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PIPER M600 SLS(2022)

Specifications

Year2022
Serial Number4698196
RegistrationN35PK
Total Hours375
LocationUNITED STATES
RegionNORTH AMERICA

Broker

Flightline Group, Inc.

Visit website sales@flightlinegroup.com

Aircraft Details

  • Engine: Pratt & Whitney PT6A-42A, 600 shaft horsepower, TBO 3,600 hours.
  • Avionics: Garmin G3000 suite, synthetic vision, GFC 700 autopilot, dual 12" PFDs, multifunction display, ADS-B equipped, WAAS, and integrated digital cabin pressurization.
  • Propeller: Hartzell 5-bladed propeller.
  • Safety Features: Piper Halo Safety System, Garmin Autoland (fully autonomous), SurfaceWatch, auto throttle, emergency descent mode, automatic level mode, underspeed protection, coupled go-around, electronic stability and protection.
  • Additional Equipment: All Weather Package (GDL 69A XM Radio/Weather, WX-500 Stormscope), Awareness Package (Jeppesen Chartview, TAWS-B, GWX 8000 Weather Radar), second transponder, TCAS I, premium package (110-volt power outlet, Lee CoolView windows, AmSafe seatbelts).
  • Interior: Deluxe six-seat club configuration, Sequoia two-tone (black).
  • Exterior: Matterhorn White top base, Slate Gray bottom base, Convoy Gold trim stripe, black spinner and exhaust.
  • Maintenance: Annual inspection due April 2026, Piper Limited Warranty until December 2026, Garmin Warranty until December 2026, Pratt & Whitney Warranty until December 2028.

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.