1975 Piper Navajo Chieftain
Description
The Piper Navajo Chieftain is a light twin-engine aircraft produced by Piper Aircraft from 1974 to 1982. It was designed to be a larger, more powerful version of the popular Piper Navajo. The aircraft was equipped with two Lycoming IO-540-K1G5 engines and had a maximum takeoff weight of 5,100 lbs. It had a range of up to 1,100 nm and was capable of cruising at speeds up to 175 kts. The Chieftain also featured a retractable tricycle landing gear, increased fuel capacity, and larger windows. The aircraft was used for both personal and business travel, as well as for air ambulance and cargo transport.
Features
- Total Time: 12200
- Engine(s):
- Left 640 SMOH
- Right 1550 SMOH
- Prop(s):
- Left 488 SPOH
- Right 488 SPOH
- Avionics:
- Garmin 530 WAAS GPS
- Garmin GTX 327 Digital Transponder
- Bendix/King KMA-24 Audio Panel
- Bendix/King KY-196A Digital Com
- Bendix/King KX-175B Com/Nav
- Bendix/King KR-87 ADF
- Bendix/King KNS-80 DME
- Bendix IN-152A Weather Radar
- Additional Options:
- Heated Windshield
- Crew Door
- Executive Cabinetry
- Prop De-Ice
- Dual Push To Talk Buttons
- Avionics Master
Location
