1969 Cessna 182 M
Single Engine Piston
FOR SALEAircraft Details
Seller reportedAvionics & Equipment
Description
Nice looking aircraft, maintained by Cessna service center, full history from new. Previous registrations OY-AGR, SE-LDF, LN-HIH.
Fresh ARC in March 2026. Aircraft is constantly flying so time will build. VAT free, delivery possible.
Interior
8/10 red carpet, gray leather seats
Exterior
9/10 good paint, always in hangar, no corrosion
Modifications / STCs
• Tanis engine heater, wings and canopy covers, 5th seat, long range tanks
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 |
|---|---|---|---|---|---|---|
|
Aeroservisas
planecheck.com
|
$149,073 *
€ 127,000
|
Lithuania | May 03, 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 182 M
This 1969 Cessna 182 M (LY- LTB) is a 4-seat single engine piston with 6,290 hours on the airframe. This aircraft is listed at the market average at $149,073.
The 182 M cruises at 140 kts (259 km/h) with a range of 915 nm (1,695 km) — ideal for short hops and local flights. Service ceiling of 18,100 ft allows operation above most weather.
Operating costs: Fuel burn is 12.5 GPH (47 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $69/hr in fuel alone. Total variable cost including maintenance reserves is approximately $160/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $20,000. With 6,290 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 1 airworthiness directive 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 182 M — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA 182
AeroGurus estimates based on industry averages for the CESSNA 182. 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 (LY- LTB) is registered outside the US.
Location & Ownership
Aircraft Location
Lithuania
LT
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 LY- LTB against the NTSB accident database.
Airworthiness Directives — Cessna 182
ADs are mandatory safety instructions issued by the FAA. 1 recent AD found for this aircraft type.
Cessna Aircraft Company Models 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, and 182R Airplanes
View full AD →Source: FAA Airworthiness Directives database. Showing most recent ADs for this aircraft type.
Service Difficulty Reports — Cessna 182
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
AIRCRAFT IS EQUIPPED WITH AN AIRWOLF REMOTE OIL FILTER ADAPTER MOUNTED ON THE FIREWALL. A TEMPEST EZ TURN OIL FILTER PART # AA48109-1 WAS INSTALLED AT THE LAST OIL CHANGE AND INSTALLED WITHOUT THE USE OF DOW CORNING DC4 LUBRICANT ON THE SEAL AS DIREC...
FLAP OPERATION INTERMITTENT. FOUND PREVIOUSLY INSTALLED CONTROL CABLE (P/N S1244-20) BINDING AT CABLE CLAMP, AT FLAP ACTUATOR. FOUND CABLE IN OTHER AIRFRAMES HAVE CABLE PROTECTION FOR CLAMP, ELIMINATING INNER CABLE RESTRICTION. SOLICITED MCFARLAND AV...
FLAP OPERATION INTERMITTENT. FOUND PREVIOUSLY INSTALLED CONTROL CABLE (P/N S1244-20) BINDING AT CABLE CLAMP, AT FLAP ACTUATOR. FOUND CABLE IN OTHER AIRFRAMES HAVE CABLE PROTECTION FOR CLAMP, ELIMINATING INNER CABLE RESTRICTION. SOLICITED TO MANUFACTU...
CRACKS WERE FOUND IN THE AFT BULKHEAD AND ALL FIVE VERTICAL FIN ATTACHMENT BOLTS WERE FOUND LOOSE. THIS WAS CAUSED BY THE AFT BULKHEAD BEING UNDER DESIGNED.
ELT FAILED OPS CHECK. REMOVAL AND INSPECTION REVEALED 2 D CELL BATTERIES LEAKING PROFUSELY. UNIT WAS CLEANED AND INSPECTED AND ALL CELLS WERE REPLACED, EXPIRATION DATES WERE 2017. BATTERY EXPIRATION DATES WERE ALL 2019. 6 (SIX) MONTHS LATER THE E...
NUMBER 5 CYLINDER ON O-470 ENGINE WITH APPROXIMATELY 300 HOURS EXPERIENCED PISTON FAILURE DUE TO WHAT APPEARS AT FIRST IMPRESSION DETONATION. HOWEVER, PISTON IS BELIEVE TO HAVE FAILED DUE TO FLAW IN MANUFACTURE OR EXPERIENCE DAMAGE SUCH AS DROPPING P...
WHILE PERFORMING A VISUAL INSP OF THE AFT FUSELAGE BULKHEAD IAW AD 72-07-09; DISCOVERED CRACKS IN THE AFT BULKHEAD BETWEEN THE RUDDER CABLE CUTOUT AND THE BULKHEAD FLANGE (BOTH SIDES). FOLLOWING THE INSTRUCTIONS IN THE AD, PERFORMED A TORQUE CHECK ...
ON INSPECTION BOTH FLAPS RT AND LT TOP AND BOTTOM FLAP SKINS WERE CRACKED 6 TO 8 INCHES ALONG THE T/E, ON THE RIVET LINE. ALSO SHEERED RIVETS ON (3) OF THE (4) FLAP TRACK LOWER TRACK TO RIBS. RESKINNED FLAPS AND INSTALLED MS21042 STEEL SCREWS IN RE...
RESEALED FUEL SELECTOR VALVE PN 0716613-1 AND DURING A LEAK TEST LEAKAGE WAS FOUND FROM ONE OF THE PN 1216107-4 SEALS. INVESTIGATION FOUND THAT THE SEAL FACE WAS DEFORMED AND THAT MOLD LINES FROM THE INJECTION MOLDING PROCESS CAUSED VOIDS IN THE SEAL...
PILOT COMPLAINED THAT THE PROPELLER CONTROL WAS HARD TO MOVE. WHEN TECHNICIAN INVESTIGATED, THE CONTROL CABLE BROKE AND CAME OFF IN TECHNICIAN`S HAND. REMOVED AND REPLACED CONTROL WITH NEW PART.
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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