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At a glance
Measured figures
Length
Single source28.07 m (92 ft 1 in)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Antonov An-74 | Cirrus SR20 |
|---|---|---|
| Type | Transport aircraft[source] | Light aircraft[source] |
| National origin | Soviet Union / Ukraine[source] | United States[source] |
| Manufacturer | Antonov[source] | Cirrus Aircraft[source] |
| Status | In service[source] | — |
| Primary users |
26 ft 0 in (7.92 m)[source]
Cruise; 297 or
Single sourceCruise; 550 or 342 or
Single sourceCruise; Cruise speed
Single sourceMaximum; Maximum speed
Single source700 km/h (435 mph, 378 kn)[source]
550 or 600 km/h (342 or 373 mph, 297 or 324 kn)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
Range
Single source4,325 km (2,688 mi, 2,336 nmi)[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]
2 × Lotarev D-36 series 1A thrust each
Single source2 × Lotarev D-36 series 1A , 63.9 kN (14,330 lbf) thrust each[source]
Wing area
Single source98.62 m 2 (1,062 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.
Islamic Revolutionary Guard Corps Aerospace Force Utair Egyptian Air Force Pouya Air[source]
| — |
| Number built | 62[source] | 2,084 (through 2025)[source] |
|---|
| Manufactured | 1986–2004[source] | 1999–present[source] |
|---|
| Introduction date | 1983[source] | — |
|---|
| First flight | September 29, 1983[source] | 21 March 1995[source] |
|---|
| Developed from | Antonov An-72[source] | — |
|---|
| Capacity | up to 52 passengers[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Developed into | — | Cirrus SR22[source] |
|---|
| Propellers | — | 3-bladed[source] |
|---|
| Stall speed | — | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|