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]
Falcon 900B · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Dassault Falcon 900 |
|---|---|---|
| Type | Light aircraft[source] | Business jet[source] |
| Manufacturer | Cirrus Aircraft[source] | Dassault Aviation[source] |
| Number built | 2,084 (through 2025)[source] | >500[source] |
| Manufactured | 1999–present[source] | 1984–present[source] |
20.21 m (66 ft 4 in)[source]
SR20-G3 · Height
Single source8 ft 11 in (2.72 m)[source]
Falcon 900B · with 8 passengers
Single source7,400 km (4,600 mi, 4,000 nmi) with 8 passengers[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]
Falcon 900B · 3 × Honeywell TFE731 -5BR-1C turbofans thrust each
Single source3 × Honeywell TFE731 -5BR-1C turbofans , 21.13 kN (4,750 lbf) thrust each[source]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[source]
Falcon 900B · Wing area
Single source49.0 m 2 (527 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] | 21 September 1984 ( 1984-09-21 )[source] |
|---|
| Developed into | Cirrus SR22[source] | Dassault Falcon 2000 Dassault Falcon 7X[source] |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 19 passengers[source] |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] |
|---|
| National origin | United States[source] | France[source] |
|---|
| Status | — | Active service, in production[source] |
|---|
| Primary users | — | French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force[source] |
|---|
| Developed from | — | Dassault Falcon 50[source] |
|---|
| Fuel capacity | — | 8,690 kg (19,160 lb)[source] |
|---|
| Aspect ratio | — | 7.63:1[source] |
|---|