1966 Cessna 150 G
Single Engine Piston
Aircraft Details
Seller reportedDescription
Cessna 150 G for sale. With Mogas STC complied with. Annual and ARC due in July. Airplane time state: Year: 1966 TTAF: 4500 hr Engine: Continental O-200-A (TBO: 1800, Remaining: 1070) Propeller: McCauley 1A101/DCM6948 (TBO: 2000, Remaining: 1767)
Engine
1 Engine, Piston
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 |
|---|---|---|---|---|---|---|
|
Aviatechnics
planecheck.com
|
$51,925 *
€ 45,000
|
Netherlands | Jun 10, 2026 | — | Active | |
|
Listing Source
globalplanesearch.com
|
Contact for price
|
— | Jun 11, 2026 | — | Active |
* Converted to USD at daily European Central Bank (ECB) exchange rates
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 150 G
This 1966 Cessna 150 G (PH-PHS) is a 2-seat single engine piston .
The 150 G cruises at 97 kts (180 km/h) with a range of 420 nm (778 km) — ideal for short hops and local flights. Service ceiling of 14,000 ft allows operation above most weather.
Operating costs: Fuel burn is 6 GPH (23 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $33/hr in fuel alone. Total variable cost including maintenance reserves is approximately $100/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $15,000.
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 150 G — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA 150
AeroGurus estimates based on industry averages for the CESSNA 150. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
FAA registry covers US-registered aircraft (N-numbers).
This aircraft (PH-PHS) is registered outside the US.
Location & Ownership
Aircraft Location
Location not available
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 PH-PHS against the NTSB accident database.
Service Difficulty Reports — Cessna 150
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
LEFT ELEVATOR SEPARATED IN FLIGHT. BOLT CONNECTING ELEVATOR LOOSENED UP AND FELL OUT. ELEVATOR WAS DAMAGED AND APPEARED TO BE BENT FROM AERODYNAMIC FORCES. AIRCRAFT WAS DIFFICULT TO CONTROL. ANY CONTROL MOVEMENT CAUSED UNCONTROLLABLE PITCHING IN TH...
(CAN) VACUUM COUPLING FAILED. PROBLEM FOUND ON START UP AND FLIGHT ABORTED. REPLACED VACUUM PUMP WITH NEW UNIT. ALL WORK PERFORMED BY MAINTENANCE AND SIGNED OUT IN LOGS.
(CAN) CRACK IN THE INTERIOR OF THE RT MUFFLER FOUND DURING ANNUAL ENGINE INSPECTION. NEW MUFFLER TO BE INSTALLED.
(CAN) AIRCRAFT IN CRUISE FLIGHT. PILOT SAW SMOKE AND SHUT DOWN ELECTRICAL POWER TO AIRCRAFT. AIRCRAFT LANDED WITHOUT INCIDENT. INVESTIGATION FOUND RING TERMINAL LAYING ON CABIN HEAT CONTROL. WIRE TRACED BACK AND FOUND CONNECTED TO AMMETER. THIS W...
ROCKER SHAFT BOSSES FOUND CRACKED WHEN CYLINDER REMOVED DUE TO FAILURE. LAST DYE CHECK WAS DONE IN 5/6/2007 (O/H DATE 1998). CYLINDER ONLY HAD 50 HRS SINCE LAST INSPECTION, BUT 5 YEARS CALENDAR TIME. POSSIBLE MORE FREQUENT DYE CHECK ON ROCKER BOS...
TESTED EIGHT REM38S SPARK PLUGS WITH 200 HRS TT AND FOUND THE RESISTORS HAD FAILED, NO RESISTANCE FOUND THROUGH THE SPARK PLUG.
DURING A PRE-PURCHASE INSPECTION, HEAVY CORROSION WAS FOUND AT THE JOINT BETWEEN THE LT STABILIZER SKIN, PN 0432001-55 AND THE RT STABILIZER SKIN, PN 0432001-54 AT THE LOWER CENTER RIVET LINE WHICH HAD EATEN AWAY NUMEROUS RIVETS, LOOSENED THE SKIN JO...
WINGS WERE PREVIOUSLY REMOVED TO FACILITATE TRANSPORTATION. INSPECTION OF THE LT AND RT FWD SPAR BEARING BLOCKS IN THE FUSELAGE (P/N 0411129) FOUND SEVERE CORROSION DAMAGE. IT APPEARS TO BE DISSIMILAR METAL CORROSION BETWEEN THE SPAR BLOCKS AND THE A...
WINGS WERE PREVIOUSLY REMOVED TO FACILITATE TRANSPORTATION. INSP OF THE LT AND RT FWD SPAR BEARING BLOCKS IN THE FUSELAGE (P/N 0411129) FOUND SEVERE CORROSION DAMAGE. IT APPEARS TO BE DISSIMILAR METAL CORROSION BETWEEN THE SPAR BLOCKS AND THE AN3-21A...
ENGINE HAD BAD HESITATION ON TAKEOFF ACCELERATION. SURGING OCCURRED DURING CLIMB WITH RPM FLUCTUATIONS OF +/- 50-75 RPM. AIRCRAFT AND ENGINE FUEL SCREENS WERE REMOVED AND INSPECTED 3 TIMES IN THE LAST 50 HOURS WITH NO EVIDENCE OF CONTAMINATION. FU...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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