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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 | Ilyushin Il-276 |
|---|---|---|
| Type | Light aircraft[source] | Military transport aircraft[source] |
| Manufacturer | Cirrus Aircraft[source] | United Aircraft Corporation[source] |
| Number built | 2,084 (through 2025)[source] | — |
| Manufactured | 1999–present[source] | — |
| First flight | 21 March 1995[source] |
37.7 m (123 ft 8 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]
2 × Aviadvigatel PD-14M turbofan engines thrust each
Single source2 × Aviadvigatel PD-14M turbofan engines, 152.98 kN (34,392 lbf) thrust each[source]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[source]
Payload
Single source20,000 kilograms (44,000 lb)[source]
Wing area
Single source160 m 2 (1,700 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Sometime in 2026[source] |
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 70 to 150 passengers[source] |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | — |
|---|
| Status | — | Under development[source] |
|---|
| Primary user | — | Russian Aerospace Forces[source] |
|---|
| Introduction date | — | Under development[source] |
|---|
| Fuel capacity | — | 30,700 kilograms (67,700 lb)[source] |
|---|
| Takeoff run | — | 1,050 metres (3,440 ft)[source] |
|---|
| Landing run | — | 1,050 metres (3,440 ft)[source] |
|---|
| Country of origin | — | Russia, India[source] |
|---|