Credit
Gartenfreuden (Wolfgang) · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
An-30 · Length
Single source24.26 m (79 ft 7 in)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Antonov An-30 | Cirrus SR20 |
|---|---|---|
| Type | Aerial cartography , reconnaissance and transport[source] | Light aircraft[source] |
| Manufacturer | Antonov[source] | Cirrus Aircraft[source] |
| Designer | Beriev[source] | — |
| Status | In limited service[source] | — |
| Primary users | Russian Air Force Ukrainian Air Force People's Liberation Army Air Force Romanian Air Force[source] |
26 ft 0 in (7.92 m)[source]
An-30 · with no reserves
Single source2,630 km (1,630 mi, 1,420 nmi) (with no reserves)[source]
An-30 · 2 × Ivchenko AI-24T VT turboprop engines (2,803 shp) each equivalent
Single source2 × Ivchenko AI-24T VT turboprop engines, 2,090 kW (2,803 shp) each equivalent[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]
An-30 · Wing area
Single source74.98 m 2 (807.1 sq ft)[source]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Number built | 123[source] | 2,084 (through 2025)[source] |
|---|
| Manufactured | 1971 – 1980[source] | 1999–present[source] |
|---|
| Introduction date | July 1968[source] | — |
|---|
| First flight | 21 August 1967[source] | 21 March 1995[source] |
|---|
| Developed from | Antonov An-24[source] | — |
|---|
| Fuel capacity | 6,200 L (1,600 US gal; 1,400 imp gal)[source] | — |
|---|
| Aspect ratio | 11.4:1[source] | — |
|---|
| Airfoil | root: TsAGI S-5-18; tip: TsAGI S-3-13[source] | — |
|---|
| Propellers | 4-bladed constant-speed propellers[source] | 3-bladed[source] |
|---|
| Take-off run | 710 m (2,329 ft)[source] | — |
|---|
| Landing run | 670 m (2,198 ft)[source] | — |
|---|
| Country of origin | Soviet Union[source] Soviet Union[source] | — |
|---|
| Developed into | — | Cirrus SR22[source] |
|---|
| Capacity | — | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Stall speed | — | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|
| National origin | — | United States[source] |
|---|