1972 Piper Seneca
Multi Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
NDB-DME) operation. Within the US National Airspace System in accordance with AC 20-138 & such countries where GPS enroute
terminal & non-precision approaches are authorized by the appropriate airworthiness authority. WX900 Stormscope
Copilot instruments Airspeed Attitude Indicator Altimeter VOR/GS DG Day/Night IFR Category 1 B-RNAV (RNP 5). OptionsLightweight Surface Pneumatic De-icing system & propeller electrothermal de-icing system
Windshield hot platePitot & stall warning heating system protected by landing gear switch Propellers with dampers Electric pitch trim installation
Logo light Currently removedhoses still present with covers installed Additional FOCA Approved documentation for 98 USG fuel tank for ferry flights. Increased MTOW approved for 4560 Lbs Remaining Useful Load with full tanks & ferry tank: 453.45 Lbs FERRY TANK NOT AVAILABLE.
InteriorBlue vinyle 9/10 Gray fabric seats 9/10 Pilot & Copilot Adjustable seats Blue carpet 9/10
Exterior Light gray with maroon stripes 7/10 RemarksIn good conditions. Landing accident with one main gear collapse and wing spar repair in performed in 1991 at TT: 6557 Missing logs from 1972 to 1981
Prior to Swiss registration. Replaced fuel tank vent line hoses 12/07.Description
Airframe
Serial Number: TBD
TT: 9,881
Engine
LH: Textron-Lycoming IO-360-C1E6
SN: L-1118-51A
TT: 10251
Propeller
LH: 2 Bladed Hartzell CH-C2YK-2CGUF
SN: AU13103
TT: 5737
Time Since Overhaul: 144:25 hrs Overhauled with New improved hubs in July. 2007
Avionics
IFR, PS Engineering audio panel with intercom and marker beacon, 1 x Garmin GNS530 WAAS 8.33 kHz 1 x King KX125 COM 760 Ch, FM Immune, KN72 NAV, KCS55 HSI, KR85 ADF with RMI, KN62A DME, ME406 ELT, King KT79 Mode “S” XPDR, ACK A30 Encoder, Autocontr III Autopilot 3 axis coupled to HSI & VOR, GPS approved for VFR/IFR enroute, B-RNAV, terminal & instrument approach (GPS, VOR, VOR-DME, NDB, NDB-DME) operation. Within the US National Airspace System in accordance with AC 20-138 & such countries where GPS enroute, terminal & non-precision approaches are authorized by the appropriate airworthiness authority. WX900 Stormscope, Copilot instruments Airspeed, Attitude Indicator, Altimeter, VOR/GS, DG Day/Night, IFR Category 1, B-RNAV (RNP 5).
Options
Lightweight Surface Pneumatic De-icing system & propeller electrothermal de-icing system, Windshield hot plate, Pitot & stall warning heating system protected by landing gear switch Propellers with dampers Electric pitch trim installation, Logo light, Currently removed, hoses still present with covers installed Additional FOCA Approved documentation for 98 USG fuel tank for ferry flights. Increased MTOW approved for 4560 Lbs Remaining Useful Load with full tanks & ferry tank: 453.45 Lbs FERRY TANK NOT AVAILABLE.
Interior
Blue vinyle 9/10 Gray fabric seats 9/10 Pilot & Copilot Adjustable seats Blue carpet 9/10
Exterior
Light gray with maroon stripes 7/10
Remarks
In good conditions. Landing accident with one main gear collapse and wing spar repair in performed in 1991 at TT: 6557 Missing logs from 1972 to 1981, Prior to Swiss registration. Replaced fuel tank vent line hoses 12/07.
Engine
LH: Textron-Lycoming IO-360-C1E6 SN: L-1118-51A TT: 10251 Propeller LH: 2 Bladed Hartzell CH-C2YK-2CGUF SN: AU13103 TT: 5737 Time Since Overhaul: 144:25 hrs Overhauled with New improved hubs in July. 2007 Avionics IFR, PS Engineering audio panel with intercom and marker beacon, 1 x Garmin GNS530 WAAS 8.33 kHz 1 x King KX125 COM 760 Ch, FM Immune, KN72 NAV, KCS55 HSI, KR85 ADF with RMI, KN62A DME, ME406 ELT, King KT79 Mode “S” XPDR, ACK A30 Encoder, Autocontr III Autopilot 3 axis coupled to HSI & VOR, GPS approved for VFR/IFR enroute, B-RNAV, terminal & instrument approach (GPS, VOR, VOR-DME, NDB, NDB-DME) operation. Within the US National Airspace System in accordance with AC 20-138 & such countries where GPS enroute, terminal & non-precision approaches are authorized by the appropriate airworthiness authority. WX900 Stormscope, Copilot instruments Airspeed, Attitude Indicator, Altimeter, VOR/GS, DG Day/Night, IFR Category 1, B-RNAV (RNP 5). Options Lightweight Surface Pneumatic De-icing system & propeller electrothermal de-icing system, Windshield hot plate, Pitot & stall warning heating system protected by landing gear switch Propellers with dampers Electric pitch trim installation, Logo light, Currently removed, hoses still present with covers installed Additional FOCA Approved documentation for 98 USG fuel tank for ferry flights. Increased MTOW approved for 4560 Lbs Remaining Useful Load with full tanks & ferry tank: 453.45 Lbs FERRY TANK NOT AVAILABLE. Interior Blue vinyle 9/10 Gray fabric seats 9/10 Pilot & Copilot Adjustable seats Blue carpet 9/10 Exterior Light gray with maroon stripes 7/10 Remarks In good conditions. Landing accident with one main gear collapse and wing spar repair in performed in 1991 at TT: 6557 Missing logs from 1972 to 1981, Prior to Swiss registration. Replaced fuel tank vent line hoses 12/07.
Interior
Blue vinyle 9/10 Gray fabric seats 9/10 Pilot & Copilot Adjustable seats Blue carpet 9/10 Exterior Light gray with maroon stripes 7/10 Remarks In good conditions. Landing accident with one main gear collapse and wing spar repair in performed in 1991 at TT: 6557 Missing logs from 1972 to 1981, Prior to Swiss registration. Replaced fuel tank vent line hoses 12/07.
Exterior
Light gray with maroon stripes 7/10 Remarks In good conditions. Landing accident with one main gear collapse and wing spar repair in performed in 1991 at TT: 6557 Missing logs from 1972 to 1981, Prior to Swiss registration. Replaced fuel tank vent line hoses 12/07.
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
avpay.aero
|
Contact for Price
|
Switzerland | Apr 05, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Piper Seneca
This 1972 Piper Seneca is a 6-seat multi engine piston with 9,881 hours on the airframe. There are currently 112 Seneca aircraft listed for sale with asking prices ranging from $53,000 to $875,612.
The Seneca cruises at 180 kts (333 km/h) with a range of 750 nm (1,389 km) — ideal for short hops and local flights. Service ceiling of 25,000 ft allows operation above most weather.
Operating costs: Fuel burn is 22 GPH (83 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $121/hr in fuel alone. Total variable cost including maintenance reserves is approximately $280/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $25,000. With 9,881 hours on the airframe, this aircraft has exceeded TBO (1,800 hrs) — verify engine status and overhaul reserve.
NTSB records show 0 incidents for this airframe — a clean safety record.
Pre-Purchase Checklist
Piper Seneca — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimatePIPER Seneca
AeroGurus estimates based on industry averages for the PIPER Seneca. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
Registration number not available.
Location & Ownership
Aircraft Location
Switzerland
CH
Seller reportedTitle 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.
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