Piper M600

Overview

• Piper’s flagship M600 gains significant capabilities from a new, clean-sheet wing design that adds 90 gallons of fuel capacity and boosts the maximum takeoff weight to 6,000 pounds. Its larger tanks increase the M600’s IFR range with reserves to 1,300 nautical miles. The M600 comes with Garmin’s touchscreen G3000 avionics suite, including autopilot, enhanced automated flight control system, and synthetic vision. Flight into known icing capability and air conditioning also are standard; options include a terrain awareness and warning system, traffic advisory system, and Iridium satellite transceiver.

  Turbine Single-Pilot Directory

  Piper M600

Specifications

• Powerplant

  Pratt & Whitney PT6A-42A, 600 shp

• Propellers

  Hartzel 4 blade Constant Speed

• Length

  29 ft 6 in

• Height

  11 ft 3 in

• Wingspan

  43 ft

• Wing Area

• Wing loading

• Power loading

• Cabin Width

  4 ft 1 in

• Empty Weight

  3,650 lb

• Maximum gross weight

  6,000 lb

• Useful load

• Payload with full fuel

  658 lb

• Fuel capacity

  260 gal usable

• Baggage capacity

  100 lb

Performance

• Takeoff distance ground roll

• Takeoff distance over 50-ft obstacle

  2,635 ft

• Rate of climb sea level

  1,556 fpm

• Service ceiling

  30,000 ft

• Landing distance over 50-ft obstacle

  2,659 ft

• Landing distance ground roll

• Cruise speed/endurance w/45-min rsv, std fuel (fuel consumption, ea engine) @ 75% power, best economy

  274 KTAS

• Range

Limiting and Recommended Airspeeds

• V_X

• V_Y

• V_NE

• V_S1

• V_SO

For more information, contact Piper Aircraft Inc at or via https://www.piper.com/model/m600sls/

All specifications are based on manufacturer's calculations. All performance figures are based on standard day, standard atmosphere, sea level, gross weight conditions unless otherwise noted.