1976 Cessna U206F
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
Description
19/6 Cessna U206F TTAF: 16,705.1 hrs Engine Continental IO-520-F S/N 835220-R Time since overhaul: 1779.2 hours (06/24/2019) Propeller Hartzell HC-C3YF-1RF S/N PY437B Time since overhaul: 1,027.9 hours (06/04/2019) Avionics: Garmin GMA340 Audio Panel Garmin SL-40 Comm (x2) Garmin GTX327 Transponder Garmin Aera 500 GPS STC's: Selkirk Interior (SA1007SE) Concorde Battery (SA01118WI) Rosen Sunvisors (SA00871SE) McFarlane Flap Rollers (SA01074WI) VHF FM Radio (SA97-129) Hartzell Propeller (SA685AL) Brackett Air Filter (SA71GL) Split Forward Cargo Door Window (SA20-34) Aircraft is subject to verification of specifications, logs, times, damage and all equipment listed.
Engine
Overhaul Done: 06/24/2019
Propeller
Overhaul Done: 06/04/2019
Inspection
Annual Completed June 9, 20206
Description and equipment details provided by the seller. AeroGurus does not verify seller-provided information.
Price Comparison
| Source | Price | Location | Listed | Days on Market | Status | Action |
|---|---|---|---|---|---|---|
|
Josh Fehr
controller.com
|
$225,000
|
La Crete, Alberta, Canada | Jul 26, 2026 | 0 days | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna U206F
This 1976 Cessna U206F (C-GICJ) is a 5-seat single engine piston with 16,705 hours on the airframe. There are currently 6 U206F aircraft listed for sale with asking prices ranging from $159,950 to $475,000.
The U206F cruises at 142 kts (263 km/h) with a range of 760 nm (1,408 km) — ideal for short hops and local flights. Service ceiling of 16,900 ft allows operation above most weather.
Operating costs: Fuel burn is 16 GPH (61 L/h), which at current 100LL avgas prices (~$6.20/gal) means approximately $99/hr in fuel alone. Total variable cost including maintenance reserves is approximately $160/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $22,000. With 16,705 hours on the airframe, this aircraft has exceeded TBO (1,700 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 U206F — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA U206F
AeroGurus estimates based on industry averages for the CESSNA U206F. 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-GICJ) 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-GICJ against the NTSB accident database.
Service Difficulty Reports — Cessna U206F
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
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...
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.
PILOT REPORTED LOW OIL PRESSURE AT IDLE, REMOVED OIL PRESSURE REGULATOR AND FOUND SHARP METAL CHIP IN BOTTOM OF REGULATOR WHERE IT HAD ARRIVED AFTER FALLING OUT OF REGULATOR SEAT. PREVIOUS EXPERIENCE LED US TO BELIEVE THAT THE METAL WAS FROM A LIFTE...
FOUND EXCESSIVE AMOUNT OF FERROUS METAL IN OIL FILTER DURING NORMAL MAINTENANCE. UPON INSPECTION FOUND 5/6 CAM LOB SPALLED. THIS IS THE SECOND WORN CAM IN THIS ENGINE IN THREE YEARS.
(CAN) DEFECT: PROP FAILED TO TURN ON START. RECTIFICATION: STARTER ADAPTER ASSEMBLY REMOVED AND REPLACED WITH OVERHAULED ASSEMBLY AND GASKET AS PER TCM MM X30039 SECT 4-21 AND SECT 7-8. AIRCRAFT GROUND RUN, FUNCTION AND LEAK CHECK FOUND SERVICEABLE. ...
(CAN) FAILED DURING FLIGHT, BATTERY RUN DOWN AS A RESULT. (TC# 20180907015)
LOW COMPRESSION DURING A 100 HOUR INSPECTION, IN ONE CYLINDER (20/80) WAS OBSERVED. BORESCOPE INSPECTION SHOWED AN INTAKE VALVE THAT HAD LOST PART OF THE LIP THAT SEALS AGAINST THE VALVE SEAT.
DURING AN ENGINE REPAIR, ONE ROCKER ARM WAS FOUND TO HAVE SEVERELY WORN AREA WHERE THE ROCKER ARM PUSHES ON THE VALVE STEM.
SHORTLY AFTER START, THE ENGINE STOPPED DURING GROUND OPERATION. ENGINE SEEMS TO BE SEIZED, HOWEVER FURTHER EVALUATION IS NEEDED TO ASCERTAIN CAUSE. THERE WAS NO INDICATION OF ANY PROBLEMS PRIOR TO THIS. WILL SUBMIT A FOLLOW UP REPORT AFTER TEARDO...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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