1979 CESSNA 414A

1979

414A0420

PH-SWN

Occasion

IFR

History: Manufacturing of this Cessna 414A RAM IV, serial number 414A0420, was completed on 26 October 1979. For testing and approval, it was registered in the United States as N2692Y by Cessna. Shortly after production, the aircraft was registered as D-IAAQ and ferried to Germany, where it was operated by two different private owners. On 28 February 2002, it was transferred to the Netherlands and registered as PH-SWN. The aircraft remained on the Dutch register, changing ownership in 2014. Since 10 September 2021, the aircraft has been owned by its current German owner, who continues to operate the aircraft under the registration PH-SWN. Damage History: no known damage history Aircraft Subject to Prior Sale or Removal from Market without Notice. Specification Subject to Verification by Purchaser.

3,755

2,275 kg

Make / Model: Cessna 414A RAM IV Year: 1979 Serial Number: 414A0420 Total Time: 3755 h TT Weights & Balance BEM 2275 kg Payload 946 kg Max fuel 780 liter Avgas 100LL

CONTINENTAL TSIO520NB

239.04 kW

310 SMOH

1600

2014

Continental TSIO-520-NB, rated at 325 hp TBO 1600 hr or 12 years recommended L/H 310 SMOH compl. in 10/2014 leak test 66 / 62 / 74 / 72 / 72 / 72 of 80 psi R/H 310 SMOH compl. in 10/2014 leak test 74 / 68 / 66 / 72 / 72 / 70 of 80 psi

CONTINENTAL TSIO520NB

239.04 kW

310 SMOH

1600

2014

Continental TSIO-520-NB, rated at 325 hp TBO 1600 hr or 12 years recommended L/H 310 SMOH compl. in 10/2014 leak test 66 / 62 / 74 / 72 / 72 / 72 of 80 psi R/H 310 SMOH compl. in 10/2014 leak test 74 / 68 / 66 / 72 / 72 / 70 of 80 psi

HARTZELL

PHC-C3YF-2UF

148 SOH

HARTZELL

PHC-C3YF-2UF

148 SOH

3

Hartzell PHC-C3YF-2UF/FC7663, 3-blade TBO 2400 hr or 6 years recommended L/H 148 SPOH compl. in 11/2020 R/H 148 SPOH compl. in 11/2020

GARMIN G600 TXI

PFD: Garmin dual G600TXi COM/NAV/GPS: Garmin GTN-750Xi COM/NAV/GPS: Garmin GTN-650Xi Autopilot: Garmin GFC-600 (4-axis) Control Panel: Garmin GCU-485 Transponder (ADS-B in/Out): Garmin GTX-345R Transponder Mode S: Garmin GTX-330E Standby PFD: Garmin GI-275 Engine Interface: Garmin dual GEA-110 Weather Radar: Garmin GWX-75 Audio Panel: Garmin GMA-35 (remote) Bluetooth/WiFi: Garmin FlightStream-510 USB Power: Garmin GSB-15 (dual USD-C) Radar Altimeter: Sperry RA-215 DME: King KN-63 ADF: King KR-87

LED Landing- and Taxi-lights LED Position & Strobe Lights Rosen sun visors New heated glass windshield (pilot side) Vortex Generators Prop Sync ELT Q-Tip propellers (de-iced) FIKI certified RAM IV engines Gear Mirror at lh cowling Cabin intercom system Oxygen system (11 cu.ft. cylinder) Boots

All over White with Red stripes (6 of 10)

Light Brown leather interior in good condition (7 of 10)

Annual: June Maintenance: In June 2026, an extensive scheduled maintenance event was completed at 3,752:22 hours total time. The work included the 100-hour, 200-hour, 600-hour and 12-month inspections, together with comprehensive inspections of the airframe, wing structure, landing gear, engines, propellers, avionics and aircraft systems. Both engines underwent cylinder borescope inspections, differential compression tests, oil and filter changes, exhaust system inspections, crankshaft corrosion inspections, magneto inspections and checks of the RAM induction, fuel injection and turbocharger systems. The right-hand fuel metering unit and the hydraulic emergency blowdown bottle were replaced. Current oil analysis results for both engines indicate no abnormal wear. The Airworthiness Review Certificate is valid until 26 May 2027.

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