1972 PIPER SENECA
Description
Specifications
Year1972
ManufacturerPIPER
ModelSENECA
ConditionUsed
Registration #HB-LML
FlightRulesIFR
Based atLSZL
Total Time9,881
AirframeAirframe total time: 9881 hrs
Engine 1 Time10,251 SNEW
Engine 1 TBO2000
Engine ManufacturerEngines:
LH: Textron-Lycoming IO-360-C1E6, sn L-1118-51A TT: 10251, TSOH: 1155:48 overhauled by Mattituck in September 1998,
RH: Textron-Lycoming LIO-360-C1E6, sn L-444-67A TT: 7758:38, TSOH: 1686:32 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")
Engine 2 Time7,758 SNEW
Prop Specs2 Bladed Hartzell Propellers
LH: CH -C2YK-2CGUF, sn AU13103B TT: 5737,
Time Since Overhaul: 144:25 hrs
Overhauled with New improved hubs in July. 2007.
RH: HC-C2YK-CLGUF. sn AU13099B TT: 6648:19, Time Since Overhaul: 144:25 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")
WAASYes
LPVYes
Avionics/RadiosIFR,
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)
Inadvertent Ice ProtectionYes
Additional EquipmentLightweight 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
Exterior NotesLight gray with maroon stripes 7/10
Number of Seats6
Interior NotesBlue vinyle 9/10 Gray fabric seats 9/10 Pilot and Copilot Adjustable seats Blue carpet 9/10
Inspection StatusIn 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
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
Annual inspection and EASA ARC are overdue.
Selling as is, where is