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Aeroprints.com · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
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At a glance
Measured figures
Falcon 20F · Length
Single source17.15 m (56 ft 3 in)[source]
Falcon 2000LXS · Length
Single sourceConfiguration
| Specification | Dassault Falcon 20 | Dassault Falcon 2000 |
|---|---|---|
| Type | Business jet[source] | Business jet[source] |
| Manufacturer | Dassault Aviation[source] | Dassault Aviation Dassault Reliance Aerospace Limited (DRAL)[source] |
| Status | Out of production, in active service[source] | Active in production[source] |
| Primary users | Federal Express (formerly) French Navy United States Coast Guard[source] |
20.23 m (66 ft 4 in)[source]
Cruise; Falcon 20F · at 12,200 m (40,000 ft) (econ. cruise)
Single sourceMaximum; Falcon 20F · at 7,620 m (25,000 ft) (max cruise)
Single source862 km/h (536 mph, 465 kn) at 7,620 m (25,000 ft) (max cruise)[source]
750 km/h (470 mph, 400 kn) at 12,200 m (40,000 ft) (econ. cruise)[source]
Maximum; Falcon 2000LXS · Mach 0.85-0.862 (
Single sourceMach 0.85-0.862 (1050-1064 km/h)[source]
Falcon 20F · 2 × General Electric CF700 -2D-2 turbofans thrust each
Single source2 × General Electric CF700 -2D-2 turbofans , 20 kN (4,500 lbf) thrust each[source]
Falcon 2000LXS · 2 × Pratt & Whitney Canada PW308C turbofan engines thrust each
Single source2 × Pratt & Whitney Canada PW308C turbofan engines, 31.14 kN (7,000 lbf) thrust each[source]
Falcon 20F · Wing area
Single source41.00 m 2 (441.3 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built | 512[source] | 675 (Oct 2022)[source] |
|---|
| Manufactured | 1965–1991[source] | 1995–present[source] |
|---|
| Introduction date | 3 June 1965[source] | — |
|---|
| First flight | 4 May 1963[source] | 4 March 1993[source] |
|---|
| Developed into | Dassault Falcon 10 Dassault Falcon 50[source] | — |
|---|
| Capacity | 8–14 passengers[source] | 10 passengers[source] |
|---|
| Fuel capacity | 5,200 L (1,100 imp gal; 1,400 US gal)[source] | 16,660 lb (7,557 kg)[source] |
|---|
| Aspect ratio | 6.4:1[source] | — |
|---|
| Stall speed | 152 km/h (94 mph, 82 kn)[source] | — |
|---|
| National origin | France[source] | France[source] |
|---|
| Developed from | — | Dassault Falcon 900[source] |
|---|
| Take-off distance | — | 1,425 m (4,675 ft)[source] |
|---|
| Landing distance | — | 689 m (2,260 ft) ((FAR 91, 6 pax, SL, NBAA IFR reserves)[source] |
|---|