C06T
CESSNA 206 (turbine)
CESSNA 206 (turbine)
Aircraft
Name
206 (turbine)
Manufacturer
Body
Narrow
Wing
Fixed Wing
WTC
L
APC
A
Type Code
L1T
Engine
Turboprop
Engine Count
Single
Manufactured as
SOLOY Turbine 206
CESSNA 206 (turbine)
C06T
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 (metric)
10.92 m
Length (metric)
8.62 m
Height (metric)
2.92 m
Powerplant
1 x 420 SHP Allison 250-C20S turboprop engine with 3 blade propeller.
Engine Model(s)
Allison 250
Indicative Performance Data
Take-Off
V2
n/a
Distance
n/a
MTOW
1632 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
988 ft/min
Initial Climb (to FL150)
IAS
n/a
ROC
n/a
Initial Climb (to FL240)
IAS
n/a
ROC
n/a
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
142 kts
MACH
n/a
Ceiling
157
Range
730 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
n/a
ROD
n/a
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
n/a
Distance
n/a
