Piper PA-34-200 Seneca I Piper - Aircraft Piston
Piper PA-34-200 Seneca I Piper - Aircraft Piston
Piper PA-34-200 Seneca I Piper - Aircraft Piston
Piper PA-34-200 Seneca I Piper - Aircraft Piston
Piper PA-34-200 Seneca I Piper - Aircraft Piston
ID: 1815
INQUIRE
Selling. Used
Piper PA-34-200 Seneca I
Piston Aircraft Piper
Description
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
Airplane time state
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
Interior
Blue vinyle 9/10 Gray fabric seats 9/10 Pilot and Copilot Adjustable seats Blue carpet 9/10
Exterior
Light gray with maroon stripes 7/10
Avionics
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)
Options
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
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
Characteristics
Registration
HB-LML
Year of construction
1972
Country
Switzerland
City/Aerodrome
Locarno
Information
Publication date
2024-12-17
Section
Aircraft
Category
Piston
Manufacturer
Views
37
Favorites
0
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Piper PA-34-200 Seneca I Piper - Aircraft Piston
5
ID: 1815
INQUIRE
Selling. Used
Piper PA-34-200 Seneca I
Piston Aircraft Piper
Description
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
Airplane time state
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
Interior
Blue vinyle 9/10 Gray fabric seats 9/10 Pilot and Copilot Adjustable seats Blue carpet 9/10
Exterior
Light gray with maroon stripes 7/10
Avionics
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)
Options
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
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
Characteristics
Registration
HB-LML
Year of construction
1972
Country
Switzerland
City/Aerodrome
Locarno
Information
Publication date
2024-12-17
Section
Aircraft
Category
Piston
Manufacturer
Views
37
Favorites
0
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