1985 Cessna P210R
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
IFRDescription
OCR Aviation is thrilled to present the exceptional Cessna P210R, a rare gem with only 42 units ever produced. This highly sought-after aircraft features a state-of-the-art Garmin Avionics Suite, providing cutting-edge navigation and communication technology for a seamless flying experience. Powered by a robust 325HP engine, it ensures outstanding performance and reliability, while its impeccable maintenance history guarantees peak operational efficiency. Additional highlights include speed brakes and factory-installed air conditioning to keep you comfortable on your journeys. Don't miss this opportunity to own an exclusive aircraft that combines performance, impeccable maintenance, and rarity-contact OCR Aviation today to schedule a viewing and take to the skies in style!
Engine
Factory remanufactured engine installed on 7/2011 - New cylinders, lifters, magnetos, propeller, fuel and oil hoses installed 3/2018 - Dual Alternators - Dual Vacuum Pumps - Millenium Cylinders
Propeller
No Known Damage History Complete Logs Dry Climate Based Factory A/C Three Owners - Professionally Flown Always Hangered
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 |
|---|---|---|---|---|---|---|
|
OCR Aviation
trade-a-plane.com
|
Contact for Price
|
Long Beach, CA | Jun 18, 2026 | 4 days | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna P210R
This 1985 Cessna P210R (N68EA) is a 6-seat single engine piston with 4,382 hours on the airframe. There are currently 3 P210R aircraft listed for sale with asking prices ranging from $425,000 to $530,000.
The P210R cruises at 213 kts (394 km/h) with a range of 900 nm (1,667 km) — ideal for short hops and local flights. Service ceiling of 23,000 ft allows operation above most weather.
Operating costs: Fuel burn is 18 GPH (68 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $99/hr in fuel alone. With 4,382 hours on the airframe, this aircraft has exceeded TBO (1,800 hrs) — verify engine status and overhaul reserve.
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 8 service difficulty reports for this type — common maintenance items to discuss during pre-buy.
Pre-Purchase Checklist
Cessna P210R — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA P210R
AeroGurus estimates based on industry averages for the CESSNA P210R. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
FAA registration data pending for N68EA.
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 N68EA against the NTSB accident database.
Airworthiness Directives — Cessna P210R
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 P210R
SDRs are reports filed by mechanics about problems found during maintenance. 8 recent reports for this aircraft type.
CYLINDER NR 1 WAS RUNNING TOO COOL. WEAK COMPRESSION WAS NOTED PULLING PROPELLER THROUGH. COMPRESSION TEST RESULTS 65/80. FERROUS METAL NOTED IN FILTER ELEMENT. ROCKER COVER WAS REMOVED. ROCKER ARM FOR EXHAUST WAS HITTING ON SPRING RETAINER. EN...
CYLINDER NR 1 WAS RUNNING TOO COOL. WEAK COMPRESSION WAS NOTED PULLING PROPELLER THROUGH. COMPRESSION TEST RESULTS 65/80. FERROUS METAL NOTED IN FILTER ELEMENT. ROCKER COVER WAS REMOVED. ROCKER ARM FOR EXHAUST WAS HITTING ON SPRING RETAINER. EN...
DURING AN ENGINE CHANGE, PLAY WAS NOTED IN ROD ASSEMBLY LINKING VAPC WITH THE THROTTLE BODY. UPON DISASSEMBLY OF THE LINK ROD UNIT, NOTED THE ROD END 632557 WAS WORN WHERE IT CONNECTED TO THEVAPC LINKAGE. APPROXIMATELY 20 PERCENT REDUCTION IN DIAM...
DURING ANNUAL INSPECTION, PLAY WAS NOTED IN ROD ASSEMBLY LINKING VAPC WITH THE THROTTLE BODY. UPON DISASSEMBLY OF LINK ROD UNIT, NOTED THE ROD END 63251 WAS WORN WHERE IT CONNECTED TO THE VAPC LINKAGE. APPROXIMATELY 20 PERCENT REDUCTION IN DIAMETER...
JUST AFTER TAKEOFF, THE ENGINE STARTED TO RUN ROUGH AND LOST POWER. PILOT RETRACTED GEAR AND LANDED IN FIELD. INVESTIGATION REVEALED THE CRANKSHAFT FAILED BETWEEN NR 2 AND NR 3 CYLINDERS NTSB NR CHI98LA360. THE ENGINE IS STILL INSTALLED ON AIRCRAF...
THREADED STUD STAKED IN ROD END PULLS THROUGH WHICH WOULD ALLOW NOSE GEAR DOOR TO JAM OR FLAP IN THE AIRFLOW. THIS WAS FOUND DURING AN INSPECTION.
WHEN CHECKING ELT OUTPUT PER FAR 91.207(D)(4), UNIT COULD NOT BE HEARD ON NEARBY AM RADIO, BUT COULD BE RECEIVED ON AIRCRAFT'S VHF RADIO. FOUND ANTENNA CABLE CENTER CONDUCTOR INTERNALLY SHORTED TO GROUND. PROPERLY OPERATING ELT SHOULD BLEED OVER ON...
FOUND BULKHEAD CRACKED AT THE LEFT AND RIGHT HORIZONTAL STABILIZER ATTACHMENT BRACKETS.
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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