1974 Piper Aztec PA-23-250E turbo
Description
The Piper PA-23 Aztec is a twin-engined light aircraft that was first introduced in 1950. It was developed as a commercial aircraft, but has also been widely used as a personal transport and in military service. The PA-23-250E Turbo is a turbocharged version of the Aztec, which was produced from 1974 to 1984. It is powered by two Lycoming TIO-540-C1A6 turbocharged engines, each producing 250 hp. The aircraft is equipped with a retractable tricycle landing gear, has a maximum speed of 211 mph, and a range of 1,231 miles. It can carry up to 6 passengers and has a useful load of 1,106 lbs.
Features
- Total Time: 4161
- Engine(s):
- Engine 1
- LYCOMING
- 250 HP
- 256 SMOH
- 2000 TBO
- Engine 2
- LYCOMING
- 250 HP
- 1440 SMOH
- 2000 TBO
- Prop(s):
- HARTZELL
- 55 SPOH
- 55 SPOH
- Modifications/Conversions:
- Metro Long Range Fuel system
- JPI EDM 730 Digital engine monitor
- JPI fuel flow
- New 406 ELT
- Recent Glass including Speed Slope one piece WS
- Avionics:
- Garmin GTN 750 Txi Touchscreen GPS WAAS
- Garmin GNS430 GPS Com/Nav
- Aspen 1000 PFD with HSI
- Garmin G 5 Indicator
- Appereo Status ESG Transponder with ADSB
- HSI
- Garmin GMA 345 Audio panel
- Bendix Alitmatic V with FD
- Additional Equipment:
- Speed slope one piece windshield
- LR fuel
- Strobe lights
- Beacon light
- Position lights
- Landing light
- Taxi light
Location
