1956 Cessna 180
Single Engine Piston
Aircraft Details
Seller reportedDescription
Detailed Description 1956 CESSNA, 180 • $159,000 • AVAILABLE FOR SALE • 1956 Cessna 180, total air time 2320, engine 896, prop 13.8 hours after overhaul. Aircraft will be sold with a fresh annual inspection. Classic IFR aircraft. Interior red leather 9 out of 10, exterior paint excellent 9 out of 10. Have owned this aircraft for the last 36 years. Aircraft has been kept in a hanger its whole life and owned by a retired airline pilot. It has an STC for unleaded car gas no aircraft damage located in South Florida. • Contact Mike Vucetic, Owner - located Coral Springs, FL 33067 United States • Tele
Interior
red leather 9 out of 10,
Exterior
paint excellent 9 out of 10
Inspection
fresh annual inspection. Classic IFR aircraft. Interior
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 |
|---|---|---|---|---|---|---|
|
Mike Vucetic
trade-a-plane.com
|
Contact for Price
|
Coral Springs, FL | Mar 30, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 180
This 1956 Cessna 180 (N4935A) is a 4-seat single engine piston with 2,320 hours on the airframe. There are currently 29 180 aircraft listed for sale with asking prices ranging from $120,000 to $399,000.
The 180 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 2,320 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. There are 9 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 180 — 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 N4935A.
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 N4935A against the NTSB accident database.
Airworthiness Directives — Cessna 180
ADs are mandatory safety instructions issued by the FAA. 9 recent ADs found for this aircraft type.
Cessna Aircraft Company 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 206, P206, U206, TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 Series Airplanes
View full AD →Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190, 195, 206, 207, 210, T303, 336, and 337 Airplanes
View full AD →Cessna Aircraft Company (Cessna) 172, 175, 177, 180, 182, 185, 206, 207, 208, 210, 303, 336, and 337 Series Airplanes
View full AD →Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series Airplanes
View full AD →Cessna Aircraft Company 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 206, P206, U206, TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 Series Airplanes
View full AD →Cessna Aircraft Company 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 206, P206, U206, TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 Series Airplanes
View full AD →Cessna Aircraft Company 150, 152, 172, 177, 180, 182, 185, 188, 206, 207, 210, and 337 Series Airplanes
View full AD →Source: FAA Airworthiness Directives database. Showing most recent ADs for this aircraft type.
Service Difficulty Reports — Cessna 180
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
SUPERIOR PISTON ASSY PART # SA640518 INSTALLED. WITHIN 40 HOURS OF INSTALLATION PISTON DISINTEGRATED RESULTING IN EXTREME VIBRATION. ENGINE WAS SHUTDOWN AND LANDING MADE IN FIELD WITHOUT INCIDENT.
ENGINE STARTED RUNNING ROUGH AT TOD AND STOPPED PRODUCING POWER SHORTLY AFTER. AN EMERGENCY LANDING WAS MADE ON TUNDRA WITH NO DAMAGE. FUEL SUMPS AND GASCOLATOR WERE FOUND TO HAVE WHAT LOOKED LIKE "COTTON OR FILTER LIKE MATERIAL" WHICH WE BELIEVE WAS...
FRAYING FOUND ON ALL THREE AILERON CONTROL CABLES AT FUSELAGE UPPER AFT CABIN PULLIES. NOTE: AIRCRAFT WAS MODIFIED BY ROBERTSON R/STOL HIGH LIFT SAFETY AND PERFORMANCE SYSTEM STC SA1435WE 20/21/1994.
LOSS OF ELECTRICAL POWER IN FLIGHT. REWIRED ELECTRICAL CONNECTIONS ON GENERATOR AND TEST RAN ENGINE.
AFTER TOUCHDOWN A WIND GUST CAUSED THE AIRCRAFT TO BECOME AIRBORNE AGAIN. RETURNED TO THE GROUND AT A SLIGHT ANGLE AND AS THE PILOT STRAIGHTENED THE AIRCRAFT DOWN THE RUNWAY THE LT WHEEL AXLE BROKE & TIRE ASSEMBLY ROLLED DOWN RUNWAY. VEERED RT OF ...
DURING FUNCTIONAL CHECK, FOUND CABLE ASSEMBLY COMPLETELY BROKEN. THIS CABLE PART OF CESSNA SK210-174A. PN 505530-405. INVESTIGATION ON THE INTERNET ( YEAH, I KNOW...THE INTERNET) MAKES IT APPEAR TO BE A COMMON PROBLEM.
PISTON IN LH BRAKE CALIPER LOCKED IN PLACE CAUSING THE BRAKE TO DRAG, PILOT ABORTED TAKE OFF TO CHECK BRAKES. WE BELIEVE THIS WAS CAUSED BY WORN BRAKE PADS. NO EMERGENCY MEASURES TAKEN. NO SBS, ADS, ICAS OR STCS APPLY. BRAKE PADS WERE WITHIN TOLERANC...
(CAN) DURING ANNUAL INSPECTION, LEFT FUSELAGE TUNNEL BULKHEAD FOUND CHAFED BY LEFT RUDDER RETURN SPRING ARM DUE TO INADEQUATE CLEARANCE. NO INDICATION OF PREVIOUS DAMAGE OR INCORRECT REPAIR WHICH WOULD CAUSE INADEQUATE CLEARANCE. SPRING FOUND INSTALL...
THROTTLE DISCONNECTED IN FLIGHT. THROTTLE FAILED TO WIDE OPEN THROTTLE CONDITION, PILOT USED MIXTURE TO CONTROL ENGINE POWER OUTPUT AND MADE SUCCESSFUL LANDING WITHOUT INCIDENT. MECHANIC FOUND THAT AN AN4-35A UNDRILLED BOLT WAS INSTALLED IN THE THR...
STAB HINGE BOXES DAMAGED. REPLACED BOTH STABILIZER HINGE REINFORCEMENT BOXES.
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.