1980 Piper Navajo CR
Description
The Piper Navajo CR is a single-engine, light aircraft manufactured by Piper Aircraft. The aircraft was introduced in 1977 and is based on the original Piper Navajo which was introduced in 1967. The airplane was designed for shorter regional flights and can seat up to six passengers. The Navajo CR has a fixed tricycle landing gear and is powered by a Lycoming TIO-540-AH1A engine. The aircraft has a cruising speed of 170 knots and a range of 1,000 nautical miles. The aircraft is equipped with modern avionics such as a Garmin G1000 avionics suite and an autopilot. The Piper Navajo CR is a popular aircraft among private pilots and is a great option for short regional flights.
Features
- Total Time: 4925
- Engine 1 Time: 225 SFOH
- Engine 2 Time: 525 SFOH
- Prop 1 Time: 225 SPOH
- Prop 2 Time: 525 SPOH
- AVIONICS:
- GARMIN AUDIO PANEL
- RADAR ALTITUDE
- BENDIX KING SLAVED HSI
- GARMIN 327 TRANSPONDER #2
- GARMIN 530 COM /NAV /GPS /Waas
- GARMIN GTX-330 W / TIS #1
- GARMIN 430 COM/ NAV/GPS
- SECOUND GLIDE SLOPE
- RCA BLACK & WHITE RADAR -INOP
- ALTIMATIC V F/D
- INTERCOM SYSTEM
- XM SATILITE STEREO SYSTEM
- ADDITIONAL EQUIPMENT:
- PANTHER CONVERSION:
- WINGLETS AND IN FLIGHT RECOGNITION LIGHTS
- "Q" TIP PROPELLORS-FOUR BLADED – NEW STYLE HUBBS
- SHADIN DIGIDATA FUEL COMPUTER CPLED TO GARMIN 530 GPS
- 40 DEGREE FLAP DRIVE KIT
- CLEVELAND WHEELS AND BRAKES
- KNOWN ICE OPTION. ALL DEICER BOOTS
- FACTORY AIR CONDITIONING
- WING LOCKERS
- COPILOT FLIGHT GROUP
- VORTEX GENERATORS
Location
