page_title: Pilatus PC-12
section_title: Specifications (PC-12NG)
hierarchical_section_title: Pilatus PC-12 / Specifications (PC-12NG)
caption_attribution_description: Landing at rwy 25R Barcelona BCN/LEBL
context_page_description: The Pilatus PC-12 is a single-engine turboprop passenger and cargo aircraft manufactured by Pilatus Aircraft of Stans, Switzerland, since 1991. The main market for the aircraft is corporate transport and regional airliner operators. The PC-12 is the best-selling pressurized single-engine turbine-powered aircraft in the world and has been for several consecutive years, with 1,700 deliveries as of October 2019.
context_section_description: Data from Pilatus
  General characteristics
  Crew: 1 or 2
  Capacity: 6 to 9 passengers seats
  Length: 14.4 m (47 ft 3 in)
  Wingspan: 16.28 m (53 ft 5 in)
  Height: 4.26 m (14 ft 0 in)
  Wing area: 25.81 m² (277.8 sq ft)
  Airfoil: root: NACA LS(1)-0417MOD; tip: NACA LS(1)-0313
  Empty weight: 2,810 kg (6,195 lb)
  Max takeoff weight: 4,740 kg (10,450 lb) 
  Maximum landing weight: 4,500 kg (9,921 lb)
  Maximum zero fuel weight: 4,100 kg (9,039 lb)
  Fuel capacity: 1,226 kg (2,703 lb) / 1,521 l (402 US gal; 335 imp gal)
  Powerplant: 1 × Pratt & Whitney Canada PT6A-67P turboprop engine, 890 kW (1,200 shp)
  Propellers: 5-bladed Hartzell Propeller composite, 2.67 m (8 ft 9 in) diameter composite constant-speed fully-feathering reversible propeller
  Performance
  Cruise speed: 528 km/h (328 mph, 285 kn)
  Stall speed: 124 km/h (77 mph, 67 kn)
  Range: 3,417 km (2,123 mi, 1,845 nmi) (HSC, VFR Reserves)
  Service ceiling: 9,144 m (30,000 ft)
  Rate of climb: 9.75 m/s (1,919 ft/min)
  Take-off run to 15 m (49 ft): 793 m (2,602 ft)
  Landing run from 15 m (49 ft): 661 m (2,169 ft)
  Fuel consumption: 250 l/h (66 gal/h; 55 imp gal/h) (915 km (569 mi; 494 nmi) trip, including climb, cruise and descent, 491 km/h (305 mph; 265 kn) average block speed)
  Avionics
  Honeywell Primus Apex
caption: Side view, flaps and gear down
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