Aircraft / Cessna / U206
Cessna Certified · Fixed-wing · United States
U206
Seats 6 6
Power 300 hp 224 kW
Cruise 142 kt 262 km/h
US register 52 aircraft 52 aircraft
Photo: Carlos E. Perez S.L · CC BY-SA 4.0
About the U206
The Textron Aviation U206 is a single-engine, fixed-landing-gear fixed-wing aircraft featuring a high-wing configuration. Suited for both commercial service and personal transportation, the type offers a spacious cabin layout, a powerful powerplant, and rugged construction that appeals to operators needing utility transport.
Developing out of a popular retractable-gear predecessor created by the Cessna Aircraft Company, this aircraft family has found widespread application as a bush plane, as well as in aerial photography and skydiving operations. Operators can adapt the airframe with floats, skis, or luxury cabin furnishings depending on the mission profile. Continuous manufacturing over several decades has yielded thousands of airframes.
Engines fitted 46 aircraft
Engine Power Share of fleet Aircraft
Continental IO-520
285 hp
44
Continental TSIO-520
300 hp
1
Continental O-520
320 hp
1
U206 variants
Designation Seats Engine power Max take-off weight Cruise speed Range
U206 This page
6 6 300 hp 224 kW 3,600 lb 1,633 kg 142 kt 262 km/h 730 nm 1,352 km
U206 Super Skywagon
6 6 300 hp 224 kW 3,600 lb 1,633 kg 142 kt 262 km/h 730 nm 1,352 km
U206A
6 6 300 hp 224 kW 3,600 lb 1,633 kg 142 kt 262 km/h 730 nm 1,352 km
U206B
6 6 300 hp 224 kW 3,600 lb 1,633 kg 142 kt 262 km/h 730 nm 1,352 km
U206C
6 6 300 hp 224 kW 3,600 lb 1,633 kg 142 kt 262 km/h 730 nm 1,352 km
U206E
6 6 300 hp 224 kW 3,600 lb 1,633 kg 142 kt 262 km/h 730 nm 1,352 km
U206F
6 6 300 hp 224 kW 3,600 lb 1,633 kg 142 kt 262 km/h 730 nm 1,352 km
U206G
6 6 300 hp 224 kW 3,600 lb 1,633 kg 142 kt 262 km/h 730 nm 1,352 km
This page covers the Cessna CESSNA U 206: the same aircraft under other designations.
Specifications 206H Stationair · Lycoming IO-540-AC1A
US Metric
Dimensions
Length 28 ft 0 in 8.53 m 8.53 m 28 ft 0 in
Wingspan 36 ft 0 in 10.97 m 10.97 m 36 ft 0 in
Wing area 175 sq ft 16.3 m² 16.3 m² 175 sq ft
Weights
Empty weight 2,176 lb 987 kg 987 kg 2,176 lb
Max take-off weight 3,600 lb 1,633 kg 1,633 kg 3,600 lb
Performance
Cruise speed 142 kt 262 km/h 262 km/h 142 kt
Max speed 151 kt 280 km/h 280 km/h 151 kt
Stall speed 55 kt 101 km/h 101 km/h 55 kt
Range 730 nm 1,352 km 1,352 km 730 nm
Service ceiling 15,700 ft 4,785 m 4,785 m 15,700 ft
Rate of climb 990 ft/min 5.0 m/s 5.0 m/s 990 ft/min
Powerplant
Engine Lycoming IO-540-AC1A
Engine power 300 hp 224 kW 224 kW 300 hp
ICAO type designator C206
Type certificate US A4CE
On the US register 52
Registered in Brazil, Australia, United States, Canada
1975 · 7,080 h USD
Low $211,000
Typical $258,000
High $309,000
By year built · United States · USD
Built Hours Low Typical High
1960 7,830 $156,000 $191,000 $228,000 1965 6,580 $178,000 $218,000 $261,000 1970 6,580 $196,000 $239,000 $286,000 1975 7,080 $211,000 $258,000 $309,000 1980 7,080 $231,000 $283,000 $339,000 2005 1,350 $540,000 $661,000 $791,000
By year built · United Kingdom · GBP
Built Hours Low Typical High
1960 7,820 £108,000 £143,000 £184,000 1965 7,190 £121,000 £160,000 £206,000 1970 5,720 £140,000 £185,000 £238,000 1975 4,860 £160,000 £211,000 £272,000 1980 5,100 £173,000 £229,000 £295,000 1985 3,580 £206,000 £273,000 £351,000 2005 1,350 £374,000 £494,000 £637,000
By year built · Euro countries · EUR
Built Hours Low Typical High
1960 7,820 €111,000 €146,000 €188,000 1965 7,190 €124,000 €164,000 €211,000 1970 5,720 €143,000 €189,000 €244,000 1975 4,860 €163,000 €216,000 €278,000 1980 5,100 €177,000 €234,000 €302,000 1985 3,580 €211,000 €279,000 €359,000 2005 1,350 €383,000 €506,000 €652,000
By year built · Elsewhere · USD
Built Hours Low Typical High
1960 7,800 $182,000 $223,000 $291,000 1965 7,800 $199,000 $244,000 $320,000 1970 9,880 $207,000 $253,000 $332,000 1975 5,060 $266,000 $325,000 $426,000 1980 6,080 $279,000 $342,000 $447,000
U206 running costs $438 an hour
A year
Low Typical High
Fuel $9,815 $12,546 $14,694 Oil $228 $285 $370 Engine overhaul reserve $3,333 $3,958 $5,192 Propeller overhaul reserve $917 $1,083 $1,250 Annual inspection and maintenance $3,000 $4,000 $5,000 Hangar $3,000 $6,300 $9,600 Insurance $2,550 $3,200 $3,850 Depreciation $6,194 $12,389 $18,583
Total $29,037 $43,761 $58,539
Per hour $290 $438 $585
Engine
Model Continental IO-520
Power 285 hp
Overhaul 1,900 h / 12 yr
Fuel burn 13.0 – 16.4 gal/h
Fuel price $8.20 /US gal
Value lost a year 5.0%
Cessna
1963 Cessna U-206 Skywagon skydive
€115,000 ≈ $128,720
Dealer
Cessna
1975 Cessna U206F, Iceland
$159,950
Dealer
U206F specs
Cessna
1964 Cessna U206
$175,000
Dealer
Cessna
1975 Cessna U206F
$190,000
Private seller
U206F specs
Cessna
1975 Cessna Turbo U206F Stationair
€175,000 ≈ $195,878
Dealer
U206F specs
Cessna
1982 Cessna U206G, Iceland
$205,995
Dealer
U206G specs