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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]
L-100-30 · Length
Single sourceConfiguration
| Specification | Dassault Falcon 20 | Lockheed L-100 Hercules |
|---|---|---|
| Type | Business jet[source] | Civilian cargo aircraft[source] |
| Manufacturer | Dassault Aviation[source] | Lockheed Lockheed Martin (LM-100J)[source] |
| Status | Out of production, in active service[source] | In service for cargo transport (L-100) Flight testing (LM-100J)[source] |
| Primary users | Federal Express (formerly) French Navy United States Coast Guard[source] |
112 ft 9 in (34.35 m)[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; L-100-30 · Empty weight
Single sourceMaximum take-off; L-100-30 · 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; L-100-30 · Cruise speed
Single sourceMaximum; L-100-30 · at 20,000 ft (6,100 m)
Single sourceL-100-30 · 4 × Allison 501-D22A turboprops , 4,510 shp ( ) each
Single source4 × Allison 501-D22A turboprops , 4,510 shp (3,360 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]
L-100-30 · 1,830 ft/min (
Single source1,830 ft/min (9.3 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Indonesian Air Force Safair Lynden Air Cargo Transafrik International[source] |
| Number built | 512[source] | 114[source] |
|---|
| Manufactured | 1965–1991[source] | 1964–1992, 2018–present (LM-100J planned)[source] |
|---|
| Introduction date | 3 June 1965[source] | September 30, 1965[source] |
|---|
| First flight | 4 May 1963[source] | April 20, 1964 (L-100) May 25, 2017 (LM-100J)[source] |
|---|
| Developed into | Dassault Falcon 10 Dassault Falcon 50[source] | — |
|---|
| Capacity | 8–14 passengers[source] | 51,050 lb (23,150 kg)[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 | — | Lockheed C-130 Hercules Lockheed Martin C-130J Super Hercules[source] |
|---|