1967 Cessna 210G
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
IFRDynon Skyview HDX Primary Flight Display o Synthetic Vision o ADSB-In Functionality with Integrated Moving Map/Approach Plates/Enroute Charts/Sectionals
Traffic and NEXRAD Weather Overlay o Primary Engine Monitor Including 6 Cylinder CHT/EGT sensors
Fuel Flow Fuel Quantity Gear Indication Gear Warning Flap Position and OATPS Engineering 8000BT Audio Panel with Bluetooth and Aux Audio input o 6 Place Intercom
Garmin GNS530W GPS Navigator o AviaDescription
1967 Cessna 210G Centurion For Sale in Illinois, United States, 2733 hours, $180000 | Aircraftforsale.com
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 |
|---|---|---|---|---|---|---|
|
Ken Peters
aircraftforsale.com
|
$180,000
|
Romeoville, Il | May 02, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 210G
This 1967 Cessna 210G (N5902F) is a 6-seat single engine piston with 2,733 hours on the airframe. There are currently 2 210G aircraft listed for sale with asking prices ranging from $150,000 to $180,000. This aircraft is priced above the market average at $180,000.
The 210G 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 2,733 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 10 service difficulty reports for this type — common maintenance items to discuss during pre-buy.
Pre-Purchase Checklist
Cessna 210G — 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 N5902F.
Location & Ownership
Aircraft Location
Romeoville, Il
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 safety data coming soon.
We'll check N5902F against the NTSB accident database.
Service Difficulty Reports — Cessna 210G
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
(CAN) CYLINDER NR 1 REMOVED DUE TO LOW COMPRESSION. PRIMARY LOSS OF COMPRESSION OBSERVED FROM CRANKCASE BREATHER, RINGS. CYLINDER REMOVED TO CORRECT CONDITION. IT WAS OBSERVED THAT THE NICKEL/CARBIDE FINISH HAS DELAMINATED FROM CYLINDER WALL. LOSS ...
AFT BULKHEAD INSPECTED IAW AD 72-07-09. FOUND A CRACK IN LOWER INBD CORNER OF RT CUTOUT. REPLACED BULKHEAD.
DURING COMPLIANCE WITH SEB88-3 TO REPLACE FORWARD STABILIZER ATTACH FITTINGS PN 0732601-5, IT WAS DISCOVERED THAT THE TOP TWO RIVETS OF BOTH FITTINGS HAD FAILED LEAVING ONLY THE THREE RIVETS IN THE LOWER PORTION OF EACH FITTING. ALL FOUR RIVETS FAIL...
DURING INSPECTION, FOUND GREASE LIKE FLUID ON INDUCTION TUBES AND WHERE CYLINDER AND HEAD ATTACH. REMOVED AND SENT TO OVERHAUL SHOP. REPORTED CRACKED HEAD WILL COME OFF SOON. REMOVED AND REPLACED CYLINDER. SUBMITTER RECOMMENDED CHECKING THIS LOCA...
RIGHT MAIN LANDING GEAR FAILED TO UNLOCK WHEN EXTENDED. PILOT TRIED NUMEROUS TIMES TO GET GEAR TO EXTEND INCLUDING MANUALLY PUMPING. HE ELECTED TO LAND GEAR UP. DURING INCIDENT INVESTIGATION, FOUND THE UPLOCK LEVER TO CONTROL LINK PIN MISSING. MA...
BULKHEAD FOUND CRACKED DURING ANNUAL INSPECTION PER AD 72-07-09. EFFECTIVE DATE 4-1-72.
PROPELLER WENT TO HIGH PITCH DURING RUN-UP AND WOULD NOT RETURN TO LOW PITCH. WHEN THE PROPELLER DOME WAS REMOVED, APPROXIMATELY 3 CC'S OF RUSTY WATER RAN OUT. DISASSEMBLY OF THE PROPELLER AT THE PROP SHOP REVEALED SEVERE RUSTING OF INTERNAL STEEL ...
TURBOCHARGER EXHAUST HOUSING CRACKED AROUND AUXILIARY MOUNTING LUG.
(CAN) CRACKS DISCOVERED AROUND BOLT HOLES ON THE OUTBOARD SIDE OF THE DOUBLER. LEFT HAND SIDE OF THE MAIN LANDING GEAR.
(CAN) DURING A 100 HOUR ANNUAL INSPECTION A CRACK WAS FOUND ON THE AFT BULKHEAD AT STA. 230.1. THE BULKHEAD IS AN ATTACH FOR THE VERTICAL FIN. THE CRACK IS LOCATED ON THE RIGHT HAND SIDE FROM THE CUT OUT FOR THE RUDDER CABLES AND MIGRATES TOWARD THE ...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
AeroGurus Market Estimate AME
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