Cessna 206 Stationair

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

142
KTAS
Cruise Speed
6
Occupants
840
nm
Max Range
-
lbs
Wet Payload

Estimated Ownership Costs

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About the Cessna 206 Stationair

The Cessna 205, 206, and 207 are a family of single-engine, general aviation aircraft used for commercial air service and personal use. The 205 was introduced in 1962 with a 260 HP engine, but was replaced by the 206 in 1964. The 206 has undergone several sub-variant designs, including the U206, P206, and 206H, with varying engine power and features. The 206H, introduced in 1998, is the current production model, with a 300 HP engine and a six-seat capacity. The Cessna 207, a stretched version of the 206, was introduced in 1969 and has a seven- or eight-seat capacity. Throughout its production, the Cessna 206 family has been used for various purposes, including bush planes, aerial photography, and skydiving, and remains in production today.

Technical Specifications

Dimensions

Wingspan
36.1 ft
Length
31.5 ft
Height
9.7 ft

Weights

Max Takeoff Weight
3,789 lbs
Max Landing Weight
3,600 lbs

Performance

Cruise Speed
142 KTAS
Range
840 NM
Service Ceiling
15,700 ft
Rate of Climb
988 fpm

Engines

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