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]
Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Fokker 50 |
|---|---|---|
| Type | Light aircraft[source] | Turboprop regional airliner[source] |
| Manufacturer | Cirrus Aircraft[source] | Fokker[source] |
| Number built | 2,084 (through 2025)[source] | 213[source] |
| Manufactured | 1999–present[source] | 1985–1997[source] |
25.25 m (82 ft 10 in)[source]
Range
Single source1,700 km (1,000 mi, 900 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 × Pratt & Whitney Canada PW125B turboprop engines each
Single source2 × Pratt & Whitney Canada PW125B turboprop engines, 1,864 kW (2,500 hp) each[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.
| First flight | 21 March 1995[source] | 28 December 1985[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 46 seats at 34" pitch to 56 seats at 30" pitch, 5,500 kg (12,100 lb) max payload[source] |
|---|
| Propellers | 3-bladed[source] | six-bladed Dowty Rotol composite propellers, 3.66 m (12 ft 0 in) diameter[source] |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | Netherlands[source] |
|---|
| Status | — | In service[source] |
|---|
| Primary users | — | PopulAir Skyward Express Air Panama Mahan Air[source] |
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| Introduction date | — | 1987[source] |
|---|
| Developed from | — | Fokker F27 Friendship[source] |
|---|
| Aspect ratio | — | 12.01[source] |
|---|
| Fuel capacity | — | 4,120 kg (9,080 lb)[source] |
|---|
| Fuselage width | — | 2.70 m (8.9 ft)[source] |
|---|
| Cabin Width | — | 2.50 m (98 in)[source] |
|---|
| Wing loading | — | 297.4 kg/m 2 (60.9 lb/sq ft)[source] |
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| Takeoff | — | 1,350 m (4,430 ft) - ISA, SL, MTOW[source] |
|---|
| Landing | — | 1,130 m (3,710 ft) - ISA, SL, MLW[source] |
|---|