1981 Cessna TU206G
Single Engine Piston
Aircraft Details
Seller reportedDescription
Showroom
Dealerships Piper M700 Fury
Archer
Seminole
Diamond DA62
DA42 VI
DA50 RG
DA20 C1
Daher Kodiak KODIAK 900
KODIAK 100
Tecnam P2006T MKII
Gran Lusso
P-Mentor
Services Parts
Maintenance
Shared Ownership
About About Us
Our Team
Contact
Showroom
Dealerships Piper M700 Fury
Archer
Seminole
Diamond DA62
DA42 VI
DA50 RG
DA20 C1
Daher Kodiak KODIAK 900
KODIAK 100
Tecnam P2006T MKII
Gran Lusso
P-Mentor
Services Parts
Maintenance
Shared Ownership
About About Us
Our Team
Contact
Showroom
Dealerships Piper M700 Fury
Archer
Seminole
Diamond DA62
DA42 VI
DA50 RG
DA20 C1
Daher Kodiak KODIAK 900
KODIAK 100
Tecnam P2006T MKII
Gran Lusso
P-Mentor
Services Parts
Maintenance
Shared Ownership
About About Us
Our Team
Contact
Engine
Notes
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 |
|---|---|---|---|---|---|---|
|
Aviation Unlimited
aviationunlimited.com
|
$199,500
|
— | Apr 03, 2026 | — | Active |
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Cessna TU206G loan calculator
AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna TU206G
This 1981 Cessna TU206G is a 6-seat single engine piston with 10,148 hours on the airframe. There are currently 8 TU206G aircraft listed for sale with asking prices ranging from $199,500 to $308,699. This aircraft is priced below the market average at $199,500.
The TU206G cruises at 142 kts (263 km/h) with a range of 840 nm (1,556 km) — ideal for short hops and local flights. Service ceiling of 15,700 ft allows operation above most weather.
Operating costs: Fuel burn is 14.5 GPH (55 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $80/hr in fuel alone. Total variable cost including maintenance reserves is approximately $175/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $22,000. With 10,148 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. Mechanics have filed 10 service difficulty reports for this type — common maintenance items to discuss during pre-buy.
Pre-Purchase Checklist
Cessna TU206G — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA 206
AeroGurus estimates based on industry averages for the CESSNA 206. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
Registration number not available.
Location & Ownership
Aircraft Location
Location not available
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.
Service Difficulty Reports — Cessna TU206G
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...
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...
(CAN) ENGINE COULD NOT ATTAIN TAKE OFF RPM. PROPELLER WAS REMOVED AND BENCH TESTED. IT WAS FOUND THAT IT WOULD NOT CYCLE INTO FINE PITCH. UPON DISASSEMBLY IT WAS FOUND THAT THE BEARING RACES, RETAINERS AND BALLS WERE SEVERELY CORRODED. PROPELLER WAS ...
ATTACHMENT NUTS SUPPLIED WITH ATTACHMENT KIT (P/N KPL2001) FAILED BEFORE REACHING RECOMMENDED TORQUE (180-220 IN LBS). THE NUTS SEEM VERY SOFT.
DURING AN ANNUAL INSPECTION, AFTER REMOVAL OF THE RT MAIN GEAR TO FUSELAGE FAIRING FOR INSPECTION, FOUND THE GEAR ATTACHMENT OUTBOARD FITTING CRACKED. THE CRACK WAS IN THE WEB OR BODY OF THE PART AND NOT EMANATING FROM AN EDGE. REQUIRED MAGNIFICATION...
DURING ANNUAL INSPECTION, AFTER REMOVAL OF THE RIGHT MAIN GEAR TO FUSELAGE FAIRING, FOUND THE ALUMINUM BRAKE LINE SEVERELY GOUGED AND CHAFED. CHAFING ON THE FUSELAGE SKIN CUTOUT WHERE THE LEAF SPRING-TYPE GEAR PASSED THROUGH. THE BRAKE LINE WALL WA...
ACFT STARTED AND RUNNING FOR A TRAINING FLIGHT, PILOTS NOTICED A VIBRATION OF THE ENGINE AND NO CYLINDER HEAD TEMP OR EXHAUST TEMP ON NR 6 CYLINDER IAW THE ENGINE MONITOR. PILOTS SHUT ENGINE DOWN AND NOTIFIED MAINTENANCE. AFTER INSPECTION OF CYLIND...
DURING LOWER FWD DOOR POST AND STRUT FITTING INSPECTION REQUIRED BY SERVICE BULLETIN SEB935R1, FOUND A CRACK IN RADIUS OF CORNER ADJACENT TO AND DISAPPEARING UNDER THE STRUT FITTING.
SQUEALING SOUND AT ENGINE START VOLTMETER SHOWING DISCHARGE. ALTERNATOR BELT WAS SHEARED.
UPON LANDING, PILOT LOST RT BRAKE PEDAL ACTUATION AS WELL AS RT BRAKE CAPABILITIES. INITIAL GVI-VISUAL INVESTIGATION REVEALED RT BRAKE MASTER CYLINDER PISTON ROD PN 0541143, BROKEN AT BASE BELOW CLEVIS CHECK NUT PN 0541140. UPON DVI-VISUAL INSPECT...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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