1964 Cessna 180G
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
VFRDescription
N411SH is a 1964 Cessna 180G with factory float kit that has new hardware and pork chops as well as a Robertson STOL kit. N411SH has a total time of 4434.00hrs. It has a Continental O-470R with 2800.00hrs and 200.00hrs SMOH that occured in February of 2018. This aircraft is equipped with a Hartzell 3-blade Scimitar propeller with TTSN of 150.00hrs. This is a four place aircraft with removable backseats for additional storage. All log books are available. For further inquiry, please contact William Schretzmann, cell: 3868675088.
Engine
Engine: Continental M/N: O-470R S/N: 212394-R TT: 2800.00hrs SMOH: 200.00hrs, occurred in February 2018 Propeller: Hartzell 3-blade Scimitar M/N: PHC-C3YF-1RF/F8060 S/N: QG1806B Blade #1 S/N: MO 4283 Blade #2 S/N: MO 4285 Blade #3 S/N: MO 4286 TT: 150.00hrs since 2020
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 |
|---|---|---|---|---|---|---|
|
William Schretzmann
trade-a-plane.com
|
$240,000
|
Live Oak, FL | Mar 30, 2026 | — | Active | |
|
William Schretzmann
barnstormers.com
|
$255,000
|
Lake Butler, FL | Apr 22, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 180G
This 1964 Cessna 180G (N411SH) is a 4-seat single engine piston with 4,434 hours on the airframe. This aircraft is listed at the market average at $240,000.
The 180G cruises at 140 kts (259 km/h) with a range of 700 nm (1,296 km) — ideal for short hops and local flights.
Operating costs: Fuel burn is 12 GPH (45 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $66/hr in fuel alone. Total variable cost including maintenance reserves is approximately $155/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $18,000. With 4,434 hours on the airframe, this aircraft has exceeded TBO (2,000 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 180G — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA 180
AeroGurus estimates based on industry averages for the CESSNA 180. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
FAA registration data pending for N411SH.
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 N411SH against the NTSB accident database.
Service Difficulty Reports — Cessna 180G
SDRs are reports filed by mechanics about problems found during maintenance. 8 recent reports for this aircraft type.
(CAN) THE RT RUDDER CABLE FIND CUT IN THE TAIL PULLEY.
(CAN) DURING SCHEDULED MAINTENANCE, IT WAS DISCOVERED THAT P/N 0790006-6 WAS BROKEN DUE TO INTERGRANULAR CORROSION. FLOOR AND ADJACENT STRUCTURES DRILLED APART TO FACILITATE CHANGING THE BRACKET. REASSEMBLED USING EXISTING RIVET SIZE AND PATTERN AS...
AIRCRAFT LOST POWER AFTER TAKEOFF IN CRUISE FLIGHT. THE PILOT WAS IN LOCAL AIRPORT AREA AND GOING TO MAKE 3 TOUCH AND GO'S, AFTER POWER LOST, PILOT LANDED 150 FEET SHORT OF RUNWAY AND NOSED-OVER. INVESTIGATION REVEALED SOME WATER IN GASCOLATOR. TH...
(CAN) FUEL DRIPPING HEAVILY FROM CARBURETOR AFTER ENGINE SHUTDOWN. CARBURETOR REMOVED AND DISASSEMBLED. CARBURETOR FLOAT PONTOON SEPARATED FROM STRUCTURE, IT APPEARS BOTH SUPPORT TANGS RADII ARE TOO SMALL WHICH LEADS TO FAILURE FIRST, LOADING THE S...
DURING CLIMB NEAR TOTAL POWER LOSS. INVESTIGATION FOUND BRACKET AIR FILTER FAULTY DUE TO BOTTOM CHANNEL CAUSES WATER/ICE CONTAMINATION OF ENGINE INTAKE BELLOWS JUST FORWARD OF AIR BOX.
PROP HUB ASSY CRACKED
HUB CORRODED.
(CAN) AFTER ROUTINE CHANGE OVER FROM FLOATS TO SKIS, A FLOAT BOLT WAS CHECKED FOR ITS CONDITION. IT WAS FOUND TO BE CORRODED TO THE POINT WHERE REPLACEMENT WAS DEEMED TO BE NECESSARY. FUTHER INVESTIGATION FOUND SPREADER BAR BOLTS AND LOWER LIFT STRUT...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.