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CESSNA 206 (turbine)

From SKYbrary Wiki
Name 206 (turbine)
Manufacturer CESSNA
Body Narrow
Wing Fixed Wing
WTC Light
Type code L1T
Engine Turboprop
Engine count Single
Mass group 1

Manufacturered as:

CESSNA 206 (turbine)
SOLOY Turbine 206

CESSNA 206 (turbine)

CESSNA 206 (turbine)


Utility light aircraft. In service since 1972. Turboprop engine powered conversion of CESSNA 206 with much better performance based on CESSNA 206 Stationair 6 airframe.

Technical Data

Wing span 10.92 m35.827 ft
Length 8.62 m28.281 ft
Height 2.92 m9.58 ft
Powerplant 1 x 420 SHP Allison 250-C20S turboprop engine with 3 blade propeller.
Engine model Allison 250

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 142 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance m ROC 988 ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance m
MTOW 16321,632 kg
1.632 tonnes
Ceiling FL157 ROD ft/min APC A
WTC L Range 730730 nm
1,351,960 m
1,351.96 km
4,435,564.308 ft

Accidents & Serious Incidents involving C06T

None on SKYbrary