FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
Be-200 · Length
Single source32 m (105 ft 0 in)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Beriev Be-200 | Cirrus SR20 |
|---|---|---|
| Type | Multirole amphibious aircraft[source] | Light aircraft[source] |
| National origin | Russia[source] | United States[source] |
| Manufacturer | Taganrog Beriev plant[source] | Cirrus Aircraft[source] |
| Designer | Beriev Aircraft Company[source] | — |
| Status |
26 ft 0 in (7.92 m)[source]
Cruise; Be-200 · Cruise speed
Single sourceCruise; Be-200 · * Economy cruise speed
Single sourceMaximum; Be-200 · Maximum speed
Single source700 km/h (430 mph, 380 kn)[source]
560 km/h (350 mph, 300 kn) * Economy cruise speed: 550 km/h (340 mph; 300 kn)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
SR20-G3 · 1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine
Single source1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine , 200 hp (150 kW)[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]
Be-200 · Wing area
Single source117.4 m 2 (1,264 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
In service, In production[source] |
| — |
| Primary user | EMERCOM[source] | — |
|---|
| Number built | 20[source] | 2,084 (through 2025)[source] |
|---|
| Introduction date | 31 July 2003 ( 2003-07-31 )[source] | — |
|---|
| First flight | 24 September 1998[source] | 21 March 1995[source] |
|---|
| Developed from | Beriev A-40[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] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[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] | — |
|---|
| Manufactured | — | 1999–present[source] |
|---|
| Developed into | — | Cirrus SR22[source] |
|---|
| Propellers | — | 3-bladed[source] |
|---|
| Stall speed | — | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|