£414,909
Aircraft Location:Schwabmünchen, Bavaria, Germany
Seller Information
View Seller InformationGeneral
Year
1979
Manufacturer
Model
Serial Number
414A0420
Registration #
PH-SWN
Condition
Used
FlightRules
IFR
Description
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.
Airframe
Total Time
3,750
Basic Empty Weight
2,275 kg
Airframe
Make / Model: Cessna 414A RAM IV
Year: 1979
Serial Number: 414A0420
Total Time: 3750 h TT
Weights & Balance
BEM 2275 kg
Payload 946 kg
Max fuel 780 liter Avgas 100LL
Engine 1
Engine 1 Make/Model
CONTINENTAL TSIO520NB
Engine 1 Horsepower
239.04 kW
Engine 1 Time
305 SMOH
Engine 1 TBO
1600
Year Engine 1 Overhauled or Installed as New
2014
Engine Specs
Continental TSIO-520-NB, rated at 325 hp
TBO 1600 hr or 12 years recommended
L/H 305 SMOH compl. in 10/2014
leak test 66 / 62 / 74 / 72 / 72 / 72 of 80 psi
R/H 305 SMOH compl. in 10/2014
leak test 74 / 68 / 66 / 72 / 72 / 70 of 80 psi
Engine 2
Engine 2 Make/Model
CONTINENTAL TSIO520NB
Engine 2 Horsepower
239.04 kW
Engine 2 Time
305 SMOH
Engine 2 TBO
1600
Year Engine 2 Overhauled or Installed as New
2014
Engine 2 Notes
Continental TSIO-520-NB, rated at 325 hp
TBO 1600 hr or 12 years recommended
L/H 305 SMOH compl. in 10/2014
leak test 66 / 62 / 74 / 72 / 72 / 72 of 80 psi
R/H 305 SMOH compl. in 10/2014
leak test 74 / 68 / 66 / 72 / 72 / 70 of 80 psi
Props
Prop 1 Manufacturer
HARTZELL
Prop 1 Model
PHC-C3YF-2UF
Prop 1 Time
143 SOH
Prop 2 Manufacturer
HARTZELL
Prop 2 Model
PHC-C3YF-2UF
Prop 2 Time
143 SOH
Number of Blades
3
Prop Specs
Hartzell PHC-C3YF-2UF/FC7663, 3-blade
TBO 2400 hr or 6 years recommended
L/H 143 SPOH compl. in 11/2020
R/H 143 SPOH compl. in 11/2020
Avionics
Flight Deck Manufacturer/Model
GARMIN G600 TXI
Avionics/Radios
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
Additional Equipment
Additional Equipment
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
Exterior
Exterior Notes
All over White with Red stripes (6 of 10)
Interior
Interior Notes
Light Brown leather interior in good condition (7 of 10)
Inspection Status
Inspection Status
Annual: April
Maintenance: In July 2023, the aircraft underwent a major maintenance event including structural and system inspections as well as the completion of an extensive Garmin avionics upgrade, with all work found satisfactory.
The Airworthiness Review Certificate received its second extension at a recorded total time of 3,733:31 hours and is valid until 11. April 2026 (will be prolonged in time).
In December 2025, a new heated front windshield on the pilot’s side was installed.
Airworthy
Yes

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