1973 Cessna 414
Multi Engine Piston
Equipment & Features
- Seats
- 7
Aircraft Details
Seller reportedAvionics & Equipment
Avionics and autopilot upgrade per EASA Mod. 0060029550-001 PS Engineering PMA8000C Audio Panel
Intercom Marker Beacon Garmin GNS530W NAV-COM-GPS interfaced with Radar System Garmin GNS430W NAV-COM-GPS Garmin G-600 EASA STC.A.S.037679 (Garmin GDU620) with TAWS and Synthetic Vision Radar Display King KI206 Number Two NAV Indicator King KX165A NAV-COM 3 8.33 kHz S-TEC 55X Autopilot with Computerl Transducer Roll/Pitch/Trim Servos Turn and Bank Yaw Damper FAA STC SA8890SW-DLBA Validated Shadin Digidata-L with Fuel Flow Option grandfathered FAA STC SA00729SE-D King KN63 DME
displayed on Garmin G600 King KR87 ADF displayed on Garmin G600 Garmin GTX330 XPDR S Number 1 Garmin GDC74A Encoder King KT73 XPDR S Number 2 ACK A30.4 Encoder Garmin GWX68 Weather Radar displayed on Garmin G600 King KRA10A Radar Altimeter Altitude Alerter integrated in the Garmin G600 L-3 Sky 497 TAS System displayed on Garmin G600 and GArmin GNS530W
connected to ACK A-30.4 Encoder Artex ELT ME406 PN 453-6603406 Mhz Intercom for all Occupants EDM760 Engine Analyzer Astro Tec Digital Clock/Timer Complete Co-Pilot Instrument Panel ASR EPU6A5 Emergency Power Supply Attitude Gyro
Attitude Indiator Vertical Speed Indicator both Airspeed Indicators Fuel Quantity IndicatorManifold Pressure Indicator repaired by Avionitec on 20.09.2013 Main Battery replaced on 20.09.2013 Both Attitude Indicators and Tachometers repaired by Avionitec on 30.03.2015 Radar Antenna GWX68 replaced on 02.11.2016 HSI replaced on 14.12.2018
Description
Cessna 414 RAM 7
Previously registered in Germany as D-ILAY
Two 335 HP RAM Engines!
Pressurized
7 Seats
4 Bladed Propellers
Avionics upgrades
Extended range fuel tanks
Max Takeoff Weight: 6765 Lbs
Empty Weight: 4986.2 Lbs
Fuel Capacity: 238 US Gallons
Engine
Engine Manufacturer: CONTINENTAL Model: TSIO-520-NB, 335 HP, Modified with RAM FAA STC SA4327SW-D Left Hand Serial Number: 813543-R Total Time: 2539:32 TSOH: 473 hrs Right Hand Serial Number: 521667 TSOH: 473 hrs TBO (in hours): 1600 Overhauled in 2013, Installed in September 2013 at Aircraft TT: 3912:10
Interior
7 Seats Light Blue Leather with Grey Carpet Courtesy Table Refreshments Cabinet Condition: 8/10
Exterior
White with blue and silver stripes. Condition: 8/10
Modifications / STCs
• Propeller Synchrophaser
• Oxygen System
• Surface De-Ice
• Alcohol Windshield Anti-Ice
• Air Conditioning provisions, system not installed, two cabin blowers are operative!
• Releaf Tube
• Toilet Potty (Potty not available)
• RAM VII per FAA STC 09469SC-D, EASA STC 10038286 including STC SA3721SW, SE4651SW, SA7984SW-D and SA09469SC-D installed on 20.09.2013 at TT: 3912:10
• LH and RH Aft Wing Locker Tank FAA STC SA2514CE installed 20.09.2013
• Left Factory Nacelle Tank
• Dual Aft Body Strakes FAA STC SA01935LA, installed 30.03.2015
• ASR EPU6A5 Emergency Power Supply
• Vortex Generators
• Rosen Sun Visor FAA STC SA51NM
• LED Taxi Light
• REMARKS
• 20.09.2013 at TT: 3912:10
• Both Windshields Replaced
• Main Landing Gear Torque Tubes Replaced
• Avionics Upgrades
• 22.02.2018 at TT: 4131:42:
• Combustion Heater replaced with new Hartzell Heater
• 27.07.2018 at TT: 4171:41:
• Engine Beams inspection
• Engine Flex Hoses inspection
• Heater Inspection
• Fuel Selector Valve inspection
• Corrosion Program Inspections performed
• A-SID Zone 2 Inspection performed per Gomolzig STC EASA A.S.03328
• 14.12.2018 at TT: 4183:48:
• Seat Belts overhaul by ASF Germany
• Oxygen Bottle overhaul
• Propeller overhaul by MT-Propeller
• 14.12.2018
• Propeller Governors overhauled by MT-Propeller
• Empty Weight: 4986.2 Lbs
• Max Ramp Weight: 6800 Lbs
• MTOW: 6765 Lbs
• Max Landing Weight: 6430 Lbs
• Current FOCA MTOW: 2880 kg
• Nose Baggage Capacity 284 Lbs
• Rear Baggage Compartment Capacity: 100 Lbs
• 338 USG Fuel Capacity
• Swiss Noise Class D
• Noise Level: 82.8 dB(A)
• Last 200 hrs annual inspection completed 14/04/2020 at 4294:40
• ARC Airworthiness Review Inspection due
• Aircraft will be sold with current Annual Inspection and ARC (Airworthiness Review Certificate)
• Engine Manufacturer: CONTINENTAL
• Model: TSIO-520-NB, 335 HP, Modified with RAM FAA STC SA4327SW-D
• Left Hand Serial Number: 813543-R
• Total Time: 2539:32
• TSOH: 473 hrs
• Right Hand Serial Number: 521667
• TSOH: 473 hrs
• TBO (in hours): 1600
• Overhauled in 2013, Installed in September 2013 at Aircraft TT: 3912:10
• Propellers Manufacturer: MT MTV-14-D-F/CF188-30g with CF188-30g Blades 4 Bladed, De-Iced, Swept Composite Blades with Propeller Synchro Phaser
• Manufactured in 2007
• TT: 474:49
• Time Since Overhaul: 201:12 Hours
• Propeller overhaul performed by MT-Propeller
• Specifications subject to verification by purchaser and aircraft subject to withdrawal from the sales at any time without notice
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 |
|---|---|---|---|---|---|---|
|
Stefano Scossa
avbuyer.com
|
$292,151
$292,551
|
— | Mar 16, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 414
This 1973 Cessna 414 (HB-LSX) is a 8-seat multi engine piston . There are currently 13 414 aircraft listed for sale with asking prices ranging from $119,000 to $642,730. This aircraft is priced below the market average at $292,151.
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.
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 registry covers US-registered aircraft (N-numbers).
This aircraft (HB-LSX) 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 database checked for HB-LSX.
Note: NTSB covers US-registered aircraft (N-numbers). This aircraft is registered in a non-US country (HB-LSX). Safety records from the national aviation authority may not be included in our 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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