1978 Cessna U206
Single Engine Piston
Equipment & Features
- Seats
- 6
Aircraft Details
Seller reportedAvionics & Equipment
BTHPS Engineering PMA 8000C w/ Bluetooth Audio Panel Garmin GTN 650 Nav/Com 1 Garmin SL 30 Nav/Com 2 Garmin GFC Auto Pilot w/Esp. Garmin G500 MFD/PFD Garmin G5 Back-Up Garmin 106B/CAI Electronics Interface MVP 50 Engine Monitor Dual Charging Ports Flight Stream
Description
Avionics / Equipment PS Engineering PMA 8000C w/ Bluetooth Audio Panel Garmin GTN 650 Nav/Com 1 Garmin SL 30 Nav/Com 2 Garmin GFC Auto Pilot w/Esp. Garmin G500 MFD/PFD Garmin G5 Back-Up Garmin 106B/CAI Electronics Interface MVP 50 Engine Monitor Dual Charging Ports Flight Stream
Engine
Continental IO-520 F SIN: 82163TR
Interior
Redone in October 2025 Like New Sheep Skin Pilot and Copilot Seats Blue
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 |
|---|---|---|---|---|---|---|
|
Listing Source
trade-a-plane.com
|
$315,000
|
Fort Myers, FL | May 05, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna U206
This 1978 Cessna U206 (N7360C) is a single engine piston with 6,010 hours on the airframe. This aircraft is listed at the market average at $315,000.
NTSB records show 0 incidents for this airframe — a clean safety record. There are 4 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
Ownership & Registration
FAA registration data pending for N7360C.
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 safety data coming soon.
We'll check N7360C against the NTSB accident database.
Airworthiness Directives — Cessna U206
ADs are mandatory safety instructions issued by the FAA. 4 recent ADs found for this aircraft type.
Cessna Aircraft Company 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 206, P206, U206, TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 Series Airplanes
View full AD →Cessna Aircraft Company 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 206, P206, U206, TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 Series Airplanes
View full AD →Cessna Aircraft Company 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 206, P206, U206, TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 Series Airplanes
View full AD →Cessna Aircraft Company P206, TP206, TU206, U206, 207, T207, 210, P210, and T210 Series Airplanes
View full AD →Source: FAA Airworthiness Directives database. Showing most recent ADs for this aircraft type.
Service Difficulty Reports — Cessna U206
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
DURING FLIGHT, PILOT REPORTED FUEL FLOW DISCREPANCY AND ENGINE ROUGHNESS AND RETUNRED TO BASE FOR A PRECAUTIONARY, ALBEIT IF VERY STRESSFUL, LANDING. UPON INSPECTION OF THE FUEL FLOW SENSOR ( PART OF THE JPI 930 ENGINE INSTRUMENTAION - STC SA01435SA...
SUSPECT VOLTAGE REGULATOR FAILED, AND ALTERNATOR PUT OUT EXCESSIVE VOLTAGE, WHICH THEN BURNT OUT THE 60-AMP CIRCUIT BREAKER INTERNALLY AND WAS THE SOURCE OF SMOKE IN CABIN. RECOMMEND LIFE LIMIT ON ALTERNATOR OUTPUT CIRCUIT BREAKER.
FOUND FACTORY DEFECT WHILE PERFORMING FIRST 500-HOUR INSPECTION MAGNETO WITH TT 477.6 IN ACCORDANCE WITH SERVICE SUPPORT MANUAL X42001. COIL TAB HAD NOT BEEN INSTALLED PARALLEL WITH HOUSING TO COVER MATING SURFACE, AS SPECIFIED IN 6-2.4 5.C. THIS H...
BETWEEN 24 & 49 HRS OIL CONSUMPTION WAS 8.7 HRS/QT. OIL CONSUMPTION WAS LOWEST AT 10 HRS PER QUART AT 240 HRS AND THEN INCREASED. AT 370 HRS IT WAS 6 HRS/QT. AT 513 HOURS WAS 4.4 HRS/QT. AT 567 HRS (100HR INSP) IT WAS 2.1 HRS/QT OVER 50 HOURS BUT WAS...
PILOT NOTICE LOSS OF POWER IN CRUISE FLIGHT, RETURNING TO AIRPORT DEBRIS AND SMOKE WAS NOTED EXITING THE ENGINE COWL. OFF AIRPORT LANDING WITHOUT INCIDENT. FOUND HOLE IN CRANKCASE INBOARD OF #4 CYLINDER. #4 CONNECTING ROD, PISTON PIN, AND OTHER PIECE...
0.0 TSMO OVH MAG INSTALLED ON 0.0 TSMO IO550F AT ENG CHANGE. TEST FLIGHTS AND GROUND RUNS ALL OK. 28.7 HOURS LATER MAG WAS REMOVED FOR MAJOR ROUGHNESS, INABILITY TO IDLE, AND MULTIPLE CYLINDERS WITH ERRANT TEMPERATURES. POINT CONTACTOR PAD IN STAMPE...
THE FRAME OF THIS PLANE IS SEVERELY CORRODED. THERE IS VISUAL DAMAGE TO MULTIPLE SURFACES INCLUDING THE SKIN AND THE SPARS. IT ALSO HAS MULTIPLE CABLES THAT ARE SEVERELY CORRODED. AN A&P DEEMED IT “AIRWORTHY” BUT NONE OF THESE ISSUES HAVE BEEN REMEDI...
PILOT WAS TAXIING AIRCRAFT WHEN ANOTHER PERSON ON THE RAMP GRABBED HIS ATTENTION REGARDING THE LH MAIN TIRE BEING FLAT. HE STOPPED AND SHUT DOWN. WHEEL WAS REMOVED AND DISASSEMBLED. TIRE INNER TUBE WAS REPLACED AND WHEEL REINSTALLED. EXAMINATION ...
ROCKER ARM FAILED CAUSING ENGINE ROUGHNESS.
125 HRS AFTER MAJOR REPAIR BY RAM AIRCRAFT FRONT TWO THROUGH BOLTS FOUND BELOW MINIMUM TORQUE AND LEAKING OIL.
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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