Piper PA-34-200T Seneca II Piper - Aircraft Piston
Piper PA-34-200T Seneca II Piper - Aircraft Piston
Piper PA-34-200T Seneca II Piper - Aircraft Piston
Piper PA-34-200T Seneca II Piper - Aircraft Piston
Piper PA-34-200T Seneca II Piper - Aircraft Piston
ID: 1818
€ 135,000
Selling. Used
Piper PA-34-200T Seneca II
Piston Aircraft Piper
Description
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
Airplane time state
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
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
Exterior
White with red stripes, original Piper desigh, in good decent
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
Magnetic Compass
Artex ELT 406 mHz

Full Copilot Instrument Panel with:
- Airspeed Indicator
- Attitude Indicator
- Altimeter
- Vertical Speed Indicator
- Directional Gyro
Options
- 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
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
Characteristics
Registration
I-CUND
Year of construction
1979
Country
Italy
City/Aerodrome
Terni
Information
Publication date
2024-12-21
Section
Aircraft
Category
Piston
Manufacturer
Views
51
Favorites
0
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Piper PA-34-200T Seneca II Piper - Aircraft Piston
5
ID: 1818
€ 135,000
Selling. Used
Piper PA-34-200T Seneca II
Piston Aircraft Piper
Description
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
Airplane time state
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
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
Exterior
White with red stripes, original Piper desigh, in good decent
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
Magnetic Compass
Artex ELT 406 mHz

Full Copilot Instrument Panel with:
- Airspeed Indicator
- Attitude Indicator
- Altimeter
- Vertical Speed Indicator
- Directional Gyro
Options
- 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
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
Characteristics
Registration
I-CUND
Year of construction
1979
Country
Italy
City/Aerodrome
Terni
Information
Publication date
2024-12-21
Section
Aircraft
Category
Piston
Manufacturer
Views
51
Favorites
0
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