1966 Cessna T210F
Single Engine Piston
Aircraft Details
Seller reportedDescription
Straight, clean, mechanically sound 1966 210F, SN 159 of 197. This plane has spent little time outside. Airframe: TTAF: 3910 Engines: Time: 1031.26 Hours SFRM
Engine
Time: 1031.26 Hours SFRM
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 |
|---|---|---|---|---|---|---|
|
Alex Navarre
aircraftdealer.com
|
$152,000
|
SC | Mar 15, 2026 | 1 days | Active |
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Cessna T210F loan calculator
AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna T210F
This 1966 Cessna T210F (N6759R) is a 4-seat single engine piston with 3,910 hours on the airframe. This aircraft is listed at the market average at $152,000.
The T210F cruises at 164 kts (304 km/h) with a range of 900 nm (1,667 km) — ideal for short hops and local flights.
FAA registration status: Valid. NTSB records show 0 incidents for this airframe — a clean safety record. Mechanics have filed 10 service difficulty reports for this type — common maintenance items to discuss during pre-buy.
Pre-Purchase Checklist
Cessna T210F — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Ownership & Registration
Registered Owner
ABC AERO LLC
Registration Address
PARADISE VALLEY, AZ
Certificate Issued
2023-08-31
Airworthiness
1966-06-14
FAA Status
Valid
Source: FAA Aircraft Registry, updated Mar 15, 2026
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 N6759R.
Service Difficulty Reports — Cessna T210F
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
INVESTIGATION OF LOW MANIFOLD PRESSURE BY TECH RVEALED THE STEEL TAB RIVETED TO ALTERNATE AIR DOOR FOR MAGNETIC CLOSURE HAD FALLEN OFF AND ENTERED TURBOCHARGER. THE RIVETS USED TO FASTEN TAB TO DOOR WERE MISSING ALONG WITH THE TAB. THE RIVET HOLES ...
DURING AN ANNUAL INSP, FOUND LT ELEVATOR TORQUE TUBE LOOSE, AFTER REPAIR WHILE CHECKING CONTROL SURFACE BALANCE, SURFACE WAS FOUND TO BE BADLY OUT OF BALANCE AT +21 IN LBS. REMOVED T/E AND FOUND IT TO HAVE BEEN REPLACED WITH A FIELD FABRICATED PART...
DURING ANNUAL INSPECTION AND C/W AD 76-14-07, R2 VISUAL INSPECTION AND DYE PENETRANT INSPECTION OF THE APPROVED P/N 1241423-1 AND P/N 1241423-2, LANDING GEAR SADDLES SHOWED CRACKS IN THE FORWARD INBOARD RADIUS OF EACH SADDLE. TOTAL TIME ON EACH PAR...
DURING ANNUAL INSPECTION AND C/W AD 76-14-07, R2 VISUAL INSPECTION AND DYE PENETRANT INSPECTION OF THE APPROVED P/N 1241423-1 AND P/N 1241423-2, LANDING GEAR SADDLES SHOWED CRACKS IN THE FORWARD INBOARD RADIUS OF EACH SADDLE. TOTAL TIME ON EACH PAR...
PILOT REPORTED ENGINE STARTED SURGING THEN CUTTING OUT PRIOR TO COMPLETING THE APPROACH TO LANDING. THE PILOT WAS FORCED TO LAND SHORT OF THE AIRPORT RESULTING IN DAMAGE TO THE AIRCRAFT. INVESTIGATION RESULTED AN IN-FLIGHT FUEL LEAK FROM THE RIGHT ...
DURING DESCENT FROM ALTITUDE AFTER A 2 HOUR CROSS COUNTRY FLIGHT AND 10 MILES FROM HOME BASE, THE ENGINE BEGAN TO RUN ROUGH. DESCENT WAS STOPPED AT 2.500 FEET TILL A SAFE LANDING WAS ASSURED. THE ENGINE, ALTHOUGH RUNNING ROUGH, RAN WITH GOOD OIL PRE...
PILOT BELIEVED FUEL WAS LOST DUE TO SIPHONING FROM FUEL CAPS. OBSERVED LIGHT FUEL STAIN BEHIND BOTH CAPS. O-RINGS APPEAR TO BE OKAY AND CAPS FEEL TIGHT. CLEANED STAINS FROM LEFT WING, FLEW AIRCRAFT, OBSERVED NO NEW STAINS. CAPS BEING REPLACED WIT...
WIRES TO SAFETY SWITCH CHAFED AND WORN INTERNALLY; ALLOWED GEAR TO RETRACT WITHOUT SWITCH BEING OPERATED. CAUSED NOSE GEAR TO RETRACT WITH INSUFFICIENT STRUT CHARGE. GEAR WOULD NOT EXTEND FOR LANDING.
DUE TO THE RELATIVELY LOW TOTAL TIME ON THIS AIRCRAFT (1,399 HRS) AND THE FACT THE LANDING GEAR SADDLES HAD BEEN REPLACED AT 739 HOURS, AD 76-14-07 R2 DID NOT APPLY AT THIS TIME, HOWEVER, THE PART IN QUESTION HAD A CRACK THAT WAS EVIDENT WITHOUT DYE ...
BIL - AFTER TAKEOFF, GEAR WOULD NOT FULLY RETRACT WHEN SELECTED UP. GEAR WAS SELECTED DOWN, AND DOWN AND LOCKED WAS INDICATED. GEAR WAS CYCLED 4 TIMES TO THE DOWN POSITION WITH NO POSITIVE INDICATION. GEAR WAS HAND-PUMPED DOWN, AND AIRCRAFT LANDED...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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