Cessna 206 Stationair

The high-wing utility aircraft built for rugged versatility.

Overview

Cessna United States ICAO: C206 1962–Present Active $740,000 (2020)

The Cessna 206 Stationair was introduced in the 1960s as a six-seat utility aircraft. Designed for hauling passengers and cargo, it became popular in remote regions. The model remains in production in updated forms.

Live Fleet Activity (C206)

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Specifications

Units
Engine
1 × Lycoming IO 540 AC1 A5
Engine type
Piston
Power
300 hp · 224 kW
Avionics
Garmin G1000 glass cockpit
Wing tips
No winglets
Seats
6
Crew
—
Cabin width
3 ft 7 in  ·  1.10 m
Cabin height
4 ft 3 in  ·  1.30 m
Cabin length
12 ft 1 in  ·  3.68 m
Exterior length
28 ft 3 in  ·  8.60 m
Tail height
9 ft 2 in  ·  2.80 m
Fuselage diameter
3 ft 11 in  ·  1.20 m
Wing span
36 ft 0 in  ·  10.97 m
Baggage volume
—
Gross weight
—
Empty weight
—
Max takeoff weight
3,600 lb  ·  1,650 kg
Max landing weight
—
Max payload
1,250 lb  ·  550 kg
Fuel capacity
90 gal · 300 L · 300 kg (AvGas)
Max cruise speed
151 kt  ·  174 mph  ·  280 km/h
Maximum speed
—
Cruise speed
—
Approach speed
57 kt  ·  66 mph  ·  106 km/h
Range
721 nm  ·  830 mi  ·  1,340 km
Fuel burn
7.80 nm/gal  ·  3.82 km/L
Ceiling
15,700 ft  ·  4,800 m
Rate of climb
960 ft/min  ·  5 m/s
Takeoff distance
1,860 ft  ·  570 m
Landing distance
1,390 ft  ·  430 m
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Cessna 206 ‘PP-SLN’

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Operational Context

Cessna 206 Stationair — high-wing single-engine utility aircraft

The 206 first flew in 1962 and entered service shortly afterward. It features a high-wing configuration and fixed landing gear. Large doors facilitate cargo loading and passenger access.

A Lycoming piston engine producing approximately 300 horsepower powers the aircraft. Cruise speed approaches 140 knots (259 km/h). Maximum takeoff weight exceeds 3,600 pounds (1,633 kg).

The Stationair is widely used in bush flying, charter, and special missions. Its durability and load capacity support diverse operations. The aircraft remains a mainstay of utility aviation.