FORCETALLY
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At a glance
Measured figures
Length
Single source34 ft 2 in (10.41 m)[source]
Falcon 900B · Length
Single sourceConfiguration
| Specification | Daher Kodiak | Dassault Falcon 900 |
|---|---|---|
| Type | Utility aircraft[source] | Business jet[source] |
| National origin | United States[source] | France[source] |
| Manufacturer | Quest Aircraft Daher[source] | Dassault Aviation[source] |
| Designer | Evan Mortenson[source] | — |
| Status |
20.21 m (66 ft 4 in)[source]
1 × Pratt & Whitney Canada PT6 A-34 turboprop , 750 shp ( ) takeoff power (700 shp (
Single source) continuous
Single source1 × Pratt & Whitney Canada PT6 A-34 turboprop , 750 shp (560 kW) takeoff power (700 shp (520 kW) continuous)[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]
1,371 ft/min (
Single source1,371 ft/min (6.96 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
In production[source] |
Active service, in production[source] |
| Number built | 300 (2021)[source] | >500[source] |
|---|
| Manufactured | 2007-present[source] | 1984–present[source] |
|---|
| Introduction date | January 2008[source] | — |
|---|
| First flight | October 16, 2004[source] | 21 September 1984 ( 1984-09-21 )[source] |
|---|
| Capacity | 9 passengers[source] | 19 passengers[source] |
|---|
| Aspect ratio | 8.4[source] | 7.63:1[source] |
|---|
| Propellers | 4-bladed constant speed, feathering, reversible, 8 ft 0 in (2.44 m) diameter[source] | — |
|---|
| Stall speed | 69 mph (110 km/h, 60 kn) (flaps down)[source] | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] |
|---|
| Wing loading | 30.2 lb/sq ft (147 kg/m 2 )[source] | — |
|---|
| Take-off distance | 934 ft (285 m)[source] | — |
|---|
| Landing roll | 705 ft (215 m)[source] | — |
|---|
| Primary users | — | French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force[source] |
|---|
| Developed from | — | Dassault Falcon 50[source] |
|---|
| Developed into | — | Dassault Falcon 2000 Dassault Falcon 7X[source] |
|---|
| Fuel capacity | — | 8,690 kg (19,160 lb)[source] |
|---|