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 20 |
|---|---|---|
| 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] | 512 |
Falcon 20F · Length
17.15 m (56 ft 3 in)[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 20F · Empty weight
Single sourceMaximum take-off; Falcon 20F · Max takeoff weight
Single sourceCruise; T210N Turbo Centurion II · at 20,000 ft (6,100 m) (80% power)
Single sourceMaximum; T210N Turbo Centurion II · at 17,000 ft (5,200 m)
Single source204 kn (235 mph, 378 km/h) at 17,000 ft (5,200 m)[source]
193 kn (222 mph, 357 km/h) at 20,000 ft (6,100 m) (80% power)[source]
Cruise; Falcon 20F · at 12,200 m (40,000 ft) (econ. cruise)
Single sourceMaximum; Falcon 20F · at 7,620 m (25,000 ft) (max cruise)
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 20F · 2 × General Electric CF700 -2D-2 turbofans thrust each
Single source2 × General Electric CF700 -2D-2 turbofans , 20 kN (4,500 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] | 1965–1991[source] |
|---|
| Introduction date | 1957[source] | 3 June 1965[source] |
|---|
| First flight | January 1957[source] | 4 May 1963[source] |
|---|
| Developed from | Cessna 182 Skylane[source] | — |
|---|
| Developed into | Cessna 205/206/207[source] | Dassault Falcon 10 Dassault Falcon 50[source] |
|---|
| Capacity | Five passengers[source] | 8–14 passengers[source] |
|---|
| Fuel capacity | 87 US gal (72 imp gal; 330 L) (usable capacity)[source] | 5,200 L (1,100 imp gal; 1,400 US gal)[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] | 152 km/h (94 mph, 82 kn)[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 | — | Out of production, in active service[source] |
|---|
| Primary users | — | Federal Express (formerly) French Navy United States Coast Guard[source] |
|---|
| Aspect ratio | — | 6.4:1[source] |
|---|