1981 CESSNA TURBO U206G STATIONAIR
Aircraft Summary
General
Year
1981
Manufacturer
CESSNA
Model
TURBO U206G STATIONAIR
Condition
Used
FlightRules
IFR
Based at
KDWX
Airframe
Total Time
3279
Max Takeoff Weight
3,800 lb
Basic Empty Weight
2,516 lb
STOL
Yes
Fuel Capacity Volume
108 gal
Auxiliary Fuel Tank
Yes
Complete Logs
Yes
Engine
Engine Manufacturer
CONTINENTAL
Engine Model
TSIO520M7B
Engine Serial Number
532107
Engine Horsepower
310 HP
Engine Time
1204.7
Engine Time Since
SNEW
Engine TBO
1600
Year Engine Overhauled or Installed as New
2000
Turbocharged
Yes
Props
Prop Manufacturer
MCCAULEY
Prop Model
D3A34C402-C
Prop Time
844
Number of Blades
3
Blade Composition
Aluminum
Modifications/Conversions
Vortex Generators
Yes
Modifications/Conversions
Gami Injectors
FIint Aero Tip Tanks
Kinsley Exhaust
Horton STOL
Avionics
GPS 1 Manufacturer
GARMIN
GPS 1 Model
GNS530WAAS
GPS 2 Manufacturer
GARMIN
GPS 2 Model
APOLLO GX60
Transponder 1 Manufacturer
GARMIN
Transponder 1 Model
GTX345
Autopilot Manufacturer
S-TEC
Autopilot Model
SYSTEM 60-2
ADS-B Equipped
Yes
WAAS
Yes
LPV
Yes
Yaw Damper
Yes
Active Traffic
Yes
Terrain Warning System
Yes
Engine Monitor
Yes
Avionics/Radios
Garmin GI-275
Additional Equipment
Oxygen System
Yes
Float Kit
Yes
Inspection Status
Inspection Status
Annual Inspection 3/1/2022
Airworthy
Yes
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