1980 Cessna P210
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
including a Garmin G500 system with synthetic vision and chart capabilities. The avionics are designed to provide pilots with the information they need to fly safely and efficiently. The aircraft also features an S-TEC 3100 autopilot system
which provides advanced autopilot capabilities for added safety and convenience. PFD MFD: Garmin G500 Synthetic Vision and Chart Capabilities GPS/NAV/COMM/MFD: Garmin GTN 750 GTN 650 Autopilot: S-TEC 3100 Inflight satellite weather: Golze ADL200 (for iPad MFDs) ADS-B Transponder: Garmin GTX345D diversity ADS-B in/out DME: Bendix KN62A Traffic Adviser: BFGoodrich Sky497 Stormscope: BFGoodrich WX-1000 Fuel Computer: MiniFlo-L coupled with GTN750 Audio Panel: Garmin GMA53C ELT: ARTEX ELT3000 406MHz AoA System: Garmin GDC74 Stand-by EFIS: Avionics AV30
Description
739.000 ex VAT EASA-Certified N-reg possible MTOW 4000lbs, 200kts TAS, pressured cabin up to FL230, 450SHP with Rolls-Royce Turbine. The Cessna P210N Silver Eagle is a high-performance aircraft that has been converted to a turbine engine. This aircraft is known for its versatility and reliability, making it an excellent choice for both personal and business use. The aircraft has a maximum takeoff weight of 4,000 lbs and can cruise at speeds of up to 200 knots. The cabin is pressurized, allowing for comfortable flight at altitudes of up to FL230. A well-equipped private use Silver Eagle P-210 maintenance by Flightteam Maintenance always in Bavaria. Available for pre buy inspection in Europe ALWAYS HANGARED Airplane time state: Airframe: ------- Total Time 3,500 Range 1,000 NM plus 30min reserve Max Ramp Weight 4,016 lb Max Takeoff Weight 4,000 lb Basic Empty Weight 2,751 lb Useful Load 1,239 lb Fuel Capacity Mass 980 lb Fuel Capacity Volume 144 gal Airframe Notes Max Ceiling: ~23,000ft Best Cruise Ceiling: ~18,000ft by 25gal/h Takeoff Distance: 1,000ft Landing Distance: 1,800ft Engine: ------- Engine 1 Make/Model ROLLS ROYCE 250B17F/2 Engine 1 Notes Engine Time Since Overhaul: ~400 hrs Props: ------- Prop 1 Manufacturer MT Prop 1 Model MT 5 Blade Reversible Prop 1 Time 400 SNEW
Engine
1 Engine, Turboprops
Interior
The interior of the aircraft is in excellent condition, with beige leather seats that are like new (refurbished 2021). The cabin is equipped with a pressurized system that maintains a comfortable cabin altitude up to FL230. The aircraft has been designed to accommodate six passengers comfortably, with ample legroom and headroom. Seats: 6-Seater beige leather, like new Plugs for Pilots: Lemo Cinch Plugs Passengers: Lemo with USB Charger (Stereo) Air Condition: O N Pressured Cabin: 3,5 psi up to FL230 DOW: 1147,59kg / 2530Lbs MTOW: 1821,63 kg/ 4016 Lbs Payload 6-Seated: 675 kg zero fuel Payload 5-Seated: 687 kg zero fuel
Exterior
Paint: Red Silver Metallic (new paint 2021)
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 |
|---|---|---|---|---|---|---|
|
WeFly
planecheck.com
|
$860,864 *
€ 739,000
|
Germany | May 03, 2026 | — | Active | |
|
Listing Source
globalplanesearch.com
|
Contact for price
|
Langenhagen Nds | Mar 17, 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 1980 Cessna P210 (D-EREA) is a 6-seat single engine piston with 3,500 hours on the airframe. There are currently 24 P210 aircraft listed for sale with asking prices ranging from $180,000 to $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 3,500 hours on the airframe, this aircraft has exceeded TBO (1,400 hrs) — verify engine status and overhaul reserve.
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 registry covers US-registered aircraft (N-numbers).
This aircraft (D-EREA) is registered outside the US.
Location & Ownership
Aircraft Location
Langenhagen Nds
Seller reportedTitle 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 database checked for D-EREA.
Note: NTSB covers US-registered aircraft (N-numbers). This aircraft is registered in a non-US country (D-EREA). Safety records from the national aviation authority may not be included in our 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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