1977 Cessna T210K
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
IFRresent update Sandel Storm scope SN3308 Trans Gar GTX-327 New Gar G5 Standby ADI Insight Strike finder Bendix King KX-155 second radio ADSB Out
Description
1977 Cessna T210K Turbo Centurion N210W - 300HP Ram Conversion $180,000 TTAF: 5475 ENG: TSIO 520-RAM Conversion 300HP Eng Prop Total SNEW: 793.9 hrs 2008 Install Prop: 3 blade Hartzell PHC-J3YF-1RF 793.9 hrs 2008 Install JPI 830 Eng Monitor GAMI Injectors Robertson STOL SPAR AD - Done - Perfect shape New tires and tubes Reel Shoulder harnesses Hydraulic Power Pack and Pressure pump New 2025 Annual Date: Aug 2025 Avionics List: 55X Auto Pilot Garmin 430 GPS, resent update Sandel Storm scope SN3308 Trans Gar GTX-327 New Gar G5 Standby ADI Insight Strike finder Bendix King KX-155 second radio ADSB Out Interior condition: New 1995 Painted 1995 Located KFLY - Colorado Springs CO Logs: All logs since New Log books available PDF upon request
Engine
ENG: TSIO 520-RAM Conversion 300HP Eng Prop Total SNEW: 793.9 hrs 2008 Install Prop: 3 blade Hartzell PHC-J3YF-1RF 793hrs 2008 Install JPI 830 Eng Monitor GAMI Injectors
Interior
6 Seats New 1995 Reel Shoulder harnesses
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 |
|---|---|---|---|---|---|---|
|
David Duncan
trade-a-plane.com
|
$180,000
|
Colorado Springs, CO | Mar 20, 2026 | — | Active | |
|
David Duncan
barnstormers.com
|
$180,000
|
Colorado Springs, CO | Mar 16, 2026 | — | Active |
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Cessna T210K loan calculator
AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna T210K
This 1977 Cessna T210K (N210W) is a 6-seat single engine piston with 5,475 hours on the airframe. There are currently 2 T210K aircraft listed for sale with asking prices ranging from $180,000 to $180,000. This aircraft is listed at the market average at $180,000.
The T210K 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 5,475 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 8 service difficulty reports for this type — common maintenance items to discuss during pre-buy.
Pre-Purchase Checklist
Cessna T210K — 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 N210W.
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 database checked for N210W.
Service Difficulty Reports — Cessna T210K
SDRs are reports filed by mechanics about problems found during maintenance. 8 recent reports for this aircraft type.
OWNER/PILOT REPORTED THAT AFTER LANDING, FLAPS WOULD NOT RETRACT TO FULL UP NOR DID FLAP INDICATOR INDICATE CORRECT POSITION OF FLAPS. TROUBLESHOOTING REVEALED THAT FLAP FOLLOW UP CABLE OUTER CASING SHATTERED JUST INBD OF ATTACH CLAMP IN ROOF ABOVE...
(CAN) THE BULKHEAD DOUBLER REINFORCES THE HOLE WHERE THE HORIZONTAL STAB ATTCHES. DOUBLER SPLIT IN TWO THROUGH THE ANCHOR NUT RIVIT HOLE. THIS DOUBLER IS ONLY FOUND ON EARLY MODELS.
FOUND (BRACKETT) AIR FILTER ASSEMBLY (NR-BA-2405) INSTALLED BACKWARDS. THE MESH SAFTEY SCREEN WAS AT THE FRONT OF THE FOAM FILTER, AND THE INLET GRID WAS INSTALLED AT THE BACK OF THE ASSEMBLY. INSPECTED ONE OTHER FILTER ASSEMBLY ON LIKE AIRCRAFT A...
(CAN) UPPER NOSE GEAR TORQUE LINK FOUND CRACKED AS SHOWN. CRACK WAS IN TWO LOCATIONS ABOUT 1/8 INCH LONG. PART HAD NOT FAILED.THIS IS THE SECOND PART FOUND CRACKED ON CESSNA 210 AIRCRAFT, BOTH IN THE SAME LOCATION.
AFTER TAKEOFF, LANDING GEAR FAILED TO RETRACT OR EXTEND. AN EMERGENCY LANDING WAS PERFORMED WITH GEAR IN THE INTERMEDIATE POSITION. POST-FLIGHT INSPECTION REVEALED THE ACTUATOR HAD RUPTURED AT THE FORGING SEAM FROM FORE TO AFT. NEW ACTUATOR WAS IN...
THE PROPELLER HUB WAS FOUND CRACKED AT 5 OF THE 6 MOUNTING STUDS. THE PROPELLER HAD ACCUMULATED APPROXIMATELY 40 HOURS OF OPERATING TIME SINCE THE LAST OVERHAUL PERFORMED ON 1-10-96. THE CRACKS WERE DISCOVERED BY AN IA WHILE PERFORMING THE ANNUAL I...
DURING 100 HOUR INSPECTION, FOUND PROP HUB CRACKED AT 5 OF THE 6 MOUNTING STUDS.
DURING ANNUAL INSPECTION, FOUND ELEVATOR 'UP' CABLE WORN THROUGH AT PULLEY JUST FORWARD OF GEARBOX. PULLEY WAS NOT TURNING DUE TO BRACKET THAT HOLDS PULLEY WAS INSTALLED AT AN ANGLE. IT APPEARS BRACKET WAS INSTALLED THAT WAY FROM FACTORY. LOG BOOK...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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