Tarragon

Overview

• The Tarragon is a high-performance, ultralight aircraft known for its speed, efficiency, and unique design. It's a two-seater, low-wing aircraft with retractable landing gear and a sleek, carbon fiber construction. The Tarragon is designed to comply with Fédération Aéronautique Internationale microlight rules and has been certified in Latvia. 

  Tarragon

Specifications

• Powerplant

  Rotax 915, 141 hp (as tested) or 916, 160 hp

• Propellers

• Length

  24 ft 8 in

• Height

  8 ft 2 in

• Wingspan

  26 ft 1 in

• Wing Area

• Wing loading

• Power loading

• Cabin Width

  27.5 in

• Empty Weight

  930 lb

• Maximum gross weight

  1,650 lb

• Useful load

  720 lb

• Payload with full fuel

  468 lb

• Fuel capacity

  42 gal

• Baggage capacity

  80 lbs

Performance

• Takeoff distance ground roll

• Takeoff distance over 50-ft obstacle

• Rate of climb sea level

• Service ceiling

• Landing distance over 50-ft obstacle

• Landing distance ground roll

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

  170 KTAS, 5 hours with VFR reserves

• Range

  1025 nm

Limiting and Recommended Airspeeds

• V_X

• V_Y

• V_NE

  200 KIAS

• V_S1

• V_SO

  48 KCAS

For more information, contact at or via https://www.tarragonaircraft.com/

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.