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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]
Tarragon · Length
Single sourceConfiguration
| Specification | Dassault Falcon 20 | Pelegrin Tarragon |
|---|---|---|
| Type | Business jet[source] | Ultralight aircraft[source] |
| Manufacturer | Dassault Aviation[source] | Pelegrin Limited[source] |
| Status | Out of production, in active service[source] | In production (2018)[source] |
| Primary users | Federal Express (formerly) French Navy United States Coast Guard[source] | — |
7.53 m (24 ft 8 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]
Cruise; Tarragon · Cruise speed
Single sourceMaximum; Tarragon · Maximum speed
Single sourceTarragon · 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine
Single source1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine , 75 kW (101 hp)[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.
| Number built | 512[source] | — |
|---|
| Manufactured | 1965–1991[source] | — |
|---|
| Introduction date | 3 June 1965[source] | — |
|---|
| First flight | 4 May 1963[source] | — |
|---|
| Developed into | Dassault Falcon 10 Dassault Falcon 50[source] | — |
|---|
| Capacity | 8–14 passengers[source] | one passenger[source] |
|---|
| Fuel capacity | 5,200 L (1,100 imp gal; 1,400 US gal)[source] | 96 litres (21 imp gal; 25 US gal)[source] |
|---|
| Aspect ratio | 6.4:1[source] | — |
|---|
| Stall speed | 152 km/h (94 mph, 82 kn)[source] | 65 km/h (40 mph, 35 kn)[source] |
|---|
| National origin | France[source] | Latvia[source] |
|---|
| Developed from | — | Millennium Master[source] |
|---|
| Propellers | — | 3-bladed constant speed propeller[source] |
|---|
| Never exceed speed | — | 370 km/h (230 mph, 200 kn)[source] |
|---|