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.Specifications
Year1979
ManufacturerCESSNA
Model414A
Serial Number414A0420
Registration #PH-SWN
ConditionUsed
FlightRulesIFR
Total Time3,755
Basic Empty Weight5,015.52 lb
Airframe NotesMake / 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
Engine 1 Make/ModelCONTINENTAL TSIO520NB
Engine 1 Horsepower320.55 HP
Engine 1 Time310 SMOH
Engine 1 TBO1600
Year Engine 1 Overhauled or Installed as New2014
Engine 1 NotesContinental 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
Engine 2 Make/ModelCONTINENTAL TSIO520NB
Engine 2 Horsepower320.55 HP
Engine 2 Time310 SMOH
Engine 2 TBO1600
Year Engine 2 Overhauled or Installed as New2014
Engine 2 NotesContinental 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
Prop 1 ManufacturerHARTZELL
Prop 1 ModelPHC-C3YF-2UF
Prop 1 Time148 SOH
Prop 2 ManufacturerHARTZELL
Prop 2 ModelPHC-C3YF-2UF
Prop 2 Time148 SOH
Number of Blades3
Prop NotesHartzell 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
Flight Deck Manufacturer/ModelGARMIN G600 TXI
Avionics/RadiosPFD: 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 EquipmentLED 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 NotesAll over White with Red stripes (6 of 10)
Interior NotesLight Brown leather interior in good condition (7 of 10)
Inspection StatusAnnual: 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.
AirworthyYes
Year1979|
ManufacturerCESSNA|
Model414A|
Serial Number414A0420|
Registration #PH-SWN|
ConditionUsed|
FlightRulesIFR|
Total Time3,755|
Basic Empty Weight5,015.52 lb|
Airframe NotesMake / 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|
Engine 1 Make/ModelCONTINENTAL TSIO520NB |
Engine 1 Horsepower320.55 HP|
Engine 1 Time310 SMOH |
Engine 1 TBO1600|
Year Engine 1 Overhauled or Installed as New2014|
Engine 1 NotesContinental 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|
Engine 2 Make/ModelCONTINENTAL TSIO520NB |
Engine 2 Horsepower320.55 HP|
Engine 2 Time310 SMOH |
Engine 2 TBO1600|
Year Engine 2 Overhauled or Installed as New2014|
Engine 2 NotesContinental 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|
Prop 1 ManufacturerHARTZELL|
Prop 1 ModelPHC-C3YF-2UF|
Prop 1 Time148 SOH |
Prop 2 ManufacturerHARTZELL|
Prop 2 ModelPHC-C3YF-2UF|
Prop 2 Time148 SOH |
Number of Blades3|
Prop NotesHartzell 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|
Flight Deck Manufacturer/ModelGARMIN G600 TXI |
Avionics/RadiosPFD: 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 EquipmentLED 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 NotesAll over White with Red stripes (6 of 10)|
Interior NotesLight Brown leather interior in good condition (7 of 10)|
Inspection StatusAnnual: 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.|
AirworthyYes|
