1981 Cessna P210
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
IFRGarmin GTS 800 TAS ADSB In/Out GTX335ES Mode "ES" converted to ES for ADSB compliance prior
Garmin 275 JPI EDM 930 power panel WX-500 storm scope O&N new style Master Caution with chip 1-2-3 Shadin fuel computer with digital fuel meters aux tanks management moved to panel with 5 tank gauge Battery backup Glare Shield lighting Precise Flight General 5 speed brakes ELT 406 Whelen LED beaconDescription
1981 model airframe, 674* P210N built by Cessna. No damage history, extremely clean. Aircraft was converted Feb 2014 by O&N. At that time this aircraft was converted the engine enhancement was an option and the engine has a cruise power rating of 21.0M over standard power and therefore was not enhanced due to the high plan rating of the engine out of Rolls-Royce Factory. This Silver Eagle is equipped, speed brakes, Bod Field electric door seal, Lo Presti Boom Beam Lights, BAS Shoulder Harness 1, Leather seats. Thermal pane interior glass windows. Has the newest carbon fiber forward headliner shell. Has wind driven drop down "BAT" generator for emergencies. Engine Specs: Rolls-Royce 250B17F/2 450hp engine with a run rating of 21.0 (ENHANCED) Has late Bleed Air inlet. Aircraft annual is fresh.
Propeller
Propeller Make: MT 5 BLADE Propeller Serial number: 140548 Propeller total time since new: 304 INSTALLED AT HOBBS 872.0 since new
Modifications / STCs
• De-ice system: Boots all new at conversion
• Glass: All new polycarbonate new interior thermal panes
• Air conditioner: Standard O&N Silver Eagle electric
• Glare shield: new one piece with LED backup lighting
• Fuel System: Main 89 gallons, aft tank, with Float Tips 31 gallons totaling 147.0
• Damage History: Non-excellent low time airframe no corrosion
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 |
|---|---|---|---|---|---|---|
|
PropJet Aviation
controller.com
|
$975,000
|
Santa Rosa, CA | Mar 25, 2026 | — | Active | |
|
PropJet Aviation
aviationtrader.com.au
|
$1,005,345
|
Santa Rosa, California, Australia | Apr 04, 2026 | — | Active | |
|
PropJet Aviation
controlleremea.co.uk
|
$993,096 *
GBP £737,126
|
Santa Rosa, CA | 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 P210
This 1981 Cessna P210 (N210NL) is a 6-seat single engine piston with 1,175 hours on the airframe. There are currently 24 P210 aircraft listed for sale with asking prices ranging from $180,000 to $975,000. This aircraft is priced above the market average at $975,000.
The P210 cruises at 180 kts (333 km/h) with a range of 850 nm (1,574 km) — ideal for short hops and local flights. Service ceiling of 23,000 ft allows operation above most weather.
Operating costs: Fuel burn is 16 GPH (61 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $88/hr in fuel alone. Total variable cost including maintenance reserves is approximately $190/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $22,000. With 1,175 hours on the airframe, this aircraft has 225 hours remaining to engine TBO .
NTSB records show 0 incidents for this airframe — a clean safety record. There are 2 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 P210 — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA P210
AeroGurus estimates based on industry averages for the CESSNA P210. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
FAA registration data pending for N210NL.
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 N210NL against the NTSB accident database.
Airworthiness Directives — Cessna P210
ADs are mandatory safety instructions issued by the FAA. 2 recent ADs found for this aircraft type.
Cessna Aircraft Company P206, TP206, TU206, U206, 207, T207, 210, P210, and T210 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 P210
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
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.
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...
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...
WHILE IN CRUISE FLIGHT ABOVE 10,000 FEET, THERE WAS INSUFFICIENT PITCH TO REDUCE RPM TO CRUISE CONDITION. PROPELLER HUB DISASSEMBLED, AND FOUND A BROKEN PROPELLER RETURN SPRING WAS INTERFERING WITH THE HIGH PITCH STOP, SUCH THAT ONLY 27 DEGREES OF P...
DURING ANNUAL INSPECTION, A FUEL ODOR WAS NOTED IN THE COCKPIT. INVESTIGATION FOUND THE ALUMINUM FUEL PRESSURE LINE HAS CORRODED THROUGH AT THE POINT WHERE A WIRE BUNDLE WAS ZIP TIED AGAINST THE FUEL PRESSURE LINE.
AIRCRAFT DEPARTED TAXIWAY. NO DAMAGE TO AIRCRAFT. AIRCRAFT TOWED TO HANGAR. FOUND AIR BUBBLES IN BRAKE LINE WHILE BLEEDING BRAKES. TOPPED OFF RESERVOIR. INSPECTED FOR LEAKS, NONE. FOUND BRAKE PEDAL WAS FIRM. RETURNED ACFT TO SERVICE.
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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