Credit
Ken Fielding · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Length
Single source26 m (85 ft 4 in)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Antonov An-8 | Cirrus SR20 |
|---|---|---|
| Type | Military transport aircraft[source] | Light aircraft[source] |
| Manufacturer | Antonov[source] | Cirrus Aircraft[source] |
| Status | One in service with Uhuru Airlines[source] | — |
| Primary users | Soviet Air Force Aeroflot[source] | — |
| Number built | ~151[source] |
26 ft 0 in (7.92 m)[source]
Range
Single source2,780 km (1,730 mi, 1,500 nmi)[source]
2 × Ivchenko AI-20D turboprop engines (5,180 shp) each
Single source2 × Ivchenko AI-20D turboprop engines, 3,860 kW (5,180 shp) 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]
Wing area
Single source117.2 m 2 (1,262 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
2,084 (through 2025)[source] |
| Manufactured | 1956-1961[source] | 1999–present[source] |
|---|
| Introduction date | 1958[source] | — |
|---|
| First flight | 11 February 1956[source] | 21 March 1995[source] |
|---|
| Developed into | Antonov An-10[source] | Cirrus SR22[source] |
|---|
| Capacity | 48 persons / 11,000 kg (24,000 lb) max payload[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Guns | One 23 mm cannon in the tail turret.[source] | — |
|---|
| Aspect ratio | 11.7[source] | — |
|---|
| Propellers | 4-bladed constant-speed propellers[source] | 3-bladed[source] |
|---|
| National origin | Soviet Union[source] | United States[source] |
|---|
| Country of origin | Soviet Union[source] Soviet Union[source] | — |
|---|
| Stall speed | — | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|