1979 Cessna 210N
Single Engine Piston
Aircraft Details
Seller reportedDescription
1979 Cessna 210N N6621A: High-performance complex aircraft Hours: 9,239 TTAF Upgraded IO-550L (300 HP) with 835 hours Since Factory Remanufacture (SFRM). Propeller 920 hours Since Overhaul (SMOH) (Hartzell Scimitar ) Avionics: Garmin GNS-530W WAAS GPS, L3 Lynx NGT-9000 Digital Transponder w/ ADS-B In/Out, and STEC 55X Autopilot with Glideslope Coupling. King KCS-55A Slaved HSI. Condition: Maintained to the strictest standards by the U.S. Customs Aviation Fleet. No Known Damage History. New custom leather interior (2020, Rated 9+). Exterior Rated 7+/8. Equipped Electric Air-Conditioning.
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 |
|---|---|---|---|---|---|---|
|
Luiz Siqueira
barnstormers.com
|
$360,000
|
Coral Springs, FL | May 15, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 210N
This 1979 Cessna 210N (N6621A) is a 6-seat single engine piston . There are currently 3 210N aircraft listed for sale with asking prices ranging from $200,000 to $360,000. This aircraft is priced above the market average at $360,000.
The 210N cruises at 164 kts (304 km/h) with a range of 900 nm (1,667 km) — ideal for short hops and local flights.
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.
NTSB records show 0 incidents for this airframe — a clean safety record. There are 1 airworthiness directive 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 210N — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA 210N
AeroGurus estimates based on industry averages for the CESSNA 210N. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
FAA registration data pending for N6621A.
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 N6621A against the NTSB accident database.
Airworthiness Directives — Cessna 210N
ADs are mandatory safety instructions issued by the FAA. 1 recent AD found for this aircraft type.
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 210N
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.
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-...
THE SHAPE OF THE FORWARD NOSE GEAR DOOR HINGES DO NOT ALLOW THE DOORS TO OPEN WITH THE BARREL LINKAGE DISCONNECTED. IF THE BARREL LINKAGE BREAKS, THE NOSE GEAR WILL NOT PUSH THE GEAR DOORS OPEN. IF THE HINGES WERE SHAPED SLIGHTLY DIFFERENT, THIS PROB...
ON TAKE OFF, AIRCRAFT EXPERIENCED A LOSS OF POWER AND THE PILOT ABORTED THE TAKE OFF. INSPECTION OF THE AIRCRAFT DID NOT SHOW ANY IRREGULARITIES. ENGINE HAD COMPRESSION IN ALL SIX CYLINDERS. ALL 12 SPARK PLUGS WERE CLEAN AND HAD GOOD SPARK WHEN THE M...
WHILE INBOUND TO SNA THE AIRCRAFT RADIOS WENT DEAD AND THE BATTERY WENT DEAD. THE PILOT CONTACTED SNA TOWER USING HIS CELL PHONE AND WAS CLEARED TO LAND. AFTER LANDING IT WAS DISCOVERED THE ALTERNATOR DRIVE BELT FAILED AND THE AIRCRAFT WAS RUNNING O...
WEATHER RADAR POD. DURING ANNUAL INSPECTION IT WAS NOTED THAT THE RADAR SUPPORT POD WAS GAPING BY APPROX 1/2 INCH AT THE REAR END AND THE BLACK WEATHER SEAL WAS DISPLACED. ON FURTHER INVESTIGATION IT WAS ESTABLISHED THAT THE REAR POD SUPPORT WAS LO...
DAMAGED BEYOND REPAIR.
THE LEFT NOSE TRUNNION SUPPORT BRACE HAD A STRESS CRACK AT THE TRUNNION MOUNT EAR. THE CRACK FINALLY CAUSED A FAILURE ON TAKEOFF AT KACT ON 10/25/2017. THIS FAILURE IN TURN CAUSED THE RIGHT TRUNNION SUPPORT TO FAIL AND ULTIMATELY COMPLETE NOSE GEAR...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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