Credit
Aeroprints.com · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
Falcon 20F · Length
Single source17.15 m (56 ft 3 in)[source]
Length
Single sourceConfiguration
| Specification | Dassault Falcon 20 | Indonesian Aerospace N219 |
|---|---|---|
| Type | Business jet[source] | Utility aircraft[source] |
| Manufacturer | Dassault Aviation[source] | Indonesian Aerospace[source] |
| Status | Out of production, in active service[source] | In production[source] |
| Primary users | Federal Express (formerly) French Navy United States Coast Guard[source] |
16.49 m (54 ft 1 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; Economical
Single sourceMaximum; Maximum speed
Single source2 × Pratt & Whitney Canada PT6A-42 turboprop engines (850 shp) each
Single source2 × Pratt & Whitney Canada PT6A-42 turboprop engines, 630 kW (850 shp) each[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]
1,938 ft/min
Single source9.85 m/s (1,938 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built | 512[source] | 2 prototypes (December 2024)[source] |
|---|
| Manufactured | 1965–1991[source] | 2017–present[source] |
|---|
| Introduction date | 3 June 1965[source] | — |
|---|
| First flight | 4 May 1963[source] | 16 August 2017[source] |
|---|
| Developed into | Dassault Falcon 10 Dassault Falcon 50[source] | — |
|---|
| Capacity | 8–14 passengers[source] | 19 passengers[source] |
|---|
| Fuel capacity | 5,200 L (1,100 imp gal; 1,400 US gal)[source] | 1,600 kg[source] |
|---|
| Aspect ratio | 6.4:1[source] | — |
|---|
| Stall speed | 152 km/h (94 mph, 82 kn)[source] | 109 km/h (68 mph, 59 kn)[source] |
|---|
| National origin | France[source] | Indonesia[source] |
|---|
| Propellers | — | 4-bladed Hartzell Propeller aluminum autofeathering or 5-bladed MT-Propeller CFRP autofeathering[source] |
|---|
| g limits | — | -1.2 g to +3.0 g (flaps retracted)[source] |
|---|
| Takeoff distance | — | 435 meters (1,427 feet)[source] |
|---|
| Landing distance | — | 509 meters (1,670 feet)[source] |
|---|
| Alternative designation | — | N219[source] |
|---|