Credit
Tomás Del Coro from Las Vegas, Nevada, USA · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
SR20-G3 · Length
Single source26 ft 0 in (7.92 m)[source]
Skyvan 3 · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Short SC.7 Skyvan |
|---|---|---|
| Type | Light aircraft[source] | Utility aircraft[source] |
| Manufacturer | Cirrus Aircraft[source] | Short Brothers[source] |
| Number built | 2,084 (through 2025)[source] | 149[source] |
| Manufactured | 1999–present[source] | 1963-1986 |
12.21 m (40 ft 1 in)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
Skyvan 3 · Range
Single source1,115 km (693 mi, 602 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]
Skyvan 3 · 2 × Garrett AiResearch TPE-331 -2-201A turboprops (715 shp) each
Single source2 × Garrett AiResearch TPE-331 -2-201A turboprops , 533 kW (715 shp) each[source]
Skyvan 3 · Wing area
Single source35.12 m 2 (378.0 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| First flight | 21 March 1995[source] | 17 January 1963[source] |
|---|
| Developed into | Cirrus SR22[source] | Short 330 Short 360 C-23 Sherpa[source] |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 19 passengers[source] |
|---|
| Propellers | 3-bladed[source] | 3-bladed Hartzell HC-B3TN-5/T10282H variable-pitch propeller[source] |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | 111 km/h (69 mph, 60 kn) flaps down, EAS[source] |
|---|
| National origin | United States[source] | United Kingdom[source] |
|---|
| Status | — | In limited service[source] |
|---|
| Fuel capacity | — | 1,109 L (244 imp gal; 293 US gal)[source] |
|---|
| Never exceed speed | — | 402 km/h (250 mph, 217 kn) EAS[source] |
|---|
| Takeoff run to 15 m (50 ft) | — | 482 m (1,581 ft) (STOL)[source] |
|---|
| Landing run from 15 m (50 ft) | — | 567 m (1,860 ft) (STOL)[source] |
|---|