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At a glance
Measured figures
Length
Single source32.23 m (105 ft 9 in)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Antonov An-178 | Cirrus SR20 |
|---|---|---|
| Type | Military transport aircraft[source] | Light aircraft[source] |
| National origin | Ukraine[source] | United States[source] |
| Designer | Antonov[source] | — |
| Built by | Antonov Serial Production Plant[source] | — |
| Status | In development[source] |
26 ft 0 in (7.92 m)[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]
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 | 1 as of 2020[source] | 2,084 (through 2025)[source] |
|---|
| First flight | 7 May 2015[source] | 21 March 1995[source] |
|---|
| Developed from | Antonov An-158[source] | — |
|---|
| Capacity | 90 soldiers, 70 paratroopers, 48 on stretchers +15 seated, 8 medical modules and 12, or 16 tons of cargo, overload variant 18 tons.[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Fuel capacity | 14,650 kg (32,298 lb)[source] | — |
|---|
| Powerplant | 2 × Progress D-436 -148FM turbofans[source] | — |
|---|
| Max landing weight | 47,000 kg (103,617 lb)[source] | — |
|---|
| Thrust each | 73.55 kN (16,534 lbf)[source] | — |
|---|
| Required field length (ISA, SL) | 2,500 m (8,200 ft)[source] | — |
|---|
| Manufacturer | Antonov[source] | Cirrus Aircraft[source] |
|---|
| Manufactured | — | 1999–present[source] |
|---|
| Developed into | — | Cirrus SR22[source] |
|---|
| Propellers | — | 3-bladed[source] |
|---|
| Stall speed | — | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|