1971 Cessna T210K
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
Description
Airframe
Total Time Since New: 2950
Engine
Type: Continental TSIO-520-H
TBO: 1400
Time Since Overhaul: 730
Time Remaining: 670
Propeller
Type: Hartzell PHC-J3YF-IRF
TBO: 2400 Hrs / 6 Years
Time Since New: 411
Next Overhaul Due: November 2025
Hours Remaining: 1989
Avionics
Garmin GMA 340 AUDIO PANEL
Garmin GNS 430 COMM/NAV/GPS
Bendix King KX 125 COMM/NAV
Bendix King KN 64 DME
Bendix King KR 87 ADF
Bendix King KT 76A TRANSPONDER
JPI EDM 700 ENGINE MONITOR
S-TEC 50 AUTOPILOT
Artex Integra A F 406MHz ELT
Interior
New Light Grey Leather with Dark Complementing Carpets
Exterior
New Overall White & Red with Silver Accents
Engine
Type: Continental TSIO-520-H TBO: 1400 Time Since Overhaul: 730 Time Remaining: 670 Propeller Type: Hartzell PHC-J3YF-IRF TBO: 2400 Hrs / 6 Years Time Since New: 411 Next Overhaul Due: November 2025 Hours Remaining: 1989 Avionics Garmin GMA 340 AUDIO PANEL Garmin GNS 430 COMM/NAV/GPS Bendix King KX 125 COMM/NAV Bendix King KN 64 DME Bendix King KR 87 ADF Bendix King KT 76A TRANSPONDER JPI EDM 700 ENGINE MONITOR S-TEC 50 AUTOPILOT Artex Integra A F 406MHz ELT Interior New Light Grey Leather with Dark Complementing Carpets Exterior New Overall White & Red with Silver Accents
Interior
New Light Grey Leather with Dark Complementing Carpets Exterior New Overall White & Red with Silver Accents
Exterior
New Overall White & Red with Silver Accents
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 |
|---|---|---|---|---|---|---|
|
Stephen Campbell
avpay.aero
|
Contact for Price
|
— | Apr 05, 2026 | — | Active |
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Cessna T210K loan calculator
AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna T210K
This 1971 Cessna T210K is a 6-seat single engine piston with 2,950 hours on the airframe. There are currently 2 T210K aircraft listed for sale with asking prices ranging from $180,000 to $180,000.
The T210K cruises at 164 kts (304 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 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 2,950 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 8 service difficulty reports for this type — common maintenance items to discuss during pre-buy.
Pre-Purchase Checklist
Cessna T210K — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA 210
AeroGurus estimates based on industry averages for the CESSNA 210. 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 T210K
SDRs are reports filed by mechanics about problems found during maintenance. 8 recent reports for this aircraft type.
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...
(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.
FOUND (BRACKETT) AIR FILTER ASSEMBLY (NR-BA-2405) INSTALLED BACKWARDS. THE MESH SAFTEY SCREEN WAS AT THE FRONT OF THE FOAM FILTER, AND THE INLET GRID WAS INSTALLED AT THE BACK OF THE ASSEMBLY. INSPECTED ONE OTHER FILTER ASSEMBLY ON LIKE AIRCRAFT A...
(CAN) UPPER NOSE GEAR TORQUE LINK FOUND CRACKED AS SHOWN. CRACK WAS IN TWO LOCATIONS ABOUT 1/8 INCH LONG. PART HAD NOT FAILED.THIS IS THE SECOND PART FOUND CRACKED ON CESSNA 210 AIRCRAFT, BOTH IN THE SAME LOCATION.
AFTER TAKEOFF, LANDING GEAR FAILED TO RETRACT OR EXTEND. AN EMERGENCY LANDING WAS PERFORMED WITH GEAR IN THE INTERMEDIATE POSITION. POST-FLIGHT INSPECTION REVEALED THE ACTUATOR HAD RUPTURED AT THE FORGING SEAM FROM FORE TO AFT. NEW ACTUATOR WAS IN...
THE PROPELLER HUB WAS FOUND CRACKED AT 5 OF THE 6 MOUNTING STUDS. THE PROPELLER HAD ACCUMULATED APPROXIMATELY 40 HOURS OF OPERATING TIME SINCE THE LAST OVERHAUL PERFORMED ON 1-10-96. THE CRACKS WERE DISCOVERED BY AN IA WHILE PERFORMING THE ANNUAL I...
DURING 100 HOUR INSPECTION, FOUND PROP HUB CRACKED AT 5 OF THE 6 MOUNTING STUDS.
DURING ANNUAL INSPECTION, FOUND ELEVATOR 'UP' CABLE WORN THROUGH AT PULLEY JUST FORWARD OF GEARBOX. PULLEY WAS NOT TURNING DUE TO BRACKET THAT HOLDS PULLEY WAS INSTALLED AT AN ANGLE. IT APPEARS BRACKET WAS INSTALLED THAT WAY FROM FACTORY. LOG BOOK...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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