2011 Cessna T206H
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
IFRDescription
Reasons to buy this turn-key 2011 Cessna Turbo 206H Stationair: • Garmin G1000 w/ GTX345R (ADS-B In and Out), SVT, WAAS/LPV, and CO Guardian • WX-500 Stormscope, Wheel Fairings, Built-in Oxygen, and 4-Place AMSAFE Inflatable Restraint System • Strong 2025 Compressions: 78 / 77 / 72 / 76 / 78 / 72 • Recent Annual – 9/2025 at El Paso Aero, a Cessna Authorized Service Center Asking $550,000.
Interior
6 passenger interior. Seats finished in tan leather with black inserts. Tan vinyl trim and black carpet.
Exterior
Overall white with blue and black accent stripes.
Modifications / STCs
• 4-Place AMSAFE Inflatable Restraint System
• Built-in Oxygen
• CO Guardian
• Wheel Fairings
Description and equipment details provided by the seller. AeroGurus does not verify seller-provided information.
Price Comparison 1 active offer
| Source | Price | Location | Listed | Days on Market | Status | Action |
|---|---|---|---|---|---|---|
|
AeroSolutions
controller.com
|
$550,000
|
Santa Teresa, NM | Apr 19, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna T206H
This 2011 Cessna T206H is a 6-seat single engine piston with 1,525 hours on the airframe. There are currently 74 T206H aircraft listed for sale with asking prices ranging from $160,294 to $1,150,000. This aircraft is priced below the market average at $550,000.
The T206H cruises at 148 kts (274 km/h) with a range of 800 nm (1,482 km) — ideal for short hops and local flights.
Operating costs: Fuel burn is 16 GPH (61 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $88/hr in fuel alone. Total variable cost including maintenance reserves is approximately $185/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $22,000. With 1,525 hours on the airframe, this aircraft has exceeded TBO (1,500 hrs) — verify engine status and overhaul reserve.
NTSB records show 0 incidents for this airframe — a clean safety record. There are 7 airworthiness directives applicable to this aircraft type — review AD compliance carefully before purchase. Mechanics have filed 10 service difficulty reports for this type — common maintenance items to discuss during pre-buy.
Pre-Purchase Checklist
Cessna T206H — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA T206H
AeroGurus estimates based on industry averages for the CESSNA T206H. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
Registration number not available.
Location & Ownership
Title Status
No FAA title records
Available for US-registered aircraft only
Source: FAA Aircraft Registry, FAA Civil Aviation Registry (DocIndex). Title data may be delayed. Always verify with an aviation attorney before purchase.
Safety Record
NTSB database checked for this aircraft.
Airworthiness Directives — Cessna T206H
ADs are mandatory safety instructions issued by the FAA. 7 recent ADs found for this aircraft type.
Cessna Aircraft Company Models 172R, 172S, 182T, T182T, 206H, and T206H Airplanes
View full AD →Cessna Aircraft Company Models 172R, 172S, 182S, 182T, T182T, 206H, and T206H Airplanes
View full AD →The Cessna Aircraft Company Models 172R, 172S, 182T, T182T, 206H, and T206H Airplanes
View full AD →Cessna Aircraft Company Models 172R, 172S, 182T, T182T, 206H, and T206H Airplanes
View full AD →Cessna Aircraft Company Models 172R, 172S, 182S, 206H, and T206H Airplanes
View full AD →Source: FAA Airworthiness Directives database. Showing most recent ADs for this aircraft type.
Service Difficulty Reports — Cessna T206H
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
WHILE CHECKING ELEVATOR TRIM CABLE TENSIONS, FOUND TENSIONS LOW. AFTER SETTING CORRECT TENSIONS, FOUND ELEVATOR TRIM TAB ACTUATOR SHAFT BROKEN AT CHAIN SPROCKETS.
ENGINE WAS RECEIVED BY EJ1R FOR SUDDEN STOPPAGE INSPECTION RESULTING FROM PRECAUTIONARY OFF FIELD LANDING DUE TO BROKEN EXHAUST VALVE ON CYLINDER #5. DURING SUDDEN STOPPAGE TEARDOWN INSPECTION WHILE CLEANING AND VISUALLY INSPECTING CONNECTING RODS, #...
MAGNETO FAILED
PILOT REPORTED MANIFOLD PRESSURE SPIKE AND ENGINE SURGE. FOUND A LOOSE EXHAUST V-BAND COUPLING AND MISSING THE V-BAND COUPLING GASKET. FOUND THE MISSING GASKET LODGED IN THE TURBOCHARGER AND DESTROYED THE TURBINE BLADES. PLEASE CONTACT ME FOR PICTUR...
DURING INSTALLATION OF OPTIONAL EQUIPMENT, A VISUAL INSPECTION WAS PERFORMED OF THE MAIN LANDING GEAR ATTACHMENT POINTS. IT WAS NOTICED THAT THE LEFT MAIN GEAR END ATTACH POINT BOLT AND NOT WERE NOT TIGHTENED. THE LOCK NUT WAS NOT RUN DOWN ALL THE WA...
DC ALTERNATOR FAILED DURING GROUND RUN. UPON REMOVAL FOUND THE ALTERNATOR TO HAVE SEIZED. ALTERNATOR WAS SENT TO HARTZELL WITH AN RMA # 13301. PRODUCT WAS REPLACED WITH A NEW ALTERNATOR. NO REPORT WAS PROVIDED TO US ON WHY THE UNIT FAILED, ALTHOUG...
DURING ANNUAL INSPECTION, ON THE PILOT'S DOOR FOUND SEVERE WEAR ON THE HARDWARE FOR THE ARM, CABIN DOOR STOP. THESE ARE COVERED BY INTERIOR TRIM. THE 8/32 MS27039-0816 SCREW AND 2 EA. 1411206-1 SPACERS ATTACHED TO THE ARM WERE WORN ALMOST ALL THE WAY...
WHILE PERFORMING AD 2015-19-07 WE CAME ACROSS 3 INJECTOR LINES THAT WERE GOUGED BY THE HOSE CLAMPS ON THE ADJACENT MANIFOLD LINES. ALL THREE ARE BEING REPLACED PER THE AD INSTRUCTIONS AND PICTURES WILL BE SENT IN TO SUPPLEMENT THIS REPORT. THE CLAM...
DURING A 50 HOUR ENGINE INSPECTION THE TECHNICIAN DISCOVERED A CRACK IN THE #5 CYLINDER EXHAUST TO CYLINDER RISER
DURING ANNUAL INSPECTION WHILE INSPECTING UNDER COCKPIT FLOOR, MECHANIC SAW BLUE FUEL STAINS IN AREA OF RH FUEL HEADER TANK. UPON REMOVAL TO INSPECT, FOUND WELDED SEAM LEAK ON FWD MIDDLE LOWER PORTION NEAR FUEL OUTLET. REMOVED AND REPLACED FUEL HEADE...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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