Specifications
Aircraft Details
- Model: PIPER M600 SLS
- Condition: Used
- Flight Rules: IFR
- Max Ramp Weight: 6,050 lb
- Max Takeoff Weight: 6,000 lb
- Max Landing Weight: 5,800 lb
- Basic Empty Weight: 3,755 lb
- Useful Load: 2,245 lb
- Fuel Capacity: 260 gal
- Engine: Pratt & Whitney PT6A-42A, 809 hours since new, TBO 3600 hours
- Propeller: Hartzell HC-E4N-3Q, 809 hours since new
- Avionics: Garmin G3000 suite, dual 12” PFDs, GFC-700 autopilot, ADS-B equipped
- Safety Features: HALO Safety System, FIKI (Flight Into Known Icing), engine fire detection system
- Interior: 6 seats in executive configuration, light gray with diamond stitching, USB ports and individual cup holders at each seat
- Exterior: Matterhorn white and dark blue with silver accents, ceramic coating applied in 2025
- Maintenance: Meticulously maintained at Piper Service Center, complete and continuous logbooks available
- Inspection Status: Annual inspection due February 2026, currently in progress
About this Model
Overview
The Piper M600/SLS is a pressurized, single-engine turboprop positioned between high-end pistons and entry-level light jets for buyers prioritizing simplified operation, runway flexibility, and contemporary safety automation. The SLS (Safe Landing System) variant centers the aircraft around Garmin’s Autoland capability, pairing it with a high-integration avionics suite and a cabin sized for practical regional missions with family, colleagues, or a small team.
Mission Fit
In day-to-day use, the M600/SLS fits missions where a single pilot wants turbine reliability and speed without stepping into jet operating complexity. It is typically chosen for point-to-point regional travel, mixed weather flying with IFR avionics, and destinations where runway length and support infrastructure are limited. Mission planning should account for passenger count, fuel, and baggage tradeoffs common to single-engine turboprops.
Cabin
The cabin is arranged as a club-style configuration in a pressurized fuselage with an enclosed feel compared with unpressurized aircraft. Seating and storage are oriented toward practical travel rather than stand-up cabin movement, and comfort is strongly influenced by interior package, seat design, and noise/vibration management typical of turboprops. Access and loading are straightforward for small groups and normal travel baggage, with best comfort realized when passenger count is kept to a manageable level for the stage length.