1968 Cessna 210
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
IFRGarmin GNX375 WAAS GPS/ADS-B Transponder installed with Garmin GI106B CDI in 2019 Avionics package also includes: STEC System 50 Autopilot with altitude hold STEC electric trim Garmin 300XL GPS/COM King KX165 NAV/COM King KA134 audio panel King KN64 DME King KI525a HSI Precise flight standby vacuum system New FAR91.411 91.413 certification will be completed before sale.
Description
Low time, well maintained and regularly flown turbo 210H. Only 100hrs on factory NEW TSIO-520 (installed Oct 2024). Equipped with very capable IFR panel that includes Garmin, STEC and JPI equipment. Vortex generators for stunning short field performance. New interior for comfortable long distance travel along with legendary 210 speed and load hauling capability. This highly versatile airplane, with its fresh engine is ready for years of high performance service.
Engine
BRAND NEW 285hp TSIO520C3B engine (built June 2024) installed Sept 2024 with just over 100hrs since. The engine bay is a clean, powerful, tightly packed work of art. NEW full exhaust system from Plane-Exhaust Three blade McCauley propeller. Overhauled in 2014 at Byam Propeller Service, Inc. Ft. Worth TX with ~600hrs since.
Propeller
Rugged 210H airframe with low total time, logbooks from new and no damage history. Recent updates and servicing include: - Installation in 2026 of Micro-Vortex Generators that significantly improve low speed handling and make this high performance aircraft as comfortable to operate on short grass strips as large regional airports. - Right fuel tank resealed in 2026. - New main gear tires in 2025 - Overhauled hydraulic power pack 2024 - Upgraded nav lights and strobes to LEDs 2021 - Carry-thru spar inspection to SEL-57-06 (AD2020-03-16) completed Nov 2019. Some notable STC's installed are : Monarch fuel caps for far superior water ingress protection on the 90gal (total) fuel tanks Veftronics voltage regulator Wing mounted gear down inspection mirror Bracket air filter Riley International turbo intercooler.
Interior
Blue, white and black paint in clean modern scheme. Excellent condition with great ramp appeal. Fresh, comfortable and SPACIOUS interior with grey leather and tinted windows. - All new Airtex interior (seats, side panels, carpet, headliner) and Plane Plastics trim installed 2018 - Seatbelts re-webbed, 2018. - New custom instrument panels installed 2001 - Aircraft stripped and repainted by Flying Colors Inc, Colorado, 1991. - Aircraft ha always been hangar kept but a Bruce's custom cockpit cover is included for nights spent outside away from base. - Six place oxygen system installed but tank certification not current at this time
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 |
|---|---|---|---|---|---|---|
|
Alan Hardwick / T Bjorling
trade-a-plane.com
|
$254,900
|
Kenly, NC | Jun 02, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 210
This 1968 Cessna 210 (N2209R) is a 6-seat single engine piston with 4,265 hours on the airframe. There are currently 26 210 aircraft listed for sale with asking prices ranging from $89,000 to $360,114. This aircraft is priced above the market average at $254,900.
The 210 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 4,265 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. There are 10 airworthiness directives applicable to this aircraft type — review AD compliance carefully before purchase. Mechanics have filed 10 service difficulty reports for this type — common maintenance items to discuss during pre-buy.
Pre-Purchase Checklist
Cessna 210 — 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
FAA registration data pending for N2209R.
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 N2209R against the NTSB accident database.
Airworthiness Directives — Cessna 210
ADs are mandatory safety instructions issued by the FAA. 10 recent ADs found for this aircraft type.
Cessna Aircraft Company 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 206, P206, U206, TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 Series Airplanes
View full AD →Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190, 195, 206, 207, 210, T303, 336, and 337 Airplanes
View full AD →Cessna Aircraft Company (Cessna) 172, 175, 177, 180, 182, 185, 206, 207, 208, 210, 303, 336, and 337 Series Airplanes
View full AD →Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series Airplanes
View full AD →Cessna Aircraft Company 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 206, P206, U206, TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 Series Airplanes
View full AD →Cessna Aircraft Company 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 206, P206, U206, TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 Series Airplanes
View full AD →Cessna Aircraft Company P206, TP206, TU206, U206, 207, T207, 210, P210, and T210 Series Airplanes
View full AD →Cessna Aircraft Company 150, 152, 172, 177, 180, 182, 185, 188, 206, 207, 210, and 337 Series Airplanes
View full AD →Cessna Aircraft Company Models T210N, P210N, and P210R Airplanes
View full AD →Source: FAA Airworthiness Directives database. Showing most recent ADs for this aircraft type.
Service Difficulty Reports — Cessna 210
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
ELECTRICAL FUEL BOOST PUMP BYPASS VALVE FAILED IN BYPASS PREVENTING FUEL FROM REACHING ENGINE PREVENTING ENGINE FROM START. PUMP FAILED AFTER 20 MONTHS IN SERVICE. FAILED WITHOUT WARNING OR INDICATION.
SEAT BACK CAM RETAINING PINS LOOSE, MISSING AND OR SHEARED FOUND SAFETY-WIRED IN PLACE. THERE APPEARS TO BE MANY OF THESE INFINITE ADJUSTABLE LOWER SEAT FRAMES WITH THE NAS SPLIT-PINS SAFETY-WIRED IN PLACE. THERE IS NO REQUIREMENT TO ADD SAFETY-WIRE ...
FAILED DURING LANDING. UPON INSPECTION AFTER A COLLAPSE OF LANDING GEAR UPON TOUCHDOWN INCIDENT, THE HYDRAULIC PUMP WAS FOUND TO BE LEAKING INTERNALLY.
OUTBOARD LEFT LANDING GEAR WELL STRUCTURAL PANEL CRACKED FROM LOWER FORWARD EDGE OF PANEL. THE CRACK EXTENDED UPWARD THROUGH THE PANEL AND A DOUBLER BRACKET TO THE FUEL LINE PENETRATION HOLE IN THE PANEL. NO PREVIOUS REPAIR ON THIS PANEL.
OUTBOARD RIGHT LANDING GEAR WELL STRUCTURAL PANEL CRACKED FROM LOWER FORWARD EDGE OF PANEL. THE CRACK EXTENDED UPWARD UNDERNEATH A DOUBLER BRACKET THROUGH THE PANEL AND A PREVIOUS REPAIR DOUBLER, THROUGH A FUEL LINE PENETRATION HOLE IN THE PANEL. THE...
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...
WE RECENTLY REPLACED AN ALTERNATOR DUE TO THE CHARGING SYSTEM DROPPING OUT IN FLIGHT, AND UPON EXAMINATION OF THE REMOVED ONE, IT WAS FOUND THAT TWO OF THE FOUR CASE SCREWS ARE LOOSE, BUT SAFETY WIRES ARE STILL IN PLACE. PLANE POWER MODEL ASG1200-1-...
UPON GEAR RETRACTION THE PISTON HOUSING FOR THE PISTON RACK ON THE ROTARY ACTUATOR CRACKED AT THE THREADED END CAP. ONCE HOUSING CRACKED FLUID ESCAPED CAUSING THE MAIN LANDING GEAR TO BE UNSECURED. PILOT MOVED GEAR HANDLE TO THE DOWN POSITION AND WAS...
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...
N4678Q, C210, DECLARED AN EMERGENCY DUE TO POSSIBLE ELECTRICAL ISSUE. THE FLIGHT LANDED SAFELY WITHOUT ISSUE.
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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