1985 Cessna P210R
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
IFRDescription
For more detailed information of the aircraft please reach out to me for the digital logs.
Engine
TTSO - 333.5 FUEL - TOTAL 149 WINGS 120. AFT AUX 29 Continental TSIO-520-CE CN: 1002675 OVERHAUL - 2021 TURBO - CHARGED DUAL ALTERNATORS DUAL VACUUM PUMPS ELECTRIC ENGINE PRIMER AUX. FUEL PUMP
Propeller
TTSN: 333.5 McCAULEY THREE BLADED PROP MODEL - D3A36C410-B SERIAL NUMBER - 201030
Interior
Interior -2021
Modifications / STCs
• FIKI
• STC - INFLATABLE DOORNO TINTED SUN VISORS
• LED LDG. GEAR LITES
• LED NAV/POSITION LITES
• LED WHELEN RED BEACON / STROBES
• TCAS
• LOW CABIN PRESSURE WARNING LITES
• PROP ANTI ICE AMPERAGE GUAGE
• ELECTRIC ENGINE PRIMER
• ELECTRIC PITCH TRIM
• RUDDER TRIM
• AUX FUEL PUMP
• OVERHEAD FRESH AIR VENTS
• ARTICULATING PILOT AND COPILOT SEAT
• ARTICULATING MIDDLE SEATS
• ELT
• THREE WAY HARNESS FOR PILOTS SEATS
• FACTORY AIR CONDITIONING
• OXYGEN FOR ALL SEATS AND MUCH MORE
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 |
|---|---|---|---|---|---|---|
|
Flying W
controller.com
|
$530,000
|
San Antonio, TX | Mar 25, 2026 | — | Active | |
|
Flying W
aviationtrader.com.au
|
Call for price *
|
San Antonio, Texas, Australia | Apr 04, 2026 | — | Active | |
|
Flying W
controlleremea.co.uk
|
Call for price *
|
San Antonio, TX | 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 P210R
This 1985 Cessna P210R (N210LA) is a 6-seat single engine piston . There are currently 2 P210R aircraft listed for sale with asking prices ranging from $425,000 to $530,000. This aircraft is priced above the market average at $530,000.
The P210R cruises at 180 kts (333 km/h) with a range of 850 nm (1,574 km) — ideal for short hops and local flights.
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.
Ownership & Registration
FAA registration data pending for N210LA.
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 N210LA 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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