Piper PA-34-200 Seneca I

Prezzo su richiesta

Quadro generale

Sommario
Tipo:	Propulsione singola
Costruttore:	Piper
Modello:	PA-34-200 Seneca I
Anno di costruzione:	1972
Numero di registrazione:	HB-LML
Ubicazione/sede:	Svizzera
Prezzo:	Prezzo su richiesta
Tutti i dettagli

Rivenditore
Aeromeccanica S.A Aeroporto Cantonale di Locarno 6596 Gordola Svizzera Tel.: +41-91-2103128 Fax: +41-91-7450037
contattare il rivenditore




Mostra tutte le 13 foto

Dettagli

Sommario
Tipo:	Propulsione singola
Costruttore:	Piper
Modello:	PA-34-200 Seneca I
Anno di costruzione:	1972
Numero di registrazione:	HB-LML
Ubicazione/sede:	Svizzera
Prezzo:	Prezzo su richiesta

Avionica

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)

Esterno
Light gray with maroon stripes 7/10

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

Altre segnalazioni

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