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At a glance
Measured figures
Length
Single source33 ft 5 + 1 ⁄ 2 in (10.20 m)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Cessna 411 | Cirrus SR20 |
|---|---|---|
| Type | Light business/cargo aircraft[source] | Light aircraft[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Cessna[source] | Cirrus Aircraft[source] |
| Number built | 302[source] | 2,084 (through 2025) |
26 ft 0 in (7.92 m)[source]
Cruise; at 25,000 ft (7,600 m) (econ cruise)
Single sourceMaximum; at 16,000 ft (4,900 m)
Single source268 mph (431 km/h, 233 kn) at 16,000 ft (4,900 m)[source]
216 mph (348 km/h, 188 kn) at 25,000 ft (7,600 m) (econ cruise)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
at 216 mph (188 kn; 348 km/h) and
Single sourcenormal fuel
Single source1,300 mi (2,100 km, 1,100 nmi) at 216 mph (188 kn; 348 km/h) and 25,000 ft (7,600 m), normal fuel[source]
2 × Continental GTSIO-520 air-cooled geared, turbocharged flat-six engines each
Single source2 × Continental GTSIO-520 air-cooled geared, turbocharged flat-six engines, 340 hp (250 kW) each[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]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1962-1968[source] | 1999–present[source] |
|---|
| First flight | July 18, 1962[source] | 21 March 1995[source] |
|---|
| Developed from | Cessna 310[source] | — |
|---|
| Developed into | Cessna 401/402 Cessna 421[source] | Cirrus SR22[source] |
|---|
| Capacity | four to six passengers[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Fuel capacity | 170 US gal (140 imp gal; 640 L) standard, 196 US gal (163 imp gal; 740 L) with auxiliary tanks[source] | — |
|---|
| Propellers | 3-bladed constant-speed, 7 ft 4 in (2.24 m) diameter[source] | 3-bladed[source] |
|---|
| Stall speed | 84 mph (135 km/h, 73 kn) (flaps down)[source] | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|
| Takeoff distance to 50 ft (15m) | 1,890 ft (580 m)[source] | — |
|---|
| Landing distance from 50 ft (15 m) | 1,815 ft (553 m)[source] | — |
|---|