept 2026 | 5.98 m | Wikipedia contributors | approved |
Evektor SportStar equipment records. Variants, orders and quantities are shown as reported in each inventory source; coverage is incomplete.
Number column of the Wikipedia list table under "Flight Training Center". The list's own wording applies; it is a compiled secondary source, not an official census.