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2010
Pilatus PC-6 Fact sheet
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Fly Club
December 5, 2010
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Aeroplanes
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PC-6 TURBO PORTER ANYWHERE, ANYTIME, IN ANY ENVIRONMENT PC-6 TURBO PORTER ANYWHERE, ANYTIME, IN ANY ENVIRONMENT The Pilatus PC-6 Turbo Porter has become a legendary aircraft, known around the world simply as "the Porter". Its unique short take-off and landing (STOL) capabilities, reliability and versatility in all weather and terrain conditions have established the reputation of the PC-6 as a rugged utility aircraft. The Porter is fully capable of operating from different types of unprepared, rough and short airstrips, in remote areas, at high altitudes and in all climates. A simple but solid construction, proven systems and features, combined with precision workmanship result in the highest reliability and lowest maintenance possible. No matter whether high and hot or low and snow - anywhere, anytime you can rely on the Porter as a high quality, life-long investment. WEIGHTS Basic empty weight 1 Max. take-off weight Max. landing weight Max. payload 1 Payload with max. fuel 1 1 approx. 2,756 - 3,086 lb 6,173 lb 5,863 lb up to approx. 2,646 lb up to approx. 2,381 lb (1,250 - 1,400 kg) (2,800 kg) (2,660 kg) (1,200 kg) (1,080 kg) Depending on configuration and fuel FEATURES 550 shp Pratt & Whitney Canada PT6A-27 turpoprop Engine (680 shp thermodynamic rating) Cockpit designed for single pilot operation (control stick and rudder pedals for co-pilot available as an option) Individual exterior paint scheme according to customer’s definition Easy conversion for various missions such as transport, para-dropping, aerial photography, surveillance, search and rescue, etc. Large cabin (over 3 m3) and up to 10 passengers or over 1,000 kg payload PERFORMANCE The PC-6/B2-H4 has the following performance under international standard atmospheric (ISA) conditions: Take-off distance over 50 ft (15 m) obstacle (STOL) 1,444 ft Landing distance over 50 ft (15 m) obstacle (STOL) 1,033 ft Rate of climb (MTOW) Max. cruise speed Max. range at 10,000 ft - with underwing tanks Max. operating altitude Stall speed (MTOW) - flaps up (Vs) - full flaps set (Vso) (440 m) (315 m) 1,010 ft/min (5.13 m/sec) 125 KTAS 500 NM 870 NM 25,000 ft 58 KEAS 52 KEAS (232 km/h) (926 km) (1,611 km) (7,620 m) (107 km/h) (96 km/h) Hartzell three-blade aluminium propeller (four-blade available as an option) Landing gear designed to operate from different types of unprepared airstrips (floats and skis available as options) Large sliding doors left and right side Trap door (in flight operation) available as an option Passenger seat stowage in the rear part of the fuselage 2.67 m (8 ft 9 in) dia. 3.00 m (9 ft 10 in) 10.90 m (35 ft 9 in) Wing area 30.15 m2 (324.54 ft2) 15.87 m (52 ft 1 in) www.pilatus-aircraft.com 5.70 m (16 ft 10 in) 3.20 m (10 ft 6 in)
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