1978 Cessna 414A
Multi Engine Piston
Aircraft Details
Seller reportedDescription
Beautifully equipped, pressurized twin with RAM VII engines, full de-ice, updated avionics, and executive interior.
Engine
Continental TSIO-520-NB 335 H.P. RAM VII SMOH: 1,125 / 1,125 (02/2016 - RAM)
Propeller
3 Bladed Heated McCauley 3AF32C515 w/ Prop Synch SN: 002024 / 002030 SPOH: 1,125 / 1,125 (02/2016)
Interior
Executive Configuration in Light Gray Leather Seating, Dual Writing Tables, Factory Installed Freon Air Conditioning, Aft Belted Side Facing Lav & Aft Refreshment Center.
Exterior
Overall White w/Blue, Gray & Red Accents.
Inspection
Annual c/w 2/01/2025
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 |
|---|---|---|---|---|---|---|
|
Listing Source
globalair.com
|
Contact for price
|
OK | Mar 13, 2026 | 2 days | Active | |
|
International Aircraft Marketing & Sales
controlleremea.co.uk
|
Call for price *
|
Oklahoma City, OK | Apr 04, 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 414A
This 1978 Cessna 414A is a 8-seat multi engine piston with 7,002 hours on the airframe. There are currently 27 414A aircraft listed for sale with asking prices ranging from $329,000 to $739,500.
The 414A cruises at 210 kts (389 km/h) with a range of 1,315 nm (2,435 km) — suitable for regional and medium-distance travel.
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 7,002 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 414A — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA 414A
AeroGurus estimates based on industry averages for the CESSNA 414A. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
Registration number not available.
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 database checked for this aircraft.
Airworthiness Directives — Cessna 414A
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 414A
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
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...
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.
LEFT ENGINE HAS SPALLED EXHAUST LIFTERS.
RIGHT ENGINE HAS SPALLED CAMSHAFT.
FOUND SPALLED INTAKE LIFTER ON RIGHT HAND ENGINE.
FOUND SPALLED EXHAUST LIFTER ON RIGHT HAND ENGINE.
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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