1980 Piper PA-23F Turbo Aztec
Description
The Piper PA-23F Turbo Aztec is a six-seat, twin-engine aircraft that was produced by Piper Aircraft from 1975 to 1981. It is powered by two Lycoming TIO-540-F2BD turbocharged engines producing 220 hp each. The Turbo Aztec has a maximum speed of 202 knots and a range of 1,240 nautical miles. It is equipped with retractable gear and can be fitted with floats or skis. It is an ideal aircraft for personal or business use, as well as for air taxi operations. The Turbo Aztec is known for its reliability and ruggedness, making it a popular choice for many pilots.
Features
- Total Time: 4473
- Engine(s):
- Engine 1
- LYCOMING IO-540-C4B5
- 0 SMOH
- By Signature Engines
- Engine 2
- LYCOMING
- 704 SMOH by Signature Engines (2005)
- Props:
- Left Prop
- HARTZELL
- 477 SPOH 2009
- Right Prop
- HARTZELL
- 538 SPOH 2008
- Avionics:
- Dual Garmin G-5 PFD/HSI
- Garmin GNS-430 WAAS GPS/Com/Nav/MFD
- Garmin GTX-345 Transponder with ADSB In and Out
- King KY-196 Digital Com
- King KNS-80 RNAV VOR LOC GS ILS
- PS Engineering Audio Panel with CD Player
- King RDR 150 Radar
- BFG WX-900 Storm Scope
- King KFC-200 Autopilot with Flight Director System
- King KCS-55A HSI Mount on Copilot station
- Dual GS Indicators
- Additional Equipment:
- Factory De Ice Boots
- Hot Plate
- Hot Props
- Long Range Fuel
- Position Lights
- Taxi Light
- Landing Light
- Strobe Lights
- Pilot Heat
- Dual Hydraulic Pumps
- Dual Alternators
- JPI Digital Engine Monitor
- Hoskins Fuel Flow Gauge
- Co Pilot Instruments
- E Style Tail
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