Cessna T206

Piston • single engine • High Wing • Fixed 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 — Reduce payload by lbs to safely operate this aircraft.

Mission Profile

Endorsements & ratings:
  • High-Performance
  • High-Altitude
164
KTAS
Cruise Speed
6
Occupants
703
nm
Max Range
791
lbs
Wet Payload

Estimated Ownership Costs

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About the Cessna T206

Overview

The Cessna T206 Turbo Stationair is the high-altitude sibling of the standard 206, trading some simplicity for the ability to maintain sea-level performance all the way to its 27,000 ft service ceiling. Powered by the 310 HP Lycoming TIO-540-AJ1A, the T206H is the ultimate “go anywhere, carry anything” piston single for pilots who need to clear mountain ranges or fly in high-density altitude environments without sacrificing the legendary ‘clamshell’ cargo utility of the Stationair airframe.

Key Features for GA Buyers

  • Turbocharged Performance: Maintains 310 HP up to 20,000 feet, allowing for much faster cruise speeds (up to 164-175 KTAS) than the naturally aspirated version at altitude.
  • Payload & Versatility: Known for its massive useful load (approx. 1,300 lbs), it remains one of the few aircraft that can actually carry 6 adults or a mix of heavy cargo and fuel.
  • Utility Access: The massive rear double doors are a standout feature, making it easy to load stretchers, bikes, or large camping gear.
  • Rugged Design: The heavy-duty fixed landing gear is ideal for rough strips and provides a stable platform for float or ski conversions.

Trade-offs

  • Operating Costs: The turbocharged engine runs hotter and is more complex, leading to higher maintenance costs and shorter typical engine life if not managed carefully (despite the 2,000-hr TBO).
  • High Fuel Flow: Expect fuel burns in the 16-20 GPH range when utilizing the turbocharger for high-speed cruise.
  • No Pressurization: While it can fly at 26,000 feet, the cabin is unpressurized, necessitating the use of oxygen for pilot and passengers on high-altitude legs.

Technical Specifications

Dimensions

Wingspan
36.0 ft
Length
28.3 ft
Height
9.3 ft
Parking area (ft2)
1531.8 ft2

Weights

Max Takeoff Weight
3,600 lbs
Max Landing Weight
3,600 lbs
Useful Load
1,343 lbs
Fuel Capacity
92 gal

Performance

Cruise Speed
164 KTAS
Never-Exceed (Vne)
182 KIAS
Max Structural Cruise (Vno)
149 KIAS
Approach Speed
75 KIAS
Stall, Clean (Vs1)
50 KIAS
Range
703 NM
Service Ceiling
27,000 ft
Rate of Climb
1050 fpm
Takeoff over 50 ft obstacle
1,740 ft
Landing ground roll
735 ft

Engine

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