1966 Cessna TU206A
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
IFRAvionics: PMA 8000C Audio Panel Icom A200 Com Icom FM Com NAT AA85 Intercom Garmin 327 Transponder Garmin 295 GPS Artex 406 elt Clock Equipment: Float Kit Aero Fabricators Inc Shoulder harness and seat belt assy STC SA1515GL Brackett Air Filter STC SA71GL Ellis and Associates CADD Lower right nose cowl exhaust system access STC SA00861LA Hartzell Propeller HC-C3YF-1RF and Spinner STC SA685AL Micro AeroDynamics STC SA00887SE McFarlane Aviation Inc Flap Roller Kit STC SA01074WI J.P Instruments Fuel Flow System STC SA00861SE Knisley Welding Inc STC SA5009NM I SA5010NM Navigator Inc Removable Nose gear panel STC SA00443WI Para-Nautics LLC Roll up Jump Door STC SA1591NM Rosen Sun Visors STC 5A008715E Selkirk Aviation Interior STC SA01007SE Visual Instruments Flap Position Indicator STC SA00819SE Robinson STOL Kit STC SA1513WE Wipaire Inc Wing Tip Extensions SA SA914NE
Description
1966 Cessna TU206A Jump Plane - 7957TT, Garmin 327 Transponder, PMA 8000C Audio Panel, Garmin 295 GPS. Jump Door Installed, 500 hr Mag Inspections done, 10 year hose replacements done, Turbo recently O/H, New Cylinders 3,5,6 Aug 8/25. Rear Doors and 6 Seats Included. Well maintained airplane with SIDS inspection. Commercial Canadian Registered.
Engine
Engine Time: 775 (Installed 7-12-2012) Prop Total Time: 45 (Hartzell HC-C3YF-1RF, due 5-1-2035)
Interior
Presently setup for skydiving. Has 5 passengers seats Selkirt Interior Rated – “7”
Exterior
White with Blue/Gray Trim Rated – “7”
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 |
|---|---|---|---|---|---|---|
|
Island Aero Services
trade-a-plane.com
|
$230,000
|
Sidney, BC, Canada | Mar 30, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna TU206A
This 1966 Cessna TU206A (C-FUGQ) is a 6-seat single engine piston with 7,957 hours on the airframe. This aircraft is listed at the market average at $230,000.
The TU206A 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 7,957 hours on the airframe, this aircraft has exceeded TBO (2,000 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 TU206A — 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
FAA registry covers US-registered aircraft (N-numbers).
This aircraft (C-FUGQ) is registered outside the US.
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 C-FUGQ against the NTSB accident database.
Service Difficulty Reports — Cessna TU206A
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
(CAN) STICKY EXHAUST VALVE
BENT COMPRESSOR BLADES, POSSIBLE FOD.
(CAN) CRACK IN REAR BULKHEAD PIN DURING MANDATORY NDT INSPECTION OF THE ARGA. (TC NR 20071227004)
(CAN) ERRATIC MANIFOLD PRESSURE DUE TO CONTROLLER FAILURE TO REGULATE OIL PRESSURE FROM WASTEGATE (TC NR 20061117002)
DURING AVIONICS RETROFIT, CORROSION NOTICED IN THE HORIZONTAL STABILIZER. FURTHER INSPECTION FOUND 85 PERCENT OF THE RUDDER ASSY WITH MAJOR CORROSION AND CABIN ROOF AREA AND MAIN WING SPAR ATTACHMENT POINTS. THIS AIRCRAFT SPENT MOST OF ITS LIFE IN F...
LINE SHOWS SIGNS OF INTERGRANULAR CORROSION. OIL LINE IN COCKPIT BEHIND INSTRUMENT PANEL SUPPLYING OIL PRESSURE GAUGE RUPTURED CAUSING APPROXIMATELY 3 QUARTS OF OIL TO ENTER CABIN PRIOR TO AIRCRAFT LANDING. REPLACED LINE ASSEMBLY, NO LEAKS NOTED. ...
INSPECTION FOUND AILERON LOWER FORWARD HINGE BRACKET CRACKED.
INSPECTION FOUND AILERON HINGE BRACKET CRACKED IN LOWER FORWARD BEND RADIUS.
INSPECTION FOUND AILERON HINGE BRACKET CRACKED IN LOWER FORWARD BEND RADIUS.
INSPECTION FOUND AILERON HINGE BRACKET CRACKED IN LOWER FORWARD BEND RADIUS.
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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