FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
T210N Turbo Centurion II · Length
Single source28 ft 2 in (8.59 m)[source]
SR20-G3 · Length
Configuration
| Specification | Cessna 210 Centurion | Cirrus SR20 |
|---|---|---|
| Type | Light aircraft[source] | Light aircraft[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Cessna[source] | Cirrus Aircraft[source] |
| Number built | 9,240[source] | 2,084 (through 2025) |
26 ft 0 in (7.92 m)[source]
Cruise; 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; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
T210N Turbo Centurion II · at 10,000 ft (3,000 m) (econ cruise)
Single source900 nmi (1,000 mi, 1,700 km) at 10,000 ft (3,000 m) (econ cruise)[source]
T210N 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]
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]
T210N Turbo Centurion II · Wing area
Single source175 sq ft (16.3 m 2 )[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1957–1986[source] | 1999–present[source] |
|---|
| Introduction date | 1957[source] | — |
|---|
| First flight | January 1957[source] | 21 March 1995[source] |
|---|
| Developed from | Cessna 182 Skylane[source] | — |
|---|
| Developed into | Cessna 205/206/207[source] | Cirrus SR22[source] |
|---|
| Capacity | Five passengers[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Fuel capacity | 87 US gal (72 imp gal; 330 L) (usable capacity)[source] | — |
|---|
| Propellers | 3-bladed McCauley Type D3A34C402/90DFA-10 constant-speed propeller , 7 ft 6 in (2.29 m) diameter[source] | 3-bladed[source] |
|---|
| Stall speed | 58 kn (67 mph, 107 km/h) (power off, flaps down) ( CAS )[source] | 56 kn (64 mph, 104 km/h) CAS[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] | — |
|---|