1974 Piper Navajo PA-31-350
Description
The Piper PA-31-350 Navajo is a six-seat, twin-engined aircraft designed and built by Piper Aircraft. It was first introduced in 1974 and has been in production since then. The Navajo is powered by two Lycoming TIO-540-A1A turboprop engines, each producing 350hp. The aircraft has a maximum range of 1,500 miles and a maximum cruise speed of 232 knots. It has a wingspan of 40 feet and a length of 33 feet. The aircraft is capable of operating from both paved and unpaved surfaces. It is used primarily for business and corporate travel, and is also popular with air charter companies.
Features
- 7,254.8 Hours Total Time
- Engine(s)
- Lycoming LTIO-540-F2BD (TBO 2,000
- Engine 1
- SN: L-224-61A
- 664 TSO (3/2014)
- Engine 2
- SN: RL-1062-68A
- 268 TSO (2/2017)
- Prop Details
- Hartzel HC-E3YR-2AFTF
- Left Prop
- 30 TSO (7/2021)
- Right Prop
- 78 TSO (11/2020)
- Avionics
- 2x Aspen Evolution 1000/ 500 w/ Synthetic vision
- Garmin GTN 750 and 650
- Auto Pilot Bendix FCS-810 Automatic 5
- TCAS Garmin GTS 800
- Radar Garmin GX-70
- 2x Garmin GTX Transponders
- Mid Continental digital clock
- KR87 ADF
- Wind and stabilizer deicing boots
- Prop heat
- Wing ice detection light LED
- Windshield heat pilot side
- Windshield wipers
- 2 LED landing lights
- NAV lights LED
- Beacon light LED
- Strobes
- All panel lights LED
- Maintenance Status
- Annual done 09/01/2022
- Single Pilot in Command Certificate
- 9 PAX/Cargo
- Features/Options
- Wind and stabilizer deicing boots
- Prop heat
- Wing ice detection light LED
- Windshield heat pilot side
- Windshield wipers
- 2 LED landing lights
- NAV lights LED
- Beacon light LED
- Strobes
- All panel lights LED
Location
