1972 Piper Seneca I for sale, Switzerland

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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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AIRFRAME / TOTAL LANDINGS / ENGINES / APU / WEIGHT

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")

  • AVIONICS & CONNECTIVITY

    IFR,
    KMA20 Audio/MB,
    Garmin GNS530 WAAS NAV-COM-GPS
    1 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 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 Red and Blue 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, (Currently Removed)
    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

    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

    Currently hangared and preserved. Annual inspection and ARC are expired

    Specifications subject to verification by purchaser

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