PC-6/B2-H4 Turbo Porter

Pilatus

фотография с сайта www.airliners.net

PC-6 Specification / Performance
 Performance Max cruise speed 125 ktas 232 km TAS
   Stall speed (idle power) with flaps up 58 ktas 108 km TAS
   Stall speed (idle power) with flaps down 52 ktas 97 km TAS
   Max range (optimum speed, no reserves, at 10'000 ft) 500 nm 927 km
   Endurance at optimum speed, no reserves 4 h 20 min   
   Max range with underwing tanks * 870 nm 1'612 km
   Endurance with underwing tanks * 7 h 35 min   
   Max operating altitude 25'000 ft 8'197 m
   Take-off ground roll at sea level 646 ft 197 m
   Take-off distance over 50 ft obstacle 1'558 ft 475 m
   Take-off distance over 50 ft obstacle (STOL) 1'443 ft 440 m
   Max rate of climb at sea level 1'010 ft/min 331 m/min
   Max rate of climb at 5'000 ft 935 ft/min 307 m/min
   Average fuel consumption 39 US Gal/h 148 ltr/h
           
Weights Max ramp weight 6'195 lb 2'810 kg
   Max take-off weight 6'173 lb 2'800 kg
   Max landing weight 5'863 lb 2'660 kg
   Max zero fuel weight 5'291 lb 2'400 kg
           
Powerplant Pratt & Whitney Canada PT6A-27   
   Take-off power (flat rated) 550 SHP   
   Thermodynamic power 680 SHP   
   Propeller, constant speed, fully reversing 3 blade Hartzell (Aluminum)
   Propeller speed 2000 rpm   
   Time between overhaul 3'600 hr   

Сайт разработчика: www.pilatus-aircraft.com