1983 Cessna 414A
Multi Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
IFRAVIONICS: Garmin G700 Txi 'Touchscreen' Primary Flight Display with Moving Map Display Garmin GMA-340 Audio Panel w/ 3-Light Marker Beacons Voice Activated Intercom Garmin GNS-530W WAAS IFR-Certified GPS-Com w/ ILS
LPVLarge Color Moving Map Terrain Avoidance Garmin GNS-430W WAAS IFR-Certified GPS-Com #2 w/ ILS
LPVColor Moving Map Terrain Avoidance Avidyne EX600 Multi-Function Display L3Harris ESI-500 Electronic Standby Instrument System King KN-64 Digital DME Garmin GTX-335 Digital Mode-S Transponder #1 w/ ADS-B Out Garmin GTX-327 Digital Transponder #2 STEC 3100 Digital Autopilot w/ Hdg Nav Tracking
GPSS Approach Mode Vertical Speed Go-Around Mode Flight DirectorAltitude Pre-Select Altitude Hold ADDITIONAL EQUIPMENT: Factory 'FIKI' Certified
Certified for Flight Into Known Icing conditions ! Air-Conditioning De-Ice Boots
Hot Prop and Heated Windshield JPI EDM-790 Twin Digital Engine Monitor System w/ TIT
EGT's CHT'setc. Shadin DigiFlo-L Digital Twin Engine Fuel Flow Computer Polished Prop Spinners Dual Executive Writing Tables with woodgrain veneer Aft Potty Seat with seat cushions seatbelt. Aft Refreshment Center with woodgrain veneer. Wing Storage Lockers. Nose Aft Baggage Compartments Forward Cabin/Cockpit Divider Bulkhead with woodgrain veneer finish
Description
Well-equipped RAM IV Chancellor with Winglets, Strakes, VG's, RAM IV Engine Prop upgrades, FIKI certified, A/C, G700Txi PFD,STEC 3100 AP, GNS-530W, GNS-430W, GMA-340, GTX-335, GTX-327, ESI-500 Backup Instrumentation, Co-Pilot Instruments, JPI EDM-790, Shadin Dig FF, and excellent maintenance history.
Engine
ENGINE 1: Only '8' hours since Complete Major Overhaul to New Parts Limits on RAM 325-Horsepower Turbocharged Engine / RAM IV STC'd engine upgrade Make: Continental / Model: TSIO-520-NB / Serial #: Factory recommended TBO is 1,600 hours. ENGINE 2: 600 hours since Major Overhaul on RAM 325-Horsepower Turbocharged Engine / RAM IV STC'd engine upgrade Make: Continental / Model: TSIO-520-NB / Serial #: 519209 Factory recommended TBO is 1,600 hours. PROPELLER 1 2: 600 hours on Hartzell 3-Blade Constant Speed Hot Props w/ Unfeathering Accumulators Make: Hartzell / Model: PHC-C3YF-2UF MODS: RAM IV Engine Conversion with 325 Horsepower TSIO-520-NB Engines Winglets Vortex Generators Strakes
Propeller
10,550 Hours Total Time
Interior
Beige leather upholstery with Dark Red leather upper seatback inserts. Matching Beige leather sidepanels. Cream interior window trim headliner. Beige carpeting. Rated 8.
Exterior
White w/ Red trim and Black accent striping. Rated 7 to 8.
Description and equipment details provided by the seller. AeroGurus does not verify seller-provided information.
Price Comparison Listed on multiple marketplaces
| Source | Price | Location | Listed | Days on Market | Status | Action |
|---|---|---|---|---|---|---|
|
Dan Howard Aircraft Sales
trade-a-plane.com
|
Contact for Price
|
Tulsa, OK | Jun 26, 2026 | 22 days | Active | |
|
Listing Source
globalplanesearch.com
|
Contact for price
|
OK | Jul 15, 2026 | 2 days | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 414A
This 1983 Cessna 414A (N569PA) is a 8-seat multi engine piston with 10,550 hours on the airframe. There are currently 29 414A aircraft listed for sale with asking prices ranging from $279,310 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. Service ceiling of 30,200 ft allows operation above most weather.
Operating costs: Fuel burn is 30 GPH (114 L/h), which at current 100LL avgas prices (~$6.20/gal) means approximately $186/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 10,550 hours on the airframe, this aircraft has exceeded TBO (1,400 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
FAA registration data pending for N569PA.
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 N569PA against the NTSB accident database.
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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