PC-7 MkII Fact Sheet
Transcription
PC-7 MkII Fact Sheet
PC-7 mkII the basic trainer PC-7 MkII THE BASIC TRAINER Since its introduction in 1994, the PC-7 MkII has come with an exceptional standard of equipment, performance and cost-effectiveness in this class of training aircraft. Offering a reliable and economic training platform, the docile behaviour of the PC-7 MkII in the hands of a beginner provides a confidencebuilding environment for inexperienced cadets. With its highly costefficient PT6A-25C engine, it provides the lowest engine operating costs of all turboprop trainer aircraft. The use of airframe and avionics systems common with the PC-9 M enables owners and operators to profit from the benefits of a combined infrastructure established at Pilatus to support both these aircraft types. TRAINING ROLES - Ab Initio Training - Basic Flying Training FEATURES Hartzell four-blade aluminium propeller Birdstrike resistant canopy Ejection seats PERFORMANCE The PC-7 MkII, in the aerobatic configuration, at MTOW, 5,180 lbs (2,350 kg) has the following performance under international standard atmospheric (ISA) conditions: Take-off distance over 50 ft (15 m) obstacle at sea level 1,500 ft 457 m Landing distance over 50 ft (15 m) obstacle at sea level 2,255 ft 687 m Max. rate of climb, sea level 2,675 ft/min 13.59 m/sec Max. operating speed (Vmo) 300 KEAS 556 km/h Max. cruise speed (VH) - at sea level - at 10,000 ft 242 KTAS 250 KTAS 448 km/h 463 km/h Stall speed - flaps and gear up (Vs) - flaps and gear down (Vso) 77 KCAS 69 KCAS 143 km/h 128 km/h g loads - max. positive - max. negative Aerobatic + 7.0 g – 3.5 g Utility + 4.5 g – 2.25 g 800 nm 1,482 km Basic empty weight (depending on configuration) 3,792 lb 1,720 kg Max. take-off weight - aerobatic - utility 5,180 lb 6,283 lb 2,350 kg 2,850 kg Max. range Anti-g system 700 shp Pratt & Whitney PT6A-25C engine (850 shp thermodynamic rating) On-board oxygen generating system (OBOGS) Stepped, tandem seating with full dual-glass cockpit Six underwing hardpoints 10 ft 8 in (3.26 m) typical WEIGHTS 8 ft (2.44 m) dia. PC-7 MkII 7 ft 7 in (2.31 m) 8 ft 4 in (2.54 m) 33 ft 4 in (10.18 m) Wing area 175.27 ft 2 (16.28 m2 ) STA0214E 12 ft 3 in (3.66 m) 33 ft 5 in (10.19 m) 3 ft 2 in (0.97 m) www.pilatus-aircraft.com
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