Credit
Tomás Del Coro from Las Vegas, Nevada, USA · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
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At a glance
Measured figures
SR20-G3 · Length
Single source26 ft 0 in (7.92 m)[source]
Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Grob G103a Twin II |
|---|---|---|
| Type | Light aircraft[source] | Two-Seater Class sailplane[source] |
| Manufacturer | Cirrus Aircraft[source] | Grob Aircraft[source] |
| Number built | 2,084 (through 2025)[source] | 549[source] |
| Manufactured | 1999–present[source] | — |
| First flight |
8.18 m (26 ft 10 in)[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]
SR20-G3 · Service ceiling
Single source17,500 ft (5,300 m)[source]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[source]
Wing area
Single source17.8 m 2 (191 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
21 March 1995[source] |
| — |
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | — |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | Germany[source] |
|---|
| Aspect ratio | — | 17.1[source] |
|---|
| g limits | — | +5.3/-2.65 at Va[source] |
|---|
| Maximum glide ratio | — | ca. 36.5[source] |
|---|
| Rate of sink | — | 0.64 m/s (126 ft/min)[source] |
|---|
| Wing loading | — | 32.6 kg/m 2 (6.68 lb/sq ft)[source] |
|---|
580 kg (1,280 lb)[source]