Credit
Aeroprints.com · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
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Measured figures
Falcon 20F · Length
Single source17.15 m (56 ft 3 in)[source]
Configuration
| Specification | Dassault Falcon 20 | Lockheed LC-130 |
|---|---|---|
| Type | Business jet[source] | Ski -equipped military transport aircraft[source] |
| Manufacturer | Dassault Aviation[source] | Lockheed Lockheed Martin[source] |
| Status | Out of production, in active service[source] | Active[source] |
| Primary users | Federal Express (formerly) French Navy United States Coast Guard[source] | United States Air Force United States Navy (former) |
Falcon 20F · Wingspan
Single source16.30 m (53 ft 6 in)[source]
Falcon 20F · Height
Single source5.32 m (17 ft 5 in)[source]
Falcon 20F · Crew
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]
Falcon 20F · Range
Single source3,350 km (2,080 mi, 1,810 nmi)[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] | 1956[source] |
|---|
| Developed into | Dassault Falcon 10 Dassault Falcon 50[source] | — |
|---|
| Capacity | 8–14 passengers[source] | — |
|---|
| Fuel capacity | 5,200 L (1,100 imp gal; 1,400 US gal)[source] | — |
|---|
| Aspect ratio | 6.4:1[source] | — |
|---|
| Stall speed | 152 km/h (94 mph, 82 kn)[source] | — |
|---|
| National origin | France[source] | United States[source] |
|---|
| Developed from | — | C-130 Hercules[source] |
|---|