1978 Piper Navajo PA-31-325
Description
The Piper PA-31 Navajo is a family of cabin-class, twin-engined aircraft designed and built by Piper Aircraft for the general aviation market, most using Lycoming engines. It was also license-built in a number of Latin American countries. Targeted at small-scale cargo and feeder liner operations and the corporate market, the aircraft was a success. It continues to prove a popular choice, but due to decreased demand across the general aviation sector in the 1980s, production of the PA-31 ceased in 1984.
Features
- Airframe Total Time: 5,978.9
- Engine(s)
- Lycoming TIO 540 J2BD Model 350 HP
- Serial Number: L-68605-61A / L-68606-61A
- Total Time Since New Hrs: 4,653.3 / 4,653.3
- Time Since Overhaul (2010): 957.6 / 957.6
- TBO: 2,000 / 2,000
- Avionics
- #1 Nav/Com/GPS: GNS 530 with WAAS/LPV
- #2 Nav/ Com/GPS: GNS 430 with WAAS
- MFD: Garmin Multi-function display with XM Satellite Sirius Weather/Radio Moving Map with Safe taxi, Charts TAWS Terrain avoidance, TIS Traffic
- EFIS ADI: Garmin G5 Attitude/Flight Director with Airspeed, Altitude and heading display
- HSI: Bendix/King KCS 55 slaved Compass system Compass System
- Transponder: Garmin GTX 300 ES with ADS-B
- ADF: Collins ADF
- Radar Altimeter: King Radar Altimeter KRA10
- Audio Panel: Garmin Audio Panel with ICS
- Autopilot : Garmin Digital GFC 600 Autopilot Flight director coupled for ILS and LPV Approaches w Altitude preselect
- Maintenance Status
- Fresh Annual inspection 1/2021
- No Damage History
- Features/Options
- Panther Navajo 350 HP conversion with 4 blade Hartzell props with syncro/ phaser
- Winglets with recon lights
- Factory Air condition
- Wing lockers
- Cleveland Wheels and Brakes
- American Aviation Intercoolers
- Shadin fuel Totalizer
- GEM digital engine analyzer TIT, individual CHT and EGT and battery monitor
- Gross Weight increase kit with vortex generators and wing fences
- Strobes
- 192 unusable fuel capacity
Location
