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At a glance
Measured figures
Conquest II · Length
Single source39 ft 0 in (11.89 m)[source]
Falcon 900B · Length
Configuration
| Specification | Cessna 441 Conquest II | Dassault Falcon 900 |
|---|---|---|
| Type | Utility aircraft[source] | Business jet[source] |
| National origin | United States[source] | France[source] |
| Manufacturer | Cessna[source] | Dassault Aviation[source] |
| Number built | 362[source] |
20.21 m (66 ft 4 in)[source]
Conquest II · Height
Single source13 ft 2 in (4.01 m)[source]
Conquest II · 2 × Garrett TPE331 -8-403S turboprops, 636 shp ( ) each
Single source2 × Garrett TPE331 -8-403S turboprops, 636 shp (474 kW) each[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]
Conquest II · 2,435 ft/min (
Single source2,435 ft/min (12.37 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
>500[source] |
| Manufactured | 1977–1986[source] | 1984–present[source] |
|---|
| First flight | August 26, 1975[source] | 21 September 1984 ( 1984-09-21 )[source] |
|---|
| Developed from | Cessna 404 Titan[source] | Dassault Falcon 50[source] |
|---|
| Capacity | Up to 10 passengers with one pilot; up to 9 passengers with two pilots[source] | 19 passengers[source] |
|---|
| Aspect ratio | 9.6:1[source] | 7.63:1[source] |
|---|
| Airfoil | NACA 23018 at root, NACA 23019 at tip[source] | — |
|---|
| Propellers | 3-bladed Hartzell or McCauley[source] | — |
|---|
| Stall speed | 86 mph (139 km/h, 75 kn) flaps and gear down[source] | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] |
|---|
| Status | — | Active service, in production[source] |
|---|
| Primary users | — | French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force[source] |
|---|
| Developed into | — | Dassault Falcon 2000 Dassault Falcon 7X[source] |
|---|
| Fuel capacity | — | 8,690 kg (19,160 lb)[source] |
|---|