1972 Piper Seneca I for sale, Switzerland

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1972 piper seneca 1 parked in front of open hangar with other aircraft in view nose forward image white body and dark stripe
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Piper Seneca I 2
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Piper Seneca I 3
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Piper Seneca I 4
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Piper Seneca I 5
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Piper Seneca I 6
Price: £55,000
Europe, Switzerland
Year
1972
S/N
TBD
Reg
HB-LML
TT
9,816

Aircraft Description

Engines: LH TSOH 1016 overhauled by Mattituck in 98- RH 1526 overhauled in 96- 2 Bladed Hartzell Propellers Overhauled with New hubs in July. 2007. Time since overhaul: 60 hrs- Interior Blue vinyle 9/10- Gray fabric seats 9/10- Pilot and Copilot Adjustable seats- Blue carpet 9/10

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Aeromeccanica SA
  • AIRFRAME / ENGINES / APU / WEIGHT / TOTAL TIME / TOTAL LANDING

    AIRFRAME

    Airframe total time: 9816:20 hrs

    ENGINES

    Engines: 

    LH: Textron-Lycoming IO-360-C1E6, sn L-1118-51A

    TT: 10186, TSOH: 1025:48 overhauled by Mattituck in September 1998, 

    RH: Textron-Lycoming LIO-360-C1E6, sn L-444-67A 

    TT: 7693:38, TSOH: 1556:32 overhauled by Mattituck in July 1996

    TBO: 2000 hrs / 12 Years (Calendar overhaul not mandatory in Switzerland for private operation. 

    Also read new EASA Notice of Proposed Amendment (NPA) No 2011-15 for future "Non-binding guidance on TBO limits")

    2 Bladed Hartzell Propellers: 

    LH: CH -C2YK-2CGUF, sn AU13103B

    TT: 5672, Time Since Overhaul: 79:25 hrs

    Overhauled with New improved hubs in July. 2007. 

    RH: HC-C2YK-CLGUF. sn AU13099B

    TT: 6583:19, Time Since Overhaul: 79:25

    Overhauled with New improved hubs in July. 2007. 

    TBO: 2000 hrs / 6 Years. 

    (Calendar overhaul not mandatory in Switzerland for private operation. 

    Also read new EASA Notice of Proposed Amendment (NPA) No 2011-15 for future "Non-binding guidance on TBO limits")

    TOTAL TIME

    9,816
  • AVIONICS & CONNECTIVITY

    IFR,

    KMA20 Audio/MB,

    2 x KX125 COM 760 Ch, FM Immune,

    KN72 NAV,

    KN75 ILS,

    KCS55 HSI,

    KR85 ADF with RMI,

    KN62A DME,

    Narco ELT10,

    Garmin 330 Mode "S" XPDR,

    ACK A30 Encoder,

    Autocontr III Autopilot 3 ax coupled to HSI and VOR,

    Intercom. Garmin GPS 155 TSO , approved for VFR/IFR enroute, B-RNAV, terminal and instrument approach (GPS, VOR, VOR-DME, NDB, NDB-DME) operation. Within the US National Airwspace System in accordance with AC 20-138 and such countries where GPS enroute, terminal and non-precision approaches are authorized by the appropriate airworthiness authority.

    WX900 Strmscope,

    Copilot instruments Airspeed, Attitude Indicator, Altimeter, VOR/GS, DG

    Certified VFR Day/Night, IFR Category 1, B-RNAV (RNP 5)

  • Interior & Entertainment

    Blue vinyle 9/10,

    Gray fabric seats 9/10,

    Pilot and Copilot Adjustable seats,

    Blue carpet 9/10

  • EXTERIOR

    Light gray with marroon stripes 7/10

  • Additional Equipment & Information
    Lightweight Surface Pneumatic De-icing system and propeller electrothermal de-icing system, 

    Windshield hot plate, 

    Pitot and stall warning heat system protected by landing gear switch

    Propellers with dampers

    Electric pitch trim installation, 

    Logo light, 

    Additional FOCA Approved 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

    WiFi

    No

    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

    Next annual inspection due 12/08

    EASA Certificate of Airworthiness

    EASA Noise Certificate 74.8 dB(A)

    Maximum Take Off Weight: 1905 kg - 4199.00 lbs

    Empty Weight: 2960.55

    Useful Load: 1235.45 Lbs

    Fuel Capacity: 93 USG

    WILL TRADE FOR ULM (Ultralight) Aircraft

    Will sell with fresh 100 hrs annual inspection that will include:

    fresh ARC

    updated approved maintenance program

    new battery

    compliance with repetitive AD's

    new nose baggage door lock

    altimeters and pitot static test

    avionics ramp test

    magnetic compass swing

    new ELT battery

    nose gear trunnion 1000 hrs inspection

    wing spar check

    7 years inspection

    magnetos 500 hrs inspection

    new engine driven fuel pumps

    one new electric fuel booster pump

    many additional new items replaced

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