Pilatus Turbo Prop Aircraft

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Pilatus Turbo Prop

Specifications

  • Crew: 1 or 2 pilots
  • Capacity: 6 to 9 passengers/seats
  • Payload: (full fuel, pilot on board)
  • Cargo: 704 kg (1602 lb)
  • 9 Passengers: 623 kg (1423 lb)
  • 6 Executive: 438 kg (1014 lb)
  • Length: 14.40 m (47 ft 3 in)
  • Wingspan: 16.28 m (53 ft 4 in)
  • Height: 4.26 m (14 ft 0 in)
  • Wing area: 25.81 m² (277.8 ft²)
  • Aspect ratio: 10.27
  • Empty weight: with 1 pilot
  • Cargo: 2,810 kg (6,194 lb)
  • 9 Passengers: 2,891 kg (6,373 lb)
  • 6 Executive : 3,076 kg (6,782 lb)
  • Maximum takeoff weight: 4,740 kg (10,500 lb)
  • Maximum landing weight: 4,500 kg (9,921 lb)
  • Maximum zero fuel weight: 4,100 kg (9,039 lb)
  • Usable fuel: 2,704 lb (1,226 kg), 1,520 l (402 US gal)
  • Maximum payload: (pilot on board)
  • Cargo: 1290 kg (2845 lb)
  • 9 Passengers: 1209 kg (2666 lb)
  • 6 Executive: 1024 kg (2257 lb)
  • Tail wingspan: 5.20 m (17 ft 1 in)
  • Propeller: 5 blade Hartzell Composite
  • Propeller diameter: 2.67 m (8 ft 9 in)
  • Propeller RPM: 1,700 rpm
  • Power plant: 1 Pratt & Whitney Canada PT6A-67P turboprop, 1,200 shp (895 kW)
  • Cruise speed: 528 km/h (285 kn)
  • Stall speed: 124 km/h (67 kn)
  • Range: 3,417 km (HSC, VFR Reserves) (1,845 nmi)
  • Service ceiling: 9,144 m (30,000 ft)
  • Rate of climb: 585 m/min (MTOW) (1,920 ft/min)
  • Wing loading: 183.6 kg/m² (37.8 lb/(sq ft))
  • Power/mass: 5.3 kg/kW (8.75 lb/hp)
  • Takeoff distance: 793 m (2,602 ft), 15 m / 50 ft obstacle
  • Landing distance: 661 m (2,170 ft), 15 m / 50 ft obstacle
  • Fuel consumption: 250 l (66.0 US gal) per hour (500 nmi trip, includes climb, cruise and descent, 265 kn average block speed)

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