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Piper PA-34-200T Seneca II |
US$ 148.467
€ 128.000 |
Обзор
| Список альбомов | | Тип: | одиночный пропеллер | | Производитель: | Piper | | модель: | PA-34-200T Seneca II | | год выпуска: | 1979 | | Регистрационный номер: | I-CUND | | Серийный номер.: | 79-70108 | | местонахождение: | Италия, Terni | | Общее время (TTAF): | 5150 h | | цена: | € 128.000
(~ US$ 148.467) | | Полные сведения |
| Провайдеры |
Aeromeccanica S.A
Aeroporto Cantonale di Locarno
6596 Gordola
Швейцария
Тел.: +41-91-2103128
Факс: +41-91-7450037 |
| Контакт с продавцом |
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Подробности
| Список альбомов | | Тип: | одиночный пропеллер | | Производитель: | Piper | | модель: | PA-34-200T Seneca II | | год выпуска: | 1979 | | Регистрационный номер: | I-CUND | | Серийный номер.: | 79-70108 | | местонахождение: | Италия, Terni | | Общее время (TTAF): | 5150 h | | цена: | € 128.000
(~ US$ 148.467) |
| Авионика | Garmin GMA340 Audio Panel with Intercom and Marker Beacon
2 Garmin GNS430 WAAS NAV-COM-GPS
Bendix King KFC200 Autopilot
Garmin 275 Attitude Indicator / Multi Function Display
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 |
| внешний вид | | White with red stripes, original Piper design, in good condition |
| интерьер | 6 seats, red velour and black carpet
Original factory interior, in good condition
All seats equipped with headrests,
New window curtains (currently not installed),
Refreshment center,
Courtesy table |
| Замечания / Прочее | 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
Annual inspection and ARC renewal performed in November 2025
See generic details of the type on this link:
https://myseneca.blogspot.com/p/specifications.html
Fuel Capacity: 61.5 USG X2, 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
Engines: Continental TSIO-360-EB, 310 HP
TSOH: 920 hours, Overhauled in 2010 by BMA Bosio Motori in Brescia, Italy
Propellers: 3 Bladed McCAULEY AVIATION CORPORATION, 3AF34C502/503 with electric de-ice
TSOH: 920 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
Specifications subject to verification by purchaser |
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