Credit
Igor Dvurekov · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
An-12 · Length
Single source33.1 m (108 ft 7 in)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Antonov An-12 | Cirrus SR20 |
|---|---|---|
| Type | Cargo aircraft / military transport aircraft[source] | Light aircraft[source] |
| Manufacturer | Irkutsk Aviation Plant Tashkent Mechanical Plant[source] | Cirrus Aircraft[source] |
| Designer | Antonov[source] | — |
| Status | In service[source] | — |
| Primary users | Soviet Air Forces (historical) Russian Air Force Ukraine Air Alliance Cavok Air[source] |
26 ft 0 in (7.92 m)[source]
An-12 · with maximum fuel
Single source5,700 km (3,500 mi, 3,100 nmi) with maximum fuel[source]
An-12 · 4 × Ivchenko AI-20L or AI-20M turboprop engines (4,000 shp) each equivalent
Single source4 × Ivchenko AI-20L or AI-20M turboprop engines, 3,000 kW (4,000 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-12 · Wing area
Single source121.7 m 2 (1,310 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Number built | 1,248[source] | 2,084 (through 2025)[source] |
|---|
| Manufactured | 1957–1973[source] | 1999–present[source] |
|---|
| Introduction date | 1959[source] | — |
|---|
| First flight | 16 December 1957 ( 1957-12-16 )[source] | 21 March 1995[source] |
|---|
| Developed from | Antonov An-10[source] | — |
|---|
| Developed into | Shaanxi Y-8[source] | Cirrus SR22[source] |
|---|
| Capacity | 20,000 kg (44,000 lb) payload / 60 paratroopers / 2x BMD-1 armoured vehicles[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Guns | 2× 23 mm (0.906 in) Nudelman-Rikhter NR-23 cannons in a tail turret (some aircraft)[source] | — |
|---|
| Propellers | 4-bladed constant-speed reversible-pitch propellers[source] | 3-bladed[source] |
|---|
| Country of origin | Soviet Union[source] | — |
|---|
| Stall speed | — | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|
| National origin | — | United States[source] |
|---|