1975 Cessna 414
Multi Engine Piston
Aircraft Details
Seller reportedDescription
Three Owner since new no damage history G600TXi x2 PFD MFD EIS GTN 750 Xi GTN 650 Auto PILOT PA STEC 60-2 Transponder GTX345R GI275 stdby GSR56 IRIDIUM WHEATER RADAR GARMIN GWX75
Inspection
Accomplished 100 hr annual inspection iaw Part 43 Appendix D see PASM work report 25-02-833. Parts replaced :LH Fuel tank aux 4142-3---LH Fuel tank aux 4262-3---Seal 600-0000-10 Qty :5---LH Dry Air Pump RAP442CW---Air filter P128156 Qty :2---Brush Cluster RAB 40189 Qty :2---Seal 630979-9 Qty :24---Oil filter AA48108-2 Qty :2---Oil 15w50 Qty :24qts---O2 botlle 801365-10 sn ON 51976T. Reinstalled GA35 antennas at FS 204.0 & FS 211.3 and GSR56 antenna at FS 169.9 iaw drawing 25091-1& form 8110-3 issued by DERT certicate N°778207227.form 337 completed. AD’s checked trough 2025-20.AD 2000-01-05 exhaust syst corrosion(b,c,d,e)---AD23-03-09 V band coupling. Note :As per TCDS A7CE REV 51 windshields pn 511604-201 & 511604-200 life limit : 13200hr.Time remaining before replacement 10 664.0 hrs Performed engine run up ops chk ok ,no leak. Inspected elt system in this acft according to applicable acft and ELT manufacturers instruction and applicable F.A.A guidance and found that it meets the requirements of section 91.207(d). ELT battery EXPIRE 04/2027 Calibration check FAR 91.411 & 91.413 expire 06/27. I certify that this aircraft has been inspected in accordance with 100 hr annual inspection, was determined to be in airworthy condition and is approved for return to service at this date.
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 |
|---|---|---|---|---|---|---|
|
Calade Air
planecheck.com
|
Call for price
|
France | May 03, 2026 | — | Active | |
|
Listing Source
globalplanesearch.com
|
Call for Price
|
— | Apr 08, 2026 | — | Active | |
|
Camille Junet
controller.com
|
Contact for price
|
Frontenas, Rhône, France | Apr 19, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 414
This 1975 Cessna 414 (N142SD) is a 8-seat multi engine piston with 2,908 hours on the airframe. There are currently 14 414 aircraft listed for sale with asking prices ranging from $119,000 to $642,730.
The 414 cruises at 210 kts (389 km/h) with a range of 1,315 nm (2,435 km) — suitable for regional and medium-distance travel. Service ceiling of 30,200 ft allows operation above most weather.
Operating costs: Fuel burn is 30 GPH (114 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $165/hr in fuel alone. Total variable cost including maintenance reserves is approximately $350/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $30,000. With 2,908 hours on the airframe, this aircraft has exceeded TBO (1,600 hrs) — verify engine status and overhaul reserve.
NTSB records show 0 incidents for this airframe — a clean safety record. There are 6 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 414 — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA 414
AeroGurus estimates based on industry averages for the CESSNA 414. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
FAA registration data pending for N142SD.
Location & Ownership
Aircraft Location
Frontenas, Rhône, France
FR
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 N142SD against the NTSB accident database.
Airworthiness Directives — Cessna 414
ADs are mandatory safety instructions issued by the FAA. 6 recent ADs found for this aircraft type.
The Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, 402B, 402C, 404, 411, 411A, 414, 414A, 421, 421A, 421B, 421C, 425, and 441 Airplanes
View full AD →Cessna Aircraft Company Models T303, 402C, 404, 414A, and 421C Airplanes
View full AD →Source: FAA Airworthiness Directives database. Showing most recent ADs for this aircraft type.
Service Difficulty Reports — Cessna 414
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
DURING A PREFLIGHT WALKAROUND, SURFACE CORROSION WAS OBSERVED ON THE VERTICAL STABILIZER AFT SECTION. AFTER CLOSER INSPECTION SEVERE DELAMINATION WAS SEEN ON THE AFT VERTICAL SUPPORT ANGLES AND AFT STAB BULKHEAD SECTION. THE RUDDER TRIM TAB BRACKET A...
DURING A PREFLIGHT WALK AROUND CORROSION WAS OBSERVED ON THE AFT SPAR ANGLE CHANNEL OF THE VERTICAL STABILIZER. UPON FURTHER INVESTIGATION SIGNIFICANT INTERGRANULAR CORROSION WAS FOUND RESULTING IN EXFOLIATION OF THE SURFACE OT THE SPAR ANGLE. THIS R...
RIGHT FORWARD WINDSHIELD (CESSNA PART NUMBER 5111604-202) BLEW OUT AT ALTITUDE 16,000 DURING CRUISE/KEVEL FLIGHT.
THE LEFT MAIN LANDING GEAR FAILED AS A RESULT OF THE NUT ON THE LEFT TORQUE LINK BOLT FAILED. THE TORQUE LINK SEPERATED AND FAILD TO KEEP THE WHEEL ALIGNED WITH THE AIRCRAFT. RESULTING IN DAMAGE TO AIRCRAFT.
LEFT ALTERNATOR FAIL ANNUNCIATOR LIGHT ILLUMINATED. NO VOLTAGE INDICATION ON LEFT ALTERNATOR. WIRING TERMINALS WERE INTACT AND FIELD VOLTAGE WAS PRESENT. INSPECTION REVEALED THE ALTERNATOR DRIVE SHAFT SHEARED SEPARATING THE DRIVE SHAFT FROM THE ALTER...
AIRCRAFT OWNER REPORTED HISSING SOUND ABOVE CABIN HEADLINER WHEN CABIN OXYGEN CONTROL WAS TURNED ON. PRESSURIZED OXYGEN SYSTEM AND CONFIRMED LOUD HISSING SOUND COMING FROM HEADLINER BETWEEN FIRST ROW OF PASSENGER SEATS. USED BORESCOPE TO INSPECT THE ...
DURING ANNUAL/100 INSPECTION, SURFACE CORROSION WAS OBSERVED NEAR AND ON THE ATTACHMENT SCREWS FOR THE ELEVATOR TRIM TAB HORN (P/N: 0831000-50). CORROSION WAS CLEANED. CRACKS WERE OBSERVED IN THE AFT TWO SCREW HOLES ON THE TOP SURFACE OF THE ELEVATOR...
INSTALLED ENGINE AFTER OVERHAUL. AFTER THIRD START, THE PROPELLER FEATHERED. FOUND OIL TRANSFER COLLAR SPALLED/GROOVED. ENGINE HAD LESS THAN 3 MINUTES TOTAL TIME SINCE OVERHAUL WHEN THE PROPELLER FEATHERED.
SPALLED CAMSHAFT.
LEFT ENGINE HAS SPALLED INTAKE LIFTERS.
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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