Credit
Artem Katranzhi · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
An-2 · Length
Single source12.4 m (40 ft 8 in)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Antonov An-2 | Cirrus SR20 |
|---|---|---|
| Type | Agricultural , utility aircraft and military transport aircraft[source] | Light aircraft[source] |
| Manufacturer | Antonov[source] | Cirrus Aircraft[source] |
| Designer | Oleg Antonov[source] | — |
| Status | In service[source] | — |
| Primary users | Soviet Air Forces (historical) Russian Aerospace Forces Korean People's Army Air Force Ukrainian Air Force[source] |
26 ft 0 in (7.92 m)[source]
SR20-G3 · Wingspan
Single source38 ft 4 in (11.68 m)[source]
An-2 · Range
Single source845 km (525 mi, 456 nmi)[source]
An-2 · 1 × Shvetsov ASh-62IR 9-cylinder air-cooled supercharged radial piston engine
Single source1 × Shvetsov ASh-62IR 9-cylinder air-cooled supercharged radial piston engine, 750 kW (1,010 hp)[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-2 · Wing area
Single source71.52 m 2 (769.8 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Number built | 18,000+[source] | 2,084 (through 2025)[source] |
|---|
| Manufactured | 1947–2001[source] | 1999–present[source] |
|---|
| First flight | 31 August 1947[source] | 21 March 1995[source] |
|---|
| Developed into | Antonov An-3 SibNIA TVS-2DTS[source] | Cirrus SR22[source] |
|---|
| Capacity | 12 passengers / 2,140 kg (4,718 lb)[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Fuel capacity | 1,200 L (320 US gal; 260 imp gal)[source] | — |
|---|
| Upper wingspan | 18.2 m (59 ft 9 in)[source] | — |
|---|
| Lower wingspan | 14.2 m (46 ft 7 in)[source] | — |
|---|
| Airfoil | TsAGI R-11 (14%)[source] | — |
|---|
| Propellers | 4-bladed constant-speed propeller[source] | 3-bladed[source] |
|---|
| Stall speed | 50 km/h (31 mph, 27 kn) circa[source] | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|
| Power/mass | 0.136 kW/kg (0.083 hp/lb)[source] | — |
|---|
| Fuel consumption | 185–200 L/h (49–53 gal/h; 41–44 imp gal/h)[source] | — |
|---|
| National origin | Soviet Union[source] | United States[source] |
|---|