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CESSNA 205 Super Skywagon

From SKYbrary Wiki

Name 205 Super Skywagon
Manufacturer CESSNA
Body Narrow
Wing Fixed Wing
WTC Light
Type code L1P
Engine Piston
Engine count Single
Mass group 1

Manufacturered as:


CESSNA 205 Super Skywagon

CESSNA 205 Super Skywagon


The Cessna 205 was introduced late in 1962 as a 1963 model year. The six-seat aircraft was essentially a Cessna 210 with fixed landing gear and with changes to the crew and passenger door arrangement and was officially designated by Cessna as a "Model 210-5".

Technical Data

Wing span 10.92 m35.827 ft <br />
Length 8.62 m28.281 ft <br />
Height 2.92 m9.58 ft <br />
Powerplant 1 x Continental IO-470-S of 260 hp (194 kW).
Engine model Continental O-470

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
(to FL100)
Descent (FL100
& below)
V2 (IAS) kts IAS kts IAS kts IAS kts MACH TAS 160 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance 400 m ROC ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance m
MTOW 15001,500 kg <br />1.5 tonnes <br /> kg Ceiling FL160 ROD ft/min APC A
WTC L Range 880880 nm <br />1,629,760 m <br />1,629.76 km <br />5,346,981.631 ft <br /> NM

Accidents & Serious Incidents involving C205

None on SKYbrary