Piper PA-34-200 Seneca I

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Resumen

Vista general
Tipo:	Monomotor
Fabricante:	Piper
Modelo:	PA-34-200 Seneca I
Año de construcción:	1972
Reg-No.:	HB-LML
Lugar:	Suiza
Precio:	Consultar precio
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Oferente
Aeromeccanica S.A Aeroporto Cantonale di Locarno 6596 Gordola Suiza Tel.: +41-91-2103128 Fax: +41-91-7450037
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Detalles

Vista general
Tipo:	Monomotor
Fabricante:	Piper
Modelo:	PA-34-200 Seneca I
Año de construcción:	1972
Reg-No.:	HB-LML
Lugar:	Suiza
Precio:	Consultar precio

Aviación

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 and VOR, 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 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 Stormscope, Copilot instruments Airspeed, Attitude Indicator, Altimeter, VOR/GS, DG Day/Night, IFR Category 1, B-RNAV (RNP 5)

Exterior
Light gray with maroon stripes 7/10

Interior
Blue vinyle 9/10 Gray fabric seats 9/10 Pilot and Copilot Adjustable seats Blue carpet 9/10

Observación / Otro

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

Good economic twin. Maximum Take Off Weight: 1905 kg - 4199.00 lbs Empty Weight: 2960.55 Useful Load: 1235.45 Lbs Fuel Capacity: 93 USG Annual inspection and EASA ARC are overdue. Selling as is, where is

Airframe Serial Number TBD TT: 9,881 Engine LH: Textron-Lycoming IO-360-C1E6, sn L-1118-51A TT: 10251 Propeller 2 Bladed Hartzell LH: CH -C2YK-2CGUF, sn AU13103B TT: 5737, Time Since Overhaul: 144:25 hrs Overhauled with New improved hubs in July. 2007

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 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 and ferry tank: 453.45 Lbs FERRY TANK NOT AVAILABLE