1974 Piper Navajo
Description
The Piper Navajo is a light twin-engine aircraft produced by Piper Aircraft. It was first introduced in 1974 and has since been used for personal and business aviation. It is an all-metal aircraft with a low wing and retractable landing gear. It can accommodate up to six passengers, and can be powered by either two Lycoming IO-540-K1A5 engines or two Lycoming TIO-540-A2A engines. The Navajo is also available in several variants, including the PA-31-300, PA-31-310, PA-31-325, PA-31-350, and PA-31P-350.
Features
- Total Time: 6479
- Engine:
- Lycoming T10-540 Series
- A/W Date 06/13/1974
- 1334/1334 SMOH
- Prop:
- 281/281 SPOH
- Avionics:
- Avidyne IFD 540/440
- Aspen Avionics Evolution PFD 1000
- C3 Pro, Stec 55X autopilot
- JPI 960 Engine Monitor
- GMA 347 Audio Panel
- GTX 345 transponder
- Bensix RDR160 Color Radar
- 6 Place Intercom
- WAAS Compliant
- DME
- Flight Director
- Moving Map
- Additional Features:
- LED Landing Light
- LED Taxi Light
- LED Beacon and Position Lights
- Reiff preheat system
- Battery minder battery charger
- Artex ELT406
- All AD's up to date
- ADS-B out compliant
- De-Ice Boots
- Alt Static
- Air Conditioner
- Oxygen
- Tinted Windows
Location
