1977 Cessna T210M
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
IFRAspen Pro-Max PFD Avidyne IFD540 GPS Garmin GTX 345 Transponder (ADS-B In/Out) Garmin GMA 345 Audio Panel STec 55X Autopilot JPI EDM 900 Primary Engine Monitor
Description
De-Turbo'd Cessna 210 M with all the features you want: CAV TKS Weeping Wing System - Known Ice Capability New Summit Aviation IO-550 Conversion with 6 point mounting system Low time MT 3 Blade Propeller Speed Brakes Excellent Paint and Interior (2019) Excellent Avionics (Aspen Pro-Max, Avidyne IFD 540, STec 55-X, Garmin GTX345....) Complete Logs
Engine
Factory New Continental IO-550 with 6 point "Quiet Ride" mounting system. Low hour 3 Blade Composite MT Propeller
Interior
Paint and Interior done in 2019 and in excellent condition. 6 Seats Oxygen
Exterior
and Interior (2019) Excellent Avionics (Aspen Pro-Max, Avidyne IFD 540, STec 55-X, Garmin GTX345....) Complete Logs
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 |
|---|---|---|---|---|---|---|
|
John Lane
trade-a-plane.com
|
$385,000
|
Columbus, IN | Mar 20, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna T210M
This 1977 Cessna T210M (N210AK) is a 6-seat single engine piston with 7,336 hours on the airframe. There are currently 8 T210M aircraft listed for sale with asking prices ranging from $199,900 to $608,015. This aircraft is priced above the market average at $385,000.
The T210M cruises at 164 kts (304 km/h) with a range of 900 nm (1,667 km) — ideal for short hops and local flights.
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 T210M — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Ownership & Registration
FAA registration data pending for N210AK.
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 N210AK against the NTSB accident database.
Service Difficulty Reports — Cessna T210M
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
THE PILOT REPORTED A LOSS OF MANIFOLD PRESSURE IN FLIGHT ALONG WITH A REDUCTION IN POWER AND CRUISE SPEED. THE AIRCRAFT SAT UNTIL THE 28TH OF MARCH AWAITING MAINTENANCE. UPON INVESTIGATION, THE CYLINDER HEAD WAS FOUND TO HAVE SEPARATED FROM THE CYLIN...
ELECTRICAL SYSTEM FAILURE. FOUND BROKEN RING TERMINAL AT POSITIVE TERMINAL OF ALTERNATOR. FOUND VOLTAGE REGULATOR INOP.
EXTREME CORROSION FOUND ON PARTS INSIDE PROP HUB POST OVERHAUL WITH LESS THAN 40 HOURS FROM OVERHAUL. OPERATOR SUSPECTS UNAPPROVED PARTS MAY HAVE BEEN USED AND REPLACEMENT KIT PARTS NOT REPLACED IAW MANDATORY REPLACEMENT KIT MANUAL PROCEDURES.
LT GEAR DOOR BUCKED IN FLIGHT. SUSPECT GEAR DOOR WAS DAMAGED DUE TO OVERSPEED. NO WORK RECENTLY PERFORMED ON LANDING GEAR. NO EMERGENCY ACTIONS TAKEN. NO APPLICABLE ADS, SBS, STCS OR ICAS. SUGGEST VISUAL INSPECTION OF ADHESIVE ATTACHING STRUCTOR TO D...
NOSE GEAR CAME LOOSE FROM NOSE GEAR FORK. NOSE GEAR BOLT FORK FOUND TO BE MISSING. NO WORK RECENTLY PERFORMED ON NOSE GEAR. NO EMERGENCY MEASURES TAKEN. NO ADS, SBS, STCS OR ICA'S APPLY. BOLT WAS NOT FOUND POST EVENT. SUGGEST PREFLIGHT INSPECTION TO ...
#1 CYLINDER LOW COMPRESSION 59/80 LEAKING THROUGH EXHAUST VALVE. FOUND LIFTERS SHOWING PITTING AND STRESS.
DURING ANNUAL INSPECTION, FOUND MOVEMENT IN THE RT WING SPAR FITTINGS, BETWEEN THE RT WING MAIN SPAR ATTACH BRACKETS AND THE FUSELAGE CARRY-THROUGH SPAR ATTACH BRACKETS.
TWO SPALLED EXHUAST LIFTERS WHICH DAMAGE CAM.
PILOT WROTE-UP "FUEL FLOW METER INOP" DURING INITIAL START-UP. FOUND NO OR VERY LOW FUEL FLOW INDICATION AT IDLE BUT ENGINE RAN NORMAL, FOUND NORMAL FUEL FLOW INDICATION AT MID TO HIGH POWER SETTINGS WITH ENGINE RUNNING NORMALLY. FOUND GAUGE TO BEOPE...
DURING A FINAL APPROACH, PILOT APPLIED THROTTLE TO ARREST HIS SINK RATE BUT THE ENGINE DID NOT RESPOND. POST ACCIDENT INVESTIGATION REVEALED AT LEAST 5 GALLONS WAS AVAILABLE IN EACH WING TANK.
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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