1961 Cessna 210A
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
IFRADSB In Out 1-Garmin GMR 345 Audio Panel 1-Garmin SL30 Nav Com 1-Garmin GI 275 ADI 1-Garmin GI 275 HSI Electronics Int. Digital Tachometer Electronics Int. Digital Volts/Amps JPI EDM-730 Engine Monitor w/Fuel Flow/Totalizer HP Readout Air Gizmo Panel Mounted Garmin 796 GPS (displays ADSB)
Description
1961 Cessna 210A, 3872 TTSN, 99 SMOH 99 SPOH, IO-470 Continental 260HP, November 2025 Annual, Excellent Paint Interior, Garmin 530W, Garmin 345 Transponder (ADSB In Out), Garmin 345 Stereo Audio Panel w/Bluetooth, Garmin SL-30 Nav-Com, Garmin G5 Attitude, Garmin G5 HSI, Garmin 106A Glideslope, JPI EDM-730 Engine Monitor w/Fuel Flow HP, EI Digital Tach, EI Digital Volts/Amps, Garmin 796 Panel Mounted (displays ADSB), This is a super nice 210 owned by a corporate pilot All Logs Since New. Beautiful, Fast, Turnkey and ready to fly. $129,000,
Engine
99 SMOH Continental IO-470-E 260HP
Interior
Excellent Paint in Retro colors, Beautiful! Excellent Light Beige Leather with matching side panels and carpet, including recent headliner.
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 |
|---|---|---|---|---|---|---|
|
Southern Wings Aircraft Sales
trade-a-plane.com
|
$129,000
|
Oklahoma City, OK | Mar 30, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 210A
This 1961 Cessna 210A (N9499X) is a 6-seat single engine piston with 3,872 hours on the airframe. There are currently 5 210A aircraft listed for sale with asking prices ranging from $70,000 to $159,000. This aircraft is priced above the market average at $129,000.
The 210A 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 3,872 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 4 service difficulty reports for this type — common maintenance items to discuss during pre-buy.
Pre-Purchase Checklist
Cessna 210A — 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 N9499X.
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 N9499X against the NTSB accident database.
Service Difficulty Reports — Cessna 210A
SDRs are reports filed by mechanics about problems found during maintenance. 4 recent reports for this aircraft type.
(AUS) HYDRAULIC PUMP DRIVE SHAFT CASE HARDENING HAD FAILED IN AREA OF KEYWAY ALLOWING KEY TO TILT AND JAM. RESIDUAL METAL FROM FAILED AREA HAD DAMAGED SHAFT SEAL LEADING TO FLUID LEAKAGE.
(AUS) RT MUFFLER PIPE CRACKED FOR APPROXIMATELY 75 PERCENT OF CIRCUMFERENCE AROUND JOINT AREA. CRACK WAS HIDDEN BY EXHAUST CLAMPS.
WHILE AC WAS IN SHOP FOR PROP/ENGINE BALANCING, CRACK APPROX 4.5 INCHES LONG WAS FOUND ON REAR PANEL OF LOWER FORWARD FUSELAGE STRUCTURE. PANEL PN 12530181. PANEL WAS REPAIRED BY ADDITION OF DOUBLER AS SHOWN ON 377. CRACK WAS LOCATED ON SHEET METAL...
THE ATTACHING FLANGE OF THE HORIZONTAL BULKHEAD WAS FOUND CRACKED DURING THE ANNUAL INSPECTION WHERE IT ATTACHES TO THE STA 209.0 VERTICAL BULKHEAD. NOTED AREA WAS CRACKED 4 INCHES IN LENGTH. CRACK WAS ON THE CENTER ATTACHING FLANGE AND WAS FOUND B...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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