FORCETALLY
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Measured figures
Falcon 900B · Length
Single source20.21 m (66 ft 4 in)[source]
Configuration
| Specification | Dassault Falcon 900 | Lockheed LC-130 |
|---|---|---|
| Type | Business jet[source] | Ski -equipped military transport aircraft[source] |
| National origin | France[source] | United States[source] |
| Manufacturer | Dassault Aviation[source] | Lockheed Lockheed Martin[source] |
| Status | Active service, in production[source] | Active |
Falcon 900B · Wingspan
Single source19.33 m (63 ft 5 in)[source]
Falcon 900B · Crew
Single sourceFalcon 900B · with 8 passengers
Single source7,400 km (4,600 mi, 4,000 nmi) with 8 passengers[source]
Falcon 900B · 3 × Honeywell TFE731 -5BR-1C turbofans thrust each
Single source3 × Honeywell TFE731 -5BR-1C turbofans , 21.13 kN (4,750 lbf) thrust each[source]
Falcon 900B · Wing area
Single source49.0 m 2 (527 sq ft)[source]
Falcon 900B · Service ceiling
Single source15,500 m (50,900 ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force[source] | United States Air Force United States Navy (former)[source] |
|---|
| Number built | >500[source] | — |
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| Manufactured | 1984–present[source] | — |
|---|
| First flight | 21 September 1984 ( 1984-09-21 )[source] | 1956[source] |
|---|
| Developed from | Dassault Falcon 50[source] | C-130 Hercules[source] |
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| Developed into | Dassault Falcon 2000 Dassault Falcon 7X[source] | — |
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| Capacity | 19 passengers[source] | — |
|---|
| Fuel capacity | 8,690 kg (19,160 lb)[source] | — |
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| Aspect ratio | 7.63:1[source] | — |
|---|
| Stall speed | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] | — |
|---|