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Piper PA-34-200T Seneca II |
CAD 201,771
€ 135,000 |
Overview
| Base data | | Type: | Single Prop | | Make: | Piper | | Model: | PA-34-200T Seneca II | | Year built: | 1979 | | Registration No.: | I-CUND | | Location: | Italy | | Price: | € 135,000
(~ CAD 201,771) | | Full details |
| Seller |
Aeromeccanica S.A
Aeroporto Cantonale di Locarno
6596 Gordola
Switzerland
Tel: +41-91-2103128
Fax: +41-91-7450037 |
| Contact seller |
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Full Details
| Base data | | Type: | Single Prop | | Make: | Piper | | Model: | PA-34-200T Seneca II | | Year built: | 1979 | | Registration No.: | I-CUND | | Location: | Italy | | Price: | € 135,000
(~ CAD 201,771) |
| Avionics | | Garming GMA340 Audio Panel with Intercom and Marker Beacon 2 Garmin GNS430 WAAS NAV-COM-GPS Bendix King KFC200 Auitopilot Sandel SN3308 HSI Bendix King KN62 GMX200 MFD Multi Function Display JPI TIT Digital Indicator JPI EGT Digital Indicator L3 Avionics WX500 Stormscope coupled to NSD3308, GNS430W number 1 and GMX200 Magnetic Compass Artex ELT 406 mHz Full Copilot Instrument Panel with: - Airspeed Indicator - Attitude Indicator - Altimeter - Vertical Speed Indicator - Directional Gyro |
| Exterior | | White with red stripes, original Piper desigh, in good decent |
| Interior | | 6 seats, red velour and black carpet Original factory intrerior, in good condition All seats equipped with headrests, New window curtains (currently not installed), Refreshment center, Courtesy table |
| Other remarks | Fuel Capacity: 61.5 USG X", Total 123 USG MTOW: 4570 LBS Empty Weight: 3293.69 LBS (1493.69 Kg) Noise Level: 78.5 dB(A) according ICAO Annex 16, Vol. 1, Chapter 10 Maximum Take Off Weight: 2073 kg Specifications subject to verification by purchaser
Private aircraft Selling due to low utilisation Two owners since new Previously registered in Switzerland, from 26/07/1979 to 24/05/2022 No damage history Always hangared See generic details of the type on this link: https://myseneca.blogspot.com/p/specifications.html
Airframe Serial Number 79-70108 Total Time: 5100 Engines, Continental TSIO-360-EB, 310 HP TSOH: 870 hours, Ovherhauled in 2010 by BMA Bosio Motori in Brescia, Italy Propellers, 3 Bladed McCAULEY AVIATION CORPORATION, 3AF34C502/503 with electric de-ice TSOH: 870 hours Tear Down Inspection performed in 2017
- Long range fuel tanks - Janitrol Cabin Heater - Surface pneumatic deice system (Boots) - Windshield hotplate - 3 Bladed propellers with electrothermal deice system - Portable oxygen cylinder (Hydrostatic test expired) - Lo Presti flaps hinges fairings - Lo Presti flaps and ailerons gaps seals - Lo Presti gear lobes fairing kit - Lo Presti Hub Cap W/Access Door. 6" Wheel - Wing Tips Recognition Lights |
Pictures
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