FORCETALLY
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At a glance
Measured figures
Falcon 900B · Length
Single source20.21 m (66 ft 4 in)[source]
C-2 · Length
Single sourceConfiguration
| Specification | Dassault Falcon 900 | Kawasaki C-2 |
|---|---|---|
| Type | Business jet[source] | Military transport aircraft[source] |
| National origin | France[source] | Japan[source] |
| Manufacturer | Dassault Aviation[source] | Kawasaki Aerospace Company[source] |
| Status | Active service, in production[source] | In service, in production |
43.9 m (144 ft 0 in)[source]
C-2 · Height
Single source14.2 m (46 ft 7 in)[source]
Falcon 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]
C-2 · 2 × General Electric CF6 -80C2K1F turbofan engines thrust each
Single source2 × General Electric CF6 -80C2K1F turbofan engines, 265.7 kN (59,740 lbf) thrust each[source]
Falcon 900B · Wing area
Single source49.0 m 2 (527 sq 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] | — |
|---|
| Number built | >500[source] | 21[source] |
|---|
| Manufactured | 1984–present[source] | 2010–present[source] |
|---|
| First flight | 21 September 1984 ( 1984-09-21 )[source] | 26 January 2010[source] |
|---|
| Developed from | Dassault Falcon 50[source] | — |
|---|
| Developed into | Dassault Falcon 2000 Dassault Falcon 7X[source] | — |
|---|
| Capacity | 19 passengers[source] | 32 t limited to + 2.5g ; 36 t limited to + 2.25g ; maximum payload 37.6 t Field Operation System or Truck Crane or 8 463L Pallets or 1 UH-60JA helicopter or 1 Type 16 maneuver combat vehicle wheeled tank destroyer[source] |
|---|
| Fuel capacity | 8,690 kg (19,160 lb)[source] | — |
|---|
| Aspect ratio | 7.63:1[source] | — |
|---|
| Stall speed | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] | — |
|---|
| Primary user | — | Japan Air Self-Defense Force[source] |
|---|
| Introduction date | — | 30 June 2016[source] |
|---|
| Minimum takeoff distance | — | 500 m (1,641 ft)[source] |
|---|