FORCETALLY
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At a glance
Measured figures
T210N Turbo Centurion II · Length
Single source28 ft 2 in (8.59 m)[source]
Configuration
| Specification | Cessna 210 Centurion | Dassault Falcon 900 |
|---|---|---|
| Type | Light aircraft[source] | Business jet[source] |
| National origin | United States[source] | France[source] |
| Manufacturer | Cessna[source] | Dassault Aviation[source] |
| Number built | 9,240[source] | >500 |
Falcon 900B · Length
20.21 m (66 ft 4 in)[source]
T210N Turbo Centurion II · Height
Single source9 ft 8 in (2.95 m)[source]
Empty; T210N Turbo Centurion II · Empty weight
Single sourceGross; T210N Turbo Centurion II · Gross weight
Single source2,303 lb (1,045 kg)[source]
4,000 lb (1,814 kg)[source]
Empty; Falcon 900B · Empty weight
Single sourceMaximum take-off; Falcon 900B · Max takeoff weight
Single sourceT210N Turbo Centurion II · 1 × Continental Motors TSIO-520-R air-cooled turbocharged flat-six
Single source1 × Continental Motors TSIO-520-R air-cooled turbocharged flat-six , 310 hp (230 kW)[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]
T210N Turbo Centurion II · 930 ft/min (
Single source930 ft/min (4.7 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1957–1986[source] | 1984–present[source] |
|---|
| Introduction date | 1957[source] | — |
|---|
| First flight | January 1957[source] | 21 September 1984 ( 1984-09-21 )[source] |
|---|
| Developed from | Cessna 182 Skylane[source] | Dassault Falcon 50[source] |
|---|
| Developed into | Cessna 205/206/207[source] | Dassault Falcon 2000 Dassault Falcon 7X[source] |
|---|
| Capacity | Five passengers[source] | 19 passengers[source] |
|---|
| Fuel capacity | 87 US gal (72 imp gal; 330 L) (usable capacity)[source] | 8,690 kg (19,160 lb)[source] |
|---|
| Propellers | 3-bladed McCauley Type D3A34C402/90DFA-10 constant-speed propeller , 7 ft 6 in (2.29 m) diameter[source] | — |
|---|
| Stall speed | 58 kn (67 mph, 107 km/h) (power off, flaps down) ( CAS )[source] | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] |
|---|
| Takeoff distance to 50 ft (15 m) | 2,160 ft (660 m)[source] | — |
|---|
| Landing distance from 50 ft (15 m) | 1,500 ft (460 m)[source] | — |
|---|
| Alternative designation | Cessna 210[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] |
|---|
| Aspect ratio | — | 7.63:1[source] |
|---|