1973 Cessna T210L
Single Engine Piston
Aircraft Details
Seller reportedDescription
Well-maintained Turbo 210L with just over 6,200 hours on the airframe, an American-overhauled TSIO-520-R engine with 1,040 hours TSO, and a practically new McCauley propeller with only 20.8 hours since overhaul. A solid opportunity in the T210 category — ideal for personal or business operations. Price is negotiable.
Engine
with 1,040 hours TSO, and a practically new McCauley
Propeller
McCauley propeller
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 |
|---|---|---|---|---|---|---|
|
AirplaneIQ
aircraftdealer.com
|
Contact for price
|
FL | Mar 15, 2026 | 1 days | Active | |
|
Listing Source
globalplanesearch.com
|
Call for Price
|
— | Mar 17, 2026 | — | Active | |
|
IQ Worldwide Solutions
aviationtrader.com.au
|
Call for price *
|
Tampa, Florida, Australia | Apr 04, 2026 | — | Active |
* Converted to USD at daily European Central Bank (ECB) exchange rates
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna T210L
This 1973 Cessna T210L (YV2811) is a single engine piston with 6,217 hours on the airframe. There are currently 12 T210L aircraft listed for sale with asking prices ranging from $179,500 to $310,000.
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
Ownership & Registration
FAA registry covers US-registered aircraft (N-numbers).
This aircraft (YV2811) 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 database checked for YV2811.
Note: NTSB covers US-registered aircraft (N-numbers). This aircraft is registered in a non-US country (YV2811). Safety records from the national aviation authority may not be included in our database.
Service Difficulty Reports — Cessna T210L
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
DURING THE 200HR/ANNUAL INSPECTION IT WAS FOUND THAT BOTH CESSNA SK210-175A AND SK210-175B KITS THAT WERE INSTALLED TO COMPLY WITH CESSNA SB SEB07-5R2 WERE FOUND IN AN INOP CONDITION (BROKEN). THE SWIVEL ADAPTER THAT IS HELD ONTO THE REEL ASSEMBLY WI...
N4678Q, C210, DECLARED AN EMERGENCY DUE TO POSSIBLE ELECTRICAL ISSUE. THE FLIGHT LANDED SAFELY WITHOUT ISSUE.
ROD ASSEMBLY BROKE AT THE THREADED END OF THE ROD END.
VOLT METER INDICATED A DISCHARGE AT 1000 RPM. NORMAL VOLT AT 1000RPM AS PER CHECK SHOULD BE 28.5+-5. VOLT METER INDICATED AT 1000 RPM 25.0 AMPS 37. AT 1700 RPM VOLT 27.8 AMPS 42, AT 2000 RPM V27.8 AMPS 39.
DURING 50 HOUR INSPECTION, MECHANIC FOUND THE MIXTURE CONTROL OPERATION TO BE VERY STIFF. FOUND THE MIXTURE CONTROL UNIT ON ENGINE SEIZED AND VERY HARD TO MOVE BY HAND, REPLACED.
ENROUTE, MANIFOLD PRESSURE DROPPED TO 24". INDUCTION TUBE FROM COMPRESSOR TO THROTTLEBODY FAILED WITH A 2" TO 3" HOLE ONLEFT SIDE BLEW OUT.
FIRST GROUND RUN REVEALED A LEAKING OIL PRESSURE TO WASTGATE HOSE OR FITTING. REPLACED FITTING IN ENGINE WITH NEW STEEL FITTING. SECOND GROUND RUN, OIL LEAKED FROM HOSE AGAIN. AFTER SLIGHT ADDITIONAL TORQUE APPLIED AND THIRD GROUND RUN, THE HOSE WA...
PILOT REPORTED NO GEAR DOWN INDICATION UPON LOWERING THE LANDING GEAR HANDLE. IFE WAS DECLARED, GEAR WAS VISUALLY CONFIRMED DOWN BY GROUND CREW AND ACFT LANDED UNEVENTFULLY. IT WAS DISCOVERED THAT THE JAMB NUT THAT SECURES THE DOWN LOCK SWITCH HAD L...
6 NEW CYLINDERS WERE INSTALLED AUG 10, 2008 AT 2812 TOTAL TIME. THE CYLINDERS EXPERIENCED A FAILURE OF THE VALVE GUIDES ON 3 OF THE 6 AT 384 HOURS TIME IN SERVICE. ALL 3 FAILED VALVE GUIDES BROKE OFF AT THE INSERT POINT AND 1 COMPLETELY DISINTEGRATED...
DURING CLIMB TO CRUISE ENGINE MADE A LOUD NOISE AND QUIT RUNNING, ENGINE REMAINED WINDMILLING TO LANDING. VISUAL INSP REVEALED NR 3 CYLINDER ROD BOLT MISSING, ROD CAP EXITED ENG THRU UPPER CASE, NO EVIDENCE OF OIL STARVATION.
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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