1972 Piper SenecaMulti-Engine Piston Aircraft • Locarno, Ticino, Switzerland

This 1972 Piper Seneca, registered as HB-LML, is a used IFR-capable piston twin based in Locarno, Switzerland (LSZL) with a total airframe time of 9,881 hours. The airframe carries a history of a landing accident in 1991 at 6,557 hours, involving one main gear collapse and a subsequent wing spar repair. Missing logs exist from 1972 to 1981, prior to Swiss registration. The annual inspection and EASA ARC are overdue, and the aircraft is being sold as is, where is.

The left engine, a Textron-Lycoming IO-360-C1E6, has 10,251 hours since new and 1,155 hours since overhaul by Mattituck in September 1998, while the right engine, a...

Year: 1972

Make: Piper

Series: Seneca

Model: Seneca

Tail #: HB-LML

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Specifications

Category: Multi-Engine Piston

Intended Use: Business, Training

Flight Rules: IFR

Useful Load: 1,235.45 lbs

Seats: 6

Hours, Logs & Inspections

Total Time: 9,881 hrs

Engine 1 Time: 10,251 hrs (SNEW)

Engine 2 Time: 7,758 hrs (SNEW)

Prop 1 Time: 5,737 hrs

Prop 2 Time: 6,648 hrs

Logbook Status: Missing Logs From 1972 To 1981, Prior To Swiss Registration.

Inspection Status: Annual Inspection And EASA ARC Are Overdue. Selling As Is, Where Is. Landing Accident With One Main Gear Collapse And Wing Spar Repair Performed In 1991 At TT: 6557. Replaced Fuel Tank Vent Line Hoses 12/07.

Avionics

GPS

Garmin GNS 530W - 1 x WAAS 8.33 kHz, GPS Approved For VFR/IFR Enroute, B-RNAV, Terminal And Instrument Approach (GPS, VOR, VOR-DME, NDB, NDB-DME) Operation. Within The US National Airspace System Accordance With AC 20-138 And Such Countries Where GPS Enroute, Terminal And Non-Precision Approaches Are Authorized By The Appropriate Airworthiness Authority.

Comms

King KX 125 - x COM 760 Ch, FM Immune, KN72 NAV

Autocontrol III - Autocontr III Autopilot 3 Axis Coupled HSI And VOR

Audio

PS Engineering Audio Panel - PS With Intercom And Marker Beacon

Weather

Stormscope WX 900

Additional Equipment

De-Icing System

Lightweight Surface Pneumatic De-Icing System And Propeller Electrothermal De-Icing System, Windshield Hot Plate, Pitot And Stall Warning Heating System Protected By Landing Gear Switch

HSI

King KCS 55 - HSI

ADF

King KR 85 - ADF With RMI

DME

King KN 62A - DME

ELT

ME 406 - ELT

Transponder

King KT 79 - Mode 'S' XPDR, ACK Encoder

Electric Pitch Trim

Electric Pitch Trim Installation

Logo Light

Currently Removed, Hoses Still Present With Covers Installed

Ferry Fuel

Additional FOCA Approved Documentation For 98 USG Fuel Tank For Ferry Flights. Increased MTOW Approved For 4560 Lbs. Remaining Useful Load With Full Tanks And Ferry Tank: 453.45 Lbs. Ferry Tank NOT Available