1980 Piper Aztec E
Description
The Piper Aztec E is a six-seat, twin-engine aircraft manufactured by Piper Aircraft. It is a turbocharged version of the four-seat Piper Aztec and was first introduced in 1971. The Aztec E is powered by two Lycoming TIO-540-A2A engines, each producing 310 hp. These engines are capable of pushing the aircraft to a maximum cruise speed of 185 mph and a maximum range of 1,360 miles. The aircraft also features a retractable landing gear and a gross weight of 4,800 lbs. The Aztec E is commonly used in business and charter operations, as well as private and training flights.
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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