FORCETALLY
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At a glance
Measured figures
Be-200 · Length
Single source32 m (105 ft 0 in)[source]
Falcon 900B · Length
Single sourceConfiguration
| Specification | Beriev Be-200 | Dassault Falcon 900 |
|---|---|---|
| Type | Multirole amphibious aircraft[source] | Business jet[source] |
| National origin | Russia[source] | France[source] |
| Manufacturer | Taganrog Beriev plant[source] | Dassault Aviation[source] |
| Designer | Beriev Aircraft Company[source] | — |
20.21 m (66 ft 4 in)[source]
Be-200 · Height
Single source8.9 m (29 ft 2 in)[source]
Be-200 · 2 × Progress D-436TP turbofan engines thrust each
Single source2 × Progress D-436TP turbofan engines, 73.55 kN (16,534 lbf) thrust 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]
Be-200 · (2,600 ft/min) at Sea Level, MTOW and Flaps 20°
Single source13 m/s (2,600 ft/min) at Sea Level, MTOW and Flaps 20°[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status |
|---|
In service, In production[source] |
Active service, in production[source] |
| Primary user | EMERCOM[source] | — |
|---|
| Number built | 20[source] | >500[source] |
|---|
| Introduction date | 31 July 2003 ( 2003-07-31 )[source] | — |
|---|
| First flight | 24 September 1998[source] | 21 September 1984 ( 1984-09-21 )[source] |
|---|
| Developed from | Beriev A-40[source] | Dassault Falcon 50[source] |
|---|
| Capacity | 44 pax Be-200ES / 72 pax Be-210 / 7,500 kg (16,500 lb) cargo payload / 12,000 kg (26,000 lb) water or retardant[source] | 19 passengers[source] |
|---|
| Airfoil | root: TsAGI 16%; tip: TsAGI 11.5%[source] | — |
|---|
| Max Take Off Weight (Water) | 37,900 kg (83,600 lb)[source] | — |
|---|
| Landing speed | 200 km/h (120 mph; 110 kn)[source] | — |
|---|
| Takeoff speed | 220 km/h (140 mph; 120 kn)[source] | — |
|---|
| Minimum speed (Flaps 38°) | 157 km/h (98 mph; 85 kn)[source] | — |
|---|
| Primary users | — | French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force[source] |
|---|
| Manufactured | — | 1984–present[source] |
|---|
| Developed into | — | Dassault Falcon 2000 Dassault Falcon 7X[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] |
|---|