Aircraft Data for: Dassault Falcon 20 - | Updated: Jan. 22nd 2009 |
| Summary: | The Falcon 20 is a twin engined short/medium range mid sized corporate aircraft.It was one of the first business jets built and was derived from Dassault military designs. Originally called the Mystere 20, it sold very well in the USA market. | | |
Country of origin: France
First flight: 1963
No. built: 477
No. in service: 400 (approx.)
Crew: 2
Passengers: 9
- 12
| | | | Power: | 2 x General Electric CFE700 (4200 - 4500 lbf) turbofan engines |
| | Typical engines would be the GE CF700-2D2 turbofans at 4500lb thrust. Some Falcon 20s have been re-engined with Garrett TFE-731-5AR-2C or TFE-731-5BR-2C engines, as Falcon 20-5s, these have their range increased by 50%. |
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| Dimensions: |
| Length: | | 56 ft. 3 in.
| | Wing Span: | | 53 ft. 6 in.
| | Height: | | 17 ft. 5 in.
| | Empty Weight: | | 16,300 lbs.
(Weights apply to the 20E versions )
| | Max. Weight: | | 26,660 lbs.
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| | | Performance: |
| Max. speed: | | 465
kts (Performance applies to the 20E version)
| | Cruise speed: | | 370
kts | | Ceiling: | | 42,000 ft.
| | Normal range: | | 1,430
nm | | Max. range: | | 1,900
nm |
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