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1972 Piper SenecaMulti-Engine Piston Aircraft

Year
1972
Make
PIPER
Series
PA-34 Seneca
Model
SENECA
Tail #
HB-LML

This 1972 Piper Seneca (HB-LML) presents as an IFR-capable twin with 9,881 hours on the airframe, currently based in Switzerland. The aircraft features a 1991 landing accident history involving a main gear collapse and wing spar repair at 6,557 hours, along with missing logs from 1972-1981 prior to Swiss registration. Power comes from two Textron-Lycoming engines - the left (IO-360-C1E6) showing 10,251 hours with 1,155 since overhaul by Mattituck in 1998, and the right (LIO-360-C1E6) at 7,758 hours with 1,686 since its 1996 overhaul. Both engines operate under Switzerland's private-use TBO exemption.

The avionics suite includes a Garmin GNS530 WAAS, King KX125 COM, coupled Autocontr III autopilot, and full IFR instrumentation with B-RNAV capability. De-icing systems include pneumatic wing/empennage protection and electrothermal propeller de-icing. The aircraft carries an increased MTOW approval to 4,560 lbs, with a current useful load of 453 lbs at full fuel (93 USG standard tanks plus optional ferry tank documentation). The exterior shows in light gray/maroon at 7/10 condition, while the blue vinyl interior and gray fabric seats rate 9/10. Annual inspection and EASA ARC are currently overdue, and the aircraft is being sold "as is" with recent maintenance including fuel vent line hose replacement in 2007 and propeller overhauls with improved hubs that same year.

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Location

Gordola, Switzerland

Listing Details

Condition
Used

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First Seen: Apr 20, 2025

Specifications

Category
Multi-Engine Piston
Intended Use
Business, Recreational
Flight Rules
IFR
Useful Load
1,235.45 lbs
Seats
6

Hours, Logs & Inspections

Engine 1 Time
10,251 hrs
Engine 2 Time
7,758 hrs (:38)
Prop 1 Time
5,737 hrs
Prop 2 Time
6,648 hrs (:19)
Logbook Status
Missing logs from 1972 to 1981
Inspection Status
Annual inspection and EASA ARC are overdue. Selling as is, where is

Avionics

GPS

Garmin GNS 530 WAAS - WAAS 8.33 kHz

Comms

King KX 125 - COM 760 Ch, FM Immune

AP

Autocontr III - III Autopilot 3 axis coupled HSI and VOR

Audio

PS Engineering - PS audio panel with intercom and marker beacon

Weather

WX 900 - Stormscope

ADS-B Out

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

Additional Equipment

Ice Protection

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

Electric Pitch Trim

Electric pitch trim installation

Logo Light

Currently removed, hoses still present with covers installed

Interior & Exterior

Interior Rating
9/10
Paint Rating
7/10
Interior Notes
Blue vinyle 9/10 Gray fabric seats 9/10 Pilot and Copilot Adjustable seats Blue carpet 9/10
Exterior Notes
Light gray with maroon stripes 7/10

Engine & Propeller

Engine Type
Piston
Engine Count
2
Engine Make
Textron-Lycoming
Engine Model
IO-360-C1E6, LIO-360-C1E6
Propeller Model
Hartzell 2 Bladed

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