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 | Dassault Falcon 7X |
|---|---|---|
| Thrust | — | 28.48 kN (6,402 lbf)[source] |
| Type | Light aircraft[source] | Intercontinental business jet[source] |
| Manufacturer | Cirrus Aircraft[source] | Dassault Aviation[source] |
| Number built | 2,084 (through 2025)[source] | 289 (7X, Q1 2020), ~50 (8X, 2018)[source] |
23.38 m (76.08 ft)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
Cruise; Cruise speed · source measurement 2
Single sourceCruise; Cruise speed · source measurement 3
Single sourceCruise; Mach 0.8 (
Single sourceMach 0.8 (459 kn; 850 km/h; 528 mph)[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]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[source]
Wing area
Single source70.7 m 2 (761 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1999–present[source] | 2005–2023[source] |
|---|
| First flight | 21 March 1995[source] | 7X: 5 May 2005 8X: 6 February 2015[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 12 to 16 passengers[source] |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | France[source] |
|---|
| Primary users | — | Air Alsie Flying Group Volkswagen AirService GmbH Shell Oil[source] |
|---|
| Introduction date | — | 7X: 15 June 2007 8X: 5 October 2016[source] |
|---|
| Developed from | — | Dassault Falcon 900[source] |
|---|
| Fuel capacity | — | 14,488 kg (31,940 lb)[source] |
|---|