Cessna T210 Turbo Centurion
Piston • single engine • High Wing • Retractable gear
Range Visualization
Origin: · click map to move · nm at current load
Payload vs. Range
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Default: 190 lbs (FAA standard)
Default: 30 lbs
Passengers
lbs
@ lbs / pax
0 lbs
Fuel on board
gal
+ Weight
Range
Available Range
/ nm
Mission capable —
Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required —
You'll need to leave gallons of fuel behind
( gal usable for nm range).
Over max gross weight —
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Mission Profile
168
KTAS
Cruise Speed
6
Occupants
900
nm
Max Range
-
lbs
Wet Payload
About the Cessna T210 Turbo Centurion
The Cessna 210 Centurion is a six-seat, high-performance, single-engined aircraft introduced in 1957. It was produced by Cessna until 1986 and featured various design changes over the years, including a wider and deeper fuselage, a cantilever wing, and improved avionics. The T210 is a turbocharged version introduced in 1970.
Technical Specifications
Dimensions
- Wingspan
- 38.8 ft
- Length
- 28.2 ft
- Height
- 9.7 ft
Weights
- Max Takeoff Weight
- 3,800 lbs
- Max Landing Weight
- 3,800 lbs
- Fuel Capacity
- 90 gal
Performance
- Cruise Speed
- 168 KTAS
- Range
- 900 NM
- Service Ceiling
- 27,000 ft
- Rate of Climb
- 930 fpm
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