FORCETALLY
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Measured figures
Falcon 20F · Length
Single source17.15 m (56 ft 3 in)[source]
Configuration
| Specification | Bombardier CRJ100/200 | Dassault Falcon 20 |
|---|---|---|
| Type | Regional jet[source] | Business jet[source] |
| National origin | Canada[source] | France[source] |
| Manufacturer | Bombardier Aerospace[source] | Dassault Aviation[source] |
| Status | In service[source] | Out of production, in active service |
Falcon 20F · Wingspan
Single source16.30 m (53 ft 6 in)[source]
Falcon 20F · Height
Single source5.32 m (17 ft 5 in)[source]
Falcon 20F · Crew
Single sourceCruise; 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]
Falcon 20F · Range
Single source3,350 km (2,080 mi, 1,810 nmi)[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 20F · Wing area
Single source41.00 m 2 (441.3 sq ft)[source]
Falcon 20F · absolute ceiling
Single source12,800 m (42,000 ft) (absolute ceiling)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | SkyWest Airlines Air Wisconsin Jazz Aviation[source] | Federal Express (formerly) French Navy United States Coast Guard[source] |
|---|
| Number built | 1,021[source] | 512[source] |
|---|
| Manufactured | 1991–2006[source] | 1965–1991[source] |
|---|
| Introduction date | 19 October 1992 with Lufthansa CityLine[source] | 3 June 1965[source] |
|---|
| First flight | 10 May 1991[source] | 4 May 1963[source] |
|---|
| Developed from | Bombardier Challenger 600 series[source] | — |
|---|
| Variant | Bombardier Challenger 850[source] | — |
|---|
| Developed into | Bombardier CRJ700 series[source] | Dassault Falcon 10 Dassault Falcon 50[source] |
|---|
| Capacity | — | 8–14 passengers[source] |
|---|
| Fuel capacity | — | 5,200 L (1,100 imp gal; 1,400 US gal)[source] |
|---|
| Aspect ratio | — | 6.4:1[source] |
|---|
| Stall speed | — | 152 km/h (94 mph, 82 kn)[source] |
|---|