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]
50EX · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Dassault Falcon 50 |
|---|---|---|
| Type | Light aircraft[source] | Business jet[source] |
| Manufacturer | Cirrus Aircraft[source] | Dassault Aviation[source] |
| Number built | 2,084 (through 2025)[source] | 352[source] |
| Manufactured | 1999–present[source] | 1976–2008[source] |
18.52 m (60 ft 9 in)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
50EX · Range
Single source5,695 km (3,539 mi, 3,075 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]
50EX · 3 × Honeywell TFE 731-40 turbofan engines thrust each
Single source3 × Honeywell TFE 731-40 turbofan engines, 16.46 kN (3,700 lbf) thrust each[source]
50EX · Wing area
Single source46.83 m 2 (504.1 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] | 7 November 1976[source] |
|---|
| Developed into | Cirrus SR22[source] | Dassault Falcon 900[source] |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 8 to 9 passengers / 1,080 kg (2,381 lb) payload with full fuel[source] |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | France[source] |
|---|
| Status | — | In service[source] |
|---|
| Primary users | — | Armee de l'Air South African Air Force Portuguese Air Force Italian Air Force[source] |
|---|
| Developed from | — | Dassault Falcon 20[source] |
|---|
| Max Landing Weight | — | 16,200 kg (35,715 lb)[source] |
|---|
| Take-off run | — | 1,504 m (4,934 ft)[source] |
|---|
| Landing run | — | 685 m (2,247 ft)[source] |
|---|