1971 Cessna 210K
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
BTHMFD EIS Garmin G5 Standby Instrument Garmin GI-106A Course Deviation Indicator Garmin GMA 340 Audio Panel Garmin GNS 430W NAV/COM/GPS Garmin GNS 430 NAV/COM/GPS Garmin GTX 345 ADS-B In Out Transponder Bendix/King KN-64 DME S-Tec 50 Autopilot
Description
Factory Remanufactured TSIO-520-H fitted Fresh Propeller Overhaul New Garmin Glass Panel New Paint Recent Interior
Engine
Engine Details: Continental TSIO-520-H Fresh Factory Remanufacture Propeller Details: Hartzell HC-G3YF-1RF Fresh Overhaul
Interior
Six-Place Grey Leather Seating with Black Carpet New Plastics Throughout Refurbished in 2023
Exterior
Overall White with Blue and Silver Accents. Refurbished in 2026
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 |
|---|---|---|---|---|---|---|
|
NEXT Aviation
trade-a-plane.com
|
Contact for Price
|
Johannesburg ZAF | Mar 20, 2026 | 119 days | Active |
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Cessna 210K loan calculator
AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 210K
This 1971 Cessna 210K is a 6-seat single engine piston with 3,090 hours on the airframe. There are currently 2 210K aircraft listed for sale with asking prices ranging from $175,000 to $175,000.
The 210K cruises at 171 kts (317 km/h) with a range of 900 nm (1,667 km) — ideal for short hops and local flights. Service ceiling of 17,300 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. With 3,090 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 210K — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA 210 IO-520 (NA)
AeroGurus estimates based on industry averages for the CESSNA 210 IO-520 (NA). Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
Registration number not available.
Location & Ownership
Aircraft Location
Johannesburg ZAF
Seller reportedTitle 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 210K
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
HYDRAULIC PUMP LEAKS 5606 FROM HOUSING PARTING SURFACES DURING OPERATION. TWO HOUSING BOLTS APPEAR TO BE STRIPPED, BROKEN AND HOUSING SEAL IS EXTRUDING PAST PARTING SURFACES AROUND LEAKAGE AREA.
LOCK ACTUATOR BINDING AND WOULD NOT LOCK IN THE DOWN POSITION. GEAR UP LANDING.
THE RETAINING RING DISLODGED FROM THE RETAINING RING GROVE, WHICH ALLOWED THE PISTON AND ROD AND MAIN GEAR ACTUATOR GLAND TO SEPARATE FROM THE MAIN GEAR ACTUATOR CYLINDER PREVENT HYDRAULIC PRESSURE FROM BUILDING WHICH IS NECESSARY TO OPEN THE MAIN.
AT CRUISE 6500 FT, NR 3 PISTON PIN ALUMINUM END PLUG BROKE OFF THE STEEL PIN. THIS CAUSED DAMAGE TO THE PISTON, RINGS, CYLINDER AND ULTIMATELY STOPPED THE ENGINE, SEIZED.
INTERNAL O-RING FAILED AND UPLOCK WOULD NOT RELEASE NOSE GEAR, RESULTING IN GEAR NOT EXTENDING, PROP DAMAGE, SUDDEN ENGINE STOPPAGE, AND LOWER SKIN DAMAGE.
OWNER/PILOT REPORTED THAT AFTER LANDING, FLAPS WOULD NOT RETRACT TO FULL UP NOR DID FLAP INDICATOR INDICATE CORRECT POSITION OF FLAPS. TROUBLESHOOTING REVEALED THAT FLAP FOLLOW UP CABLE OUTER CASING SHATTERED JUST INBD OF ATTACH CLAMP IN ROOF ABOVE...
WHILE UNDERGOING AN ANNUAL INSPECTION THE ENGINE FIREWALL WAS FOUND TO BE CRACKED WHERE THE EXHAUST HANGER BRACKETS ATTACH ON THE LT SIDE. ADDITIONAL CRACKING WAS ALSO FOUND ON THE INNER BULKHEAD.
WHILE UNDERGOING AN ANNUAL INSPECTION THE ENGINE FIREWALL WAS FOUND TO BE CRACKED WHERE THE EXHAUST HANGER BRACKETS ATTACH ON THE LT SIDE. ADDITIONAL CRACKING WAS ALSO FOUND ON THE INNER BULKHEAD.
WHILE UNDERGOING AN ANNUAL INSPECTION THE ENGINE FIREWALL WAS FOUND TO BE CRACKED WHERE THE EXHAUST HANGER BRACKETS ATTACH ON THE LT SIDE. ADDITIONAL CRACKING WAS ALSO FOUND ON THE INNER BULKHEAD.
(CAN) THE BULKHEAD DOUBLER REINFORCES THE HOLE WHERE THE HORIZONTAL STAB ATTCHES. DOUBLER SPLIT IN TWO THROUGH THE ANCHOR NUT RIVIT HOLE. THIS DOUBLER IS ONLY FOUND ON EARLY MODELS.
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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