1975 Piper PA-31-325 Navajo C/R

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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.


  • 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)

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