1980 Piper Navajo Chieftain
Description
The Piper Navajo Chieftain is a twin-engined light aircraft produced by Piper Aircraft. It was introduced in 1976, and is a variant of the Piper PA-31 Navajo. It is powered by two Lycoming TIO-540-A2A piston engines, each producing 350 horsepower. It is equipped with retractable landing gear, and a pressurized cabin, and can carry up to eight passengers. It has a cruise speed of 187 knots, and a maximum range of 1,300 nautical miles. It has a maximum takeoff weight of 8,000 lbs.
Features
- Total Time: 7375
- Engines / Mods / Prop
- Engine Time:
- Left 1715 SMOH
- Right 1898 SMOH
- Prop Time:
- Left 145 SPOH (Aug 2019)
- Right 145 SPOH (Aug 2019)
- Avionics / Equipment
- AVIONICS
- Garmin GMA340 Audio Panel
- King KX165 Nav/Com G/S
- King KX165 Nav/Com G/S
- King HSI
- King 150 MFD
- King KFC-200 Autopilot
- Garmin GPS
- Garmin 327 Transponder
- Collins ADF 650
- Radar Altimeter
- Fuel Flow
- EGT
Location
