Credit
Tomás Del Coro from Las Vegas, Nevada, USA · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
SR20-G3 · Length
Single source26 ft 0 in (7.92 m)[source]
SportStar Max · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Evektor SportStar |
|---|---|---|
| Type | Light aircraft[source] | Light Sport Aircraft[source] |
| Manufacturer | Cirrus Aircraft[source] | Evektor-Aerotechnik[source] |
| Number built | 2,084 (through 2025)[source] | — |
| Manufactured | 1999–present[source] | 1997–present[source] |
5.98 m (19 ft 7 in)[source]
SportStar Max · with max fuel
Single source1,300 km (810 mi, 700 nmi) with max fuel[source]
SR20-G3 · 1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine
Single source1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine , 200 hp (150 kW)[source]
SportStar Max · 1 × Rotax 912ULS four-cylinder air and liquid-cooled, horizontally-opposed, piston engine
Single source1 × Rotax 912ULS four-cylinder air and liquid-cooled, horizontally-opposed, piston engine, 73.4 kW (98.4 hp)[source]
SportStar Max · Wing area
Single source10.6 m 2 (114 sq ft)[source]
SportStar Max · Endurance
Single source8 hours 30 minutes[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| First flight |
|---|
21 March 1995[source] |
| — |
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | one passenger[source] |
|---|
| Propellers | 3-bladed[source] | 3-bladed VZLU V230C ground adjustable propeller[source] |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | 83 km/h (52 mph, 45 kn) power off flaps up[source] |
|---|
| National origin | United States[source] | Czech Republic[source] |
|---|
| Status | — | In production[source] |
|---|
| Variant | — | Evektor EPOS[source] |
|---|
| Airfoil | — | NACA 2315 mod[source] |
|---|
| Fuel capacity | — | 118 L (31 US gal; 26 imp gal) usable / 85 kg (187 lb) max fuel weight[source] |
|---|
| Never exceed speed | — | 270 km/h (170 mph, 150 kn)[source] |
|---|
| g limits | — | +6/-3[source] |
|---|
| Wing loading | — | 56.6 kg/m 2 (11.6 lb/sq ft)[source] |
|---|
| Power/mass | — | 0.128 kW/kg (0.078 hp/lb)[source] |
|---|
| Take-off run | — | 190 m (623 ft)[source] |
|---|
| Take-off distance to 15 m (49 ft) | — | 365 m (1,198 ft)[source] |
|---|
| Landing run | — | 180 m (591 ft)[source] |
|---|