1974 Piper Seneca II PA-34-200T
Description
The Piper PA-34 Seneca II is a twin-engine, six-seat, light aircraft manufactured by Piper Aircraft. It was first introduced in 1975, and is still in production today. The Seneca II features a high-wing design, two Lycoming IO-360 engines, a retractable landing gear, and a pressurized cabin. The Seneca II is popular with both private pilots and flight schools, as it can be used for both personal and commercial use. Its range of up to 800 nm makes it an ideal choice for longer trips. It is also relatively fuel-efficient, making it a cost-effective option for many pilots.
Features
- Airframe Total Time: 5161.3
- Engine(s)
- Continental TSIO-360-KB4B
- S/N 811325R / 812059R
- SFRM: 1554.2 / 1549.9
- 1800 TBO / 1800 TBO
- 610.58 STOH by Western Skyways 4/1/2015 (six new cylinders)
- Prop Details
- Hartzell BHC-C2YF-2CKUF
- S/N: AN4217 / AN829
- TSOH: 1554.2 / 1554.2
- Number of Blades: 2 (electrically heated)
- Avionics
- Garmin GNS 430W
- Garmin GI 106A Nav Indicator
- Garmin GTX 327 Transponder
- Garmin GMA 340 Audio Panel
- PS Engineering PCD7100-P CD Player
- King KR 87 ADF
- Piper Autocontrol IIIC Autopilot with Glideslope Coupler
- Maintenance Status
- Date of last annual: 4/13/22
- Date of last Pitot Static, Altimeter, and Transponder checks: 7/16/21
- Features/Options
- Merlyn Products Turbocharger Differential Pressure Control Unit
- Avionics Master Switch
- Vertical Card Compass
- Over-boost Annunciators Lights
- Pitot Heat
- Inflatable Door Seals
- EGT Gauges
- Electric Trim
- Autopilot Disconnect Switch
- Six-place Intercom
- Right Engine Disassembled and Crankcase replaced with serviceable by Western Skyways 4/1/2015
- Right Engine Alternator replaced, and Battery replaced 1/4/2016
- Left Engine Alternator replaced 10/22/2015
- New prop cables 6/15/2015
- New Wingtips w/ strobes and landing lights installed 5/20/1992
- Fuselage modified for camera holes 5/20/1997
Location
