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Pilatus PC-12 prop plane review

Pilatus PC-12 prop plane review

Pilatus PC-12 prop plane review

Pilatus PC-12
When you’re seeking world-class craftsmanship, no country has a more famed reputation than the Swiss. And where is precision craftsmanship more important than in a plane? That’s why a safe choice for air transportation is the Pilatus PC-12 turboprop plane. Since 1939, Pilatus Aircraft has stood for Swiss quality and innovation. Indeed, the skies are your bowl of cherries when you’re flying a Pilatus PC-12 that’s powered by a Pratt & Whitney Canada PT6A-67B engine that reaches a maximum cruising speed of 312 mph. Fly by yourself in this “Best Of” turboprop and you can travel an impressive 2,593 miles. Load it up with nine passengers and you still can travel 1,753 miles at a comfortable cruising altitude of 30,000 feet. The Pilatus PC-12 offers a large interior with lots of flexibility because seats are removable. Since it can land in less than 1,000 feet of runway, the Pilatus PC-12 is a favorite of executives on the go who need to fly in and out of smaller airports.

Pilatus Aircraft, Ltd.
P.O. Box 992
6371 Stans, Switzerland
www.pilatus-aircraft.com

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FEATURES
  • Crew: one or two pilots
  • Capacity: 9 passengers standard, 6 executive
  • Length: 14.40 m (47 ft 3 in)
  • Wingspan: 16.23 m (53 ft 3 in)
  • Height: 4.26 m (14 ft 0 in)
  • Tail wingspan: 5.20 m (17 ft 1 in)
  • Wing area: 25.81 m² (277.8 ft²)
  • Wing loading: 174.3 kg/m² (35.7 lb/ft²)
  • Empty: 2,661 kg (5,867 lb)
  • Loaded: 4,500 kg (10,450 lb)
  • Maximum takeoff: 4,700 kg (10,450 lb)
  • Maximum landing: 4,500 kg (9,921 lb)
  • Maximum payload: 1,600 kg (3,502 lb)
  • Maximum payload full fuel: 539 kg (1,189 lb)
  • Powerplant: 1x Pratt & Whitney Canada PT6A-67B turboprop, 895 kW (1,200 shp)
  • Propeller: Hartzell HC - E4A - 3D/E10477K – 4 blade aluminum
  • Propeller diameter: 2.67 m (8 ft 9 in)
  • Propeller RPM: 1,700 rpm constant speed
  • Maximum cruise speed: 500 km/h (312.5 mph) (270 KTAS)
  • Stall speed, landing configuration: 120 km/h (74.8 mph) (65 KCAS)
  • Range 0 passenger: 4,149 km (2,593 mi) (2,239 NM)
  • Range 9 passenger: 2,804 km (1,753 mi) (1,513 NM)
  • Service ceiling: 9,150 m (30,000 ft)
  • Rate of climb: 512 m/min (1,680 ft/min)at sea level
  • Power loading: 3.7 kg/shp (8.2 lb/shp)
  • Takeoff distance over 15 m (50 ft) obstacle: 701 m (2,300 ft)
  • Takeoff distance ground roll: 450 m (1,475 ft)
  • Landing distance over 15 m (50 ft) obsacle: 558 m (1,830 ft)
  • Landing distance ground roll: 228 m (945 ft)


 
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