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Aeromeccanica S.A - Our current offers
Piper PA-34-200 Seneca I |
on request |
Overview
| Base data | | Type: | Single Prop | | Make: | Piper | | Model: | PA-34-200 Seneca I | | Year built: | 1972 | | Registration No.: | HB-LML | | Serial No.: | TBD | | Location: | Switzerland, Locarno | | Total Time (TTAF): | 9881 h | | Price: | on request | | Full details |
| Seller |
Aeromeccanica S.A
Aeroporto Cantonale di Locarno
6596 Gordola
Switzerland
Tel: +41-91-2103128
Fax: +41-91-7450037 |
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Full Details
| Base data | | Type: | Single Prop | | Make: | Piper | | Model: | PA-34-200 Seneca I | | Year built: | 1972 | | Registration No.: | HB-LML | | Serial No.: | TBD | | Location: | Switzerland, Locarno | | Total Time (TTAF): | 9881 h | | Price: | on request |
| 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 operation
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 |
| Other remarks | 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
Engine LH: Textron-Lycoming IO-360-C1E6, sn L-1118-51A
Propeller 2 Bladed Hartzell LH: CH -C2YK-2CGUF, sn AU13103B
Overhauled with New improved hubs in July 2007
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
In good conditions.
Landing accident with one main gear collapse and wing spar repair performed in 1991 at TT: 6557
Missing logs from 1972 to 1981, Prior to Swiss registration.
Replaced fuel tank vent line hoses 12/07
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
Specifications subject to verification by purchaser |
Pictures
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