Cessna 206 Stationair vs Cessna T210 Turbo Centurion

Side-by-side specs, range, and operating costs.

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Cessna 206 Stationair
36 ft × 28 ft ⭥ 9 ft
1× Piston Fixed Unpressurized
Cessna T210 Turbo Centurion
39 ft × 28 ft ⭥ 10 ft
1× Piston Retractable Unpressurized

Flight Profile

Service ceiling, range, and climb rate.

Tap legend to isolate

Arc represents the climb-cruise-descent profile based on published service ceiling and range. Climb rate annotated on ascent. FL180 (18,000 ft) shown for reference.

Mission Performance

Stall, approach, cruise, range, ceiling and climb: best values are at the top.

Mission performance specifications
Specification Cessna 206 StationairCessna T210 Turbo Centurion
Stall speed 54 kt58 kt
Approach speed 70 kt73 kt
Cruise speed 142 kt190 kt
Range 730 nm900 nm
Service ceiling 15700 ft27000 ft
Rate of climb 988 fpm930 fpm
Fuel burn 15.8 gph15.0 gph

Each axis is scaled independently across the compared aircraft and printed in its own units; every vertex sits at the published figure. Higher is better on all axes: Stall, Approach and Fuel Burn are inverted (lower = higher). A missing figure breaks the line at that axis.

Fuel Burn & Range

Range, endurance, and what the fuel costs by the hour.

Cessna 206 Stationair Avgas
15.8 gph
Baseline
730 nm range 9.0 nm/gal 88 gal usable $103 fuel/hr 5h 34m endurance
Cessna 206 Stationair: 15.8 gph at cruise, 730 nautical mile published range, 5 hour 34 minute endurance, 9.0 nautical miles per gallon.
Cessna T210 Turbo Centurion Avgas
15.0 gph
Baseline
900 nm range 12.7 nm/gal 89 gal usable $98 fuel/hr 5h 56m endurance
Cessna T210 Turbo Centurion: 15.0 gph at cruise, 900 nautical mile published range, 5 hour 56 minute endurance, 12.7 nautical miles per gallon.
Avgas range each cell = 1 hr of cruise · width scales with speed

Bars show published still-air range: select a cell to view cruise-hours and fuel usage. Endurance is full tank at the displayed cruise burn rate; the extra is reserve and economy margin. Estimates only. Always verify against the POH.

Runway Performance

Density altitude adjusted estimates

Outside Air Temp
0°F57°F115°F
Field Elevation
SL4,0008,000 ft

Takeoff over 50 ft obstacle

Landing over 50 ft obstacle

Density Altitude

Monte cristo

Base distance DA penalty
Scale: 6,000 ft

FAA 10%/1,000 ft DA rule of thumb (FAA-H-8083-25B). Turboprops and jets are less sensitive in practice. Always verify against the POH.

Estimated Operating Costs

Hourly direct and annual fixed costs

Scale:
Cessna 206 Stationair Avgas
$155 /hr
Baseline
Cessna 206 Stationair: $155 per flight hour — fuel $103, maintenance and reserve $52.
Cessna T210 Turbo Centurion Avgas
$201 /hr
Baseline
Cessna T210 Turbo Centurion: $201 per flight hour — fuel $98, maintenance and reserve $103.
Cessna 206 Stationair Piston
$13,700 /yr Baseline
Cessna 206 Stationair: $13,700 per year — insurance $4,500, hangar $6,000, annual inspection $3,200.
Cessna T210 Turbo Centurion Piston
$14,591 /yr Baseline
Cessna T210 Turbo Centurion: $14,591 per year — insurance $3,800, hangar $7,291, annual inspection $3,500.

Estimates only. Hourly direct operating cost, based on fuel price and reserves; Annual fixed costs (insurance, hangar, and inspection). Costs vary by location, pilot profile, and market conditions. See individual aircraft pages for source notes.

Capability & limits

Payload vs useful load limit

+ cargo
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Cessna 206 Stationair Piston
6 / 6 seats cargo 88 gal / 88 gal fuel 815 lbs wet payload 1,343 lbs useful 3,600 lbs MTOW
Cessna T210 Turbo Centurion Piston
6 / 6 seats cargo 89 gal / 89 gal fuel 1,001 lbs wet payload 1,535 lbs useful 4,000 lbs MTOW

Shows selected occupants against full fuel, within the aircraft's useful-load limit. Fuel weight at 6.7 lb/gal jet-A, 6.0 lb/gal avgas; pax and luggage are 190 + 30 . Change payload weights in global settings.

Payload-Range Map

Origin: → · two fingers to move map

+ cargo
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