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Aeroprints.com · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
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At a glance
Measured figures
Falcon 20F · Length
Single source17.15 m (56 ft 3 in)[source]
MC-130J Commando II · Length
Single sourceConfiguration
| Specification | Dassault Falcon 20 | Lockheed MC-130 |
|---|---|---|
| Type | Business jet[source] | STOL Special operations military transport aircraft[source] |
| Manufacturer | Dassault Aviation[source] | Lockheed Corporation[source] |
| Status | Out of production, in active service[source] | Active[source] |
| Primary users | Federal Express (formerly) French Navy United States Coast Guard[source] | — |
97 ft 9 in (29.79 m)[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; MC-130J Commando II · at 22,000 feet
Single source417 mph (671 km/h, 362 kn) at 22,000 feet[source]
MC-130J Commando II · 4 × Rolls-Royce AE 2100D3 turboprop engines, 4,591 shp ( ) each
Single source4 × Rolls-Royce AE 2100D3 turboprop engines, 4,591 shp (3,424 kW) 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]
Falcon 20F · Wing area
Single source41.00 m 2 (441.3 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built | 512[source] | MC-130E: 18 MC-130H: 24 MC-130P: 28 MC-130W: 12 MC-130J: 64[source] |
|---|
| Manufactured | 1965–1991[source] | — |
|---|
| Introduction date | 3 June 1965[source] | MC-130E: 1966 MC-130P: 1986 MC-130H: 1991 MC-130W: 2006 MC-130J: 2012[source] |
|---|
| First flight | 4 May 1963[source] | MC-130J: April 2011[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] | — |
|---|
| Primary user | — | United States Air Force[source] |
|---|
| Retired | — | MC-130E: April 15, 2013 MC-130P: May 15, 2015 MC-130H: April 2, 2023[source] |
|---|
| Developed from | — | C-130 Hercules C-130J Super Hercules[source] |
|---|
| Propellers | — | 6-bladed fully feathering reversible propellers[source] |
|---|
| Country of origin | — | United States[source] United States[source] |
|---|