Daher Kodiak 100

Overview

• The Kodiak was designed for missionary and humanitarian flying in the remotest parts of the world to replace the aging Cessna 185s and 206s and de Havilland Beavers, all of which are still prowling the planet in support of backcountry operations. But they are increasingly difficult to maintain. And piston engines can be expensive to fuel in the many parts of the world where avgas is nearly impossible to get. The Kodiak’s 700-shaft-horsepower variant of the venerable PT6 turboprop simplifies operations, reduces maintenance, increases reliability, and—although it burns more per hour—actually reduces fuel costs in many places.

  Daher Kodiak 100

  Daher Kodiak 100: Ramp Appeal

Specifications

• Powerplant

  Pratt & Whitney PT6A-34, 750 shp

• Propellers

  Constant speed, feathering, reversible

• Length

  33 ft 10 in

• Height

  14 ft 8 in

• Wingspan

  45 ft

• Wing Area

  240 sq ft

• Wing loading

  30.2 lb/sq ft

• Power loading

  9.67 lb/hp

• Cabin Width

  4 ft 6 in

• Empty Weight

  3,775 lb

• Maximum gross weight

  7,305 lb

• Useful load

  3,530 lb

• Payload with full fuel

  1387 lb

• Fuel capacity

  320 gal

• Baggage capacity

  248 cu ft

Performance

• Takeoff distance ground roll

  934 ft

• Takeoff distance over 50-ft obstacle

  1,468 ft

• Rate of climb sea level

  1,340 fpm

• Service ceiling

  25,000 ft

• Landing distance over 50-ft obstacle

• Landing distance ground roll

  765 ft

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

  174 KTAS/5.8 hr (48 gph)

• Range

Limiting and Recommended Airspeeds

• V_X

• V_Y

• V_NE

• V_S1

  77 KCAS

• V_SO

  60 KCAS

For more information, contact Daher at or via https://kodiak.aero/

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.