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]
EMB 110P1A/41 · Length
Single sourceConfiguration
| Specification | Dassault Falcon 20 | Embraer EMB 110 Bandeirante |
|---|---|---|
| Type | Business jet[source] | Turboprop regional airliner[source] |
| Manufacturer | Dassault Aviation[source] | Embraer[source] |
| Status | Out of production, in active service[source] | In limited commercial service, in active military service[source] |
| Primary users | Federal Express (formerly) French Navy United States Coast Guard[source] |
15.1 m (49 ft 6 in)[source]
Empty; Falcon 20F · Empty weight
Single sourceMaximum take-off; Falcon 20F · Max takeoff weight
Single source7,530 kg (16,601 lb)[source]
13,000 kg (28,660 lb)[source]
Empty; EMB 110P1A/41 · empty equipped - passengers
Single sourceMaximum take-off; EMB 110P1A/41 · Max takeoff weight
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]
Cruise; EMB 110P1A/41 · maximum at 2,440 m (8,000 ft)
Single source411 km/h (255 mph, 222 kn) maximum at 2,440 m (8,000 ft)[source]
EMB 110P1A/41 · 2 × Pratt & Whitney Canada PT6A-34 turboprop engines (750 shp) each
Single source2 × Pratt & Whitney Canada PT6A-34 turboprop engines, 560 kW (750 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]
EMB 110P1A/41 · 1,630 ft/min
Single source8.3 m/s (1,630 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Brazilian Air Force Wiggins Airways Transportes Aereos Guatemaltecos[source] |
| Number built | 512[source] | 503[source] |
|---|
| Manufactured | 1965–1991[source] | 1968–1990[source] |
|---|
| Introduction date | 3 June 1965[source] | 16 April 1973[source] |
|---|
| First flight | 4 May 1963[source] | 26 October 1968[source] |
|---|
| Developed into | Dassault Falcon 10 Dassault Falcon 50[source] | — |
|---|
| Capacity | 8–14 passengers[source] | 18 passengers[source] |
|---|
| Fuel capacity | 5,200 L (1,100 imp gal; 1,400 US gal)[source] | 1,308 kg (2,884 lb) / 1,720 L (450 US gal; 380 imp gal) in four integral wing tanks[source] |
|---|
| Aspect ratio | 6.4:1[source] | — |
|---|
| Stall speed | 152 km/h (94 mph, 82 kn)[source] | — |
|---|
| National origin | France[source] | Brazil[source] |
|---|
| Airfoil | — | root: NACA 23016 mod. ; tip: NACA 23012[source] |
|---|
| Propellers | — | 3-bladed Hartzell HC-B3TN-3C/T10178H-8R, 2.36 m (7 ft 9 in) diameter fully-feathering reversible-pitch constant-speed propellers[source] |
|---|
| Economical cruise speed | — | 341 km/h (212 mph; 184 kn) at 3,050 m (10,000 ft)[source] |
|---|
| Take-off run | — | 807 m (2,648 ft) (FAR23.135 / SFAR 41A)[source] |
|---|
| Landing run | — | 868 m (2,848 ft) at MLW[source] |
|---|