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Cessna U206D

AircraftCessna205 / 206 / 207 › U206D

The Cessna U206D Super Skywagon / Stationair is a model in the 205 / 206 / 207 family. It is described here as a Six-seat high-wing piston single. FAA type-certificate reference: A4CE.

Cessna U206D specifications

ManufacturerCessna
ModelU206D
Production years1969
Aircraft typeSix-seat high-wing piston single
Seats6
Landing gearFixed tricycle
CertificationFAA A4CE

Cessna U206D weights and capacities

Maximum takeoff weight3,600 lb
Standard fuel capacity65 gal total / 63 gal usable

FAA A4CE refers to the approved weight-and-balance data for baggage/cargo loading.

Cessna U206D engine and configuration

EngineContinental · IO-520-F · 300 hp

Baggage and loading applicability

BaggageFAA A4CE refers to the approved weight-and-balance data for baggage/cargo loading.

Cessna U206D history and development

The cataloged production period is 1969.

Cessna U206D Super Skywagon / Stationair is part of the Cessna 206 / Stationair type family certificated under FAA A4CE. The represented landplane configuration uses the IO-520-F rated at 300 hp and a 3,600 lb maximum takeoff weight. The standard fuel configuration represented here provides 63 U.S. gallons usable from 65 gallons total. The 206 family spans Super Skylane, Super Skywagon, Stationair and turbocharged derivatives, so model suffix, serial number, engine and fuel-system applicability must be kept distinct.

Cessna U206D fuel capacity

Standard total fuel: 65 U.S. gallons. Standard usable fuel: 63 U.S. gallons. The 65/63-gallon standard system is represented here; A4CE also contains approved long-range fuel configurations.

Cessna U206D model applicability and configuration

FAA A4CE contains model-, serial-number-, float/skiplane-, fuel-system- and equipment-specific branches. Use the aircraft data plate, serial number, applicable POH/AFM, equipment list and current weight-and-balance record before applying these model-level figures. The IO-520-F takeoff rating is 300 hp; maximum continuous rating is lower in the applicable TCDS operating limits.

Cessna U206D weight and balance

Maximum takeoff weight: 3,600 lb. FAA A4CE refers to the approved weight-and-balance data for baggage/cargo loading. The represented landplane maximum takeoff weight is 3,600 lb. Floatplane, amphibian or skiplane limits can differ where approved. Operational loading must use the individual aircraft's approved station arms, baggage/cargo limits and CG envelope. Use the approved aircraft-specific documentation and current weight-and-balance record for operational calculations. WBcalc does not currently provide a model-specific Cessna U206D Super Skywagon / Stationair calculator.

Always verify aircraft applicability. Check the current POH or AFM, equipment list and weight and balance records for the individual aircraft.

Cessna U206D frequently asked questions

What engine does the Cessna U206D Super Skywagon / Stationair use?

The engine listed for this model is Continental IO-520-F.

What is the maximum takeoff weight of the Cessna U206D Super Skywagon / Stationair?

The represented maximum takeoff weight is 3,600 lb.

How much usable fuel does the Cessna U206D Super Skywagon / Stationair carry?

The represented standard usable fuel capacity is 63 U.S. gallons.

Reference sources

FAA: Type Certificate Data Sheet A4CE, Revision 51 - Textron Aviation / Cessna 206 series

Related 205 / 206 / 207 models

← All Cessna 205 / 206 / 207 models
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