Dassault Falcon 20

Airplanes

Length

17.15 m

Flat Wing Span

16.3 m

Height

5.32 m

Flat Wing Area

41 m²

Flat Wing Aspect Ratio

6.4

Max Seating

Cruise Speed

750 km/h

Max Speed

862 km/h

Max Ceiling

12800 m

Number of Engines

Aircraft Engine

First Flight

1963-05-04

Entry Into service

1965-06-03

Number Built

512

Maximum Take-Off Weight

13 t (paragliders: kg)

Total Fuel Capacity

5200

Maximum Range

3350 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Dassault Falcon 20	13	5200	3350

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Gulfstream G100	Garrett TFE731	16.94	16.64	9	Compare
Hawker 800 (Raytheon)		15.5448	15.5448		Compare
Ilyushin Il-30		18	16.5		Compare
Cessna Citation III	Garrett TFE731	16.9	16.31	9	Compare
Ilyushin Il-108	Lotarev DV-2	15.85	15	15	Compare
Tupolev Tu-82	Klimov VK-1	17.57	17.81		Compare

All data (29 fields)

Name: Dassault Falcon 20
Manufacturer: Dassault Aviation
Description: The Dassault Falcon 20 is a French business jet developed and manufactured by Dassault Aviation.
ICAO Code: FA20
First Flight: 1963-05-04
Entry Into service: 1965-06-03
Production End: 1991-01-01
Designer: Dassault Aviation
Type: Business jet
Length (m): 17.15
Height (m): 5.32
Cockpit Crew: 2
Max Seating: 14
Max Speed (km/h): 862
Cruise Speed (km/h): 750
Min Speed (km/h): 152
Max Ceiling (m): 12800
Capacity Description: 8–14 passengers
Number Built: 512
Powerplant Description: 2 × General Electric CF700-2D-2 turbofans, 20 kN thrust each
Primary Users: Federal Express (formerly), French Navy , United States Coast Guard
Status: Out of production, in active service
Wikipedia Article (URL): en.wikipedia.org/wiki/Dassault_Falcon_20
Flat Wing Span (m): 16.3
Flat Wing Area (m²): 41
Flat Wing Aspect Ratio: 6.4
Wake Category: M
Aircraft Engine: General Electric CF700
Number of Engines: 2