Piper PA-34-200T Seneca II

Hersteller: Piper Aircraft Modellbezeichnung: PA-34-200T Seneca II Flugzeugtyp: Motorflugzeug Motor: Continental (L)TSIO-360-EB 200 PS Leergewicht: 1.478,00 kg MTOW: 1.999,00 kg Sitzplätze: - Baujahr: 1978 Gesamtzeit: 3.920 h TT Landungen: - Standort: Augsburg (DE) Unfall: Ja, Schäden durch LTB behoben Zustand: gebraucht Nächste JNP: August 2026 1978 Piper PA-34-200T Seneca II The Piper Seneca II combines a spacious six-seat cabin with turbocharged twin-engine performance, making it a versatile aircraft for private and business travel. Its counter-rotating engines, practical cabin and useful load have made the Seneca a popular choice among owner-pilots for decades. D-GARE offers comparatively low total time, a well-equipped IFR panel with dual instrumentation and wing de-ice boots. According to the owner, the aircraft has always been hangared and is currently kept in a heated hangar. This Seneca II represents an attractive opportunity to acquire a capable and versatile twin at a competitive asking price. We offer this aircraft as exclusive broker - contact us for any question! Make / Model: Piper PA-34-200T Seneca II Year: 1978 Serial Number: 34-7870205 Total Time: 3,920 h TT Annual: August Maintenance: 100-hour inspection and Airworthiness Review completed on 21 August 2026. ARC valid until 20 August 2027. New R/H vacuum pump installed in 08/2026. L/H centre fuel bladder replaced in 2025. R/H wing de-ice boot and both front windshields replaced during the documented repair in 2003. Interior: Grey and red leather interior, renewed twice, in good condition (7 of 10) Exterior: Allover white with red and black stripes, repainted in 1990, in good condition (7 of 10) Weights & Balance: Empty weight: 1,478 kg Maximum take-off mass (MTOM): 1,999 kg Useful load: 521 kg Fuel capacity: 464 litres Engine(s): Continental (L)TSIO-360-EB, rated at 200 hp TBO 1.800 hr or 12 years recommended L/H 1.797 SMOH compl. in 08/1990 R/H 1.797 SMOH compl. in 08/1990 Leak test in 08/2026: L/H 70/66/70/69/68/69 of 80 psi R/H 69/70/68/69/68/68 of 80 psi Propeller(s) Hartzell BHC-C2YF-2CKUF / BHC-C2YF-2CLKU(F), 2-blade TBO 2.000 hr or 5 years recommended L/H 400 SPOH compl. in 12/2006 R/H 546 SPOH compl. in 12/2002 History Built in 1978 and initially registered in Sweden as SE-GVN. According to the owner, the aircraft was imported from Sweden to Germany around 1990. Logbooks No. 2 to 4 and the corresponding aircraft records are available continuously from 6 July 1990 to the present. According to the present owner, two previous owners are known; both have since passed away. The complete ownership history prior to 1990 has not yet been confirmed. According to the owner, the aircraft has always been hangared and is currently kept in a heated hangar. Damage History In 2001, the aircraft sustained damage during a hard landing. The documented repair was completed and released to service on 12 March 2003 at 3,374 hours total time. The repair included work to the right wing, lower right fuselage aft of the wing attachment, right main landing gear, right aileron, right flap, right wingtip and right propeller. According to the owner, no other damage is known. Avionics Audio / Marker: King KMA 20 COM / NAV / GPS: Garmin GNS 430 COM / NAV: Garmin GNC 255A Transponder: Garmin GTX 330 Mode S Transponder: King KT 76C DME: King KN 62A ADF: King KR 87 Autopilot: Piper Altimatic III C Weather: Sperry/RCA Weather Scout 1006 ELT: Artex ME 406 Equipment Wing de-ice boots Co-pilot instruments Club seating Intercom Propeller de-ice Windshield ice plate Strobe Lights Aircraft Subject to Prior Sale or Removal from Market without Notice. Specification Subject to Verification by Purchaser.