1972 Piper PA34 Seneca I Multi EngineFor Sale
FOR SALE

1972 Piper PA34 Seneca I Multi EngineFor Sale

Multi Engine Piston

Contact for price
Total Time 9,881 hrs

Equipment & Features

Seats
6
✓ Clean NTSB ✓ Verified recently

Aircraft Details

Seller reported

Avionics & Equipment

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.

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 Action
Stefano Scossa
avpay.aero
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AeroGurus Data & Analysis

Independent data from FAA, NTSB, and market analysis

About This Piper PA34 Seneca I Multi EngineFor Sale

This 1972 Piper PA34 Seneca I Multi EngineFor Sale is a multi engine piston with 9,881 hours on the airframe.

NTSB records show 0 incidents for this airframe — a clean safety record.

Pre-Purchase Checklist

Safety record: 0 NTSB incidents
Airframe: 9,881 hours
Budget $5,000-15,000 for pre-purchase inspection

Ownership & Registration

Registration number not available.

Location & Ownership

FAA records

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 safety data coming soon.

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Disclaimer: All prices, cost estimates, and market values shown are based on asking prices from third-party sources and are provided for informational purposes only. AeroGurus is not an appraiser, broker, or financial advisor. Always obtain a professional appraisal and independent inspection before making a purchase decision. Actual transaction prices may differ from asking prices.