1975 Piper PA-31-325 Navajo C/R
Description
The Piper PA-31-325 Navajo C/R is a single-engine, low-wing, six-seat, light business aircraft. It was originally developed in the mid-1970s from the Piper PA-31-300 Navajo by Piper Aircraft. It was designed as an improved version of the earlier aircraft, offering increased performance and better handling characteristics. The Navajo C/R is powered by a single Lycoming TIO-540-A1A piston engine, which produces 325 horsepower. It has a range of 1,100 nautical miles and is capable of reaching speeds of up to 230 knots. The aircraft has a maximum takeoff weight of 5,400 pounds and a maximum seating capacity of six passengers. The aircraft is equipped with retractable landing gear and can be configured with a variety of optional features, including an autopilot, GPS navigation, and a cabin pressurization system. The Navajo C/R has proved popular with both private and corporate operators and is still in production today.
Features
- Total Time: 8,765 Hours
- Engine(s)
- Lycoming LTIO-540-F2BD
- TBO: 1,800 Hour
- Time Since Overhaul: 911.7/1148
- Prop Details
- 3-Blade Hartzell
- Time Since Overhaul: 69 / 69
- Avionics
- Garmin GNS-430W GPS/COMM
- 3M WX-10ª Strike Finder
- Garmin GTX-327 Transponder
- GARMIN 696 Moving Map GPS
- Aspen Evolution PFD
- Garmin GMA-340 Audio Panel
- KX 165 TSO Nav/Comm
- Maintenance Status
- This beautiful Navajo just returned from Cardinal Aviation with a fresh annual.
- Features/Options
- Hot Plate Pilot Window
- De-Ice Boots
- Oxygen
- Auto Pilot
- Air Conditioning
- UAVIONIX Tail Beacon ADSB
- Vortex Generators
- Tinted Rear Windows
- Pull out Desk (Not Currently Installed)
Location
