Vulcanair P68C

Overview

• The VR P68C is powered by two 200-horsepower Lycoming IO-360 engines that can utilize the aircraft’s 177-gallon fuel load to provide 7 hours of endurance. The aircraft can be configured for 6 passengers or for cargo only.

  Vulcanair P68R

  Vulcanair P68 Observer 2

Specifications

• Powerplant

  (2) Lycoming IO-360-A1B6, 200 hp each

• Propellers

  Hartzell constant speed, full feathering

• Length

  31 ft 4 in

• Height

  11 ft 2 in

• Wingspan

  39 ft 4 in

• Wing Area

  200.23 sq ft

• Wing loading

  23.1 lb/sq ft

• Power loading

  11.6 lb/hp

• Cabin Width

  3 ft 10 in

• Empty Weight

  3,130 bl

• Maximum gross weight

  4,630 lb

• Useful load

  4,336 lb

• Payload with full fuel

• Fuel capacity

  177 gal

• Baggage capacity

  400 lb, 23 cu ft

Performance

• Takeoff distance ground roll

  787 ft

• Takeoff distance over 50-ft obstacle

  1,312 ft

• Rate of climb sea level

  1,100 fpm

• Service ceiling

  18,000 ft

• Landing distance over 50-ft obstacle

  1,969 ft

• Landing distance ground roll

  656 ft

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

  160 KTAS

• Range

Limiting and Recommended Airspeeds

• V_X

• V_Y

• V_NE

• V_S1

• V_SO

  57 KCAS

For more information, contact Vulcanair Aircraft at or via https://www.vulcanair.com/p68c

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.