2020 PILATUS PC 7

2020

PILATUS

PC-7

New

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

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 242 KTAS 448 km/h - at 10,000 ft 250 KTAS 463 km/h Stall speed - flaps and gear up (Vs) 77 KCAS 143 km/h - flaps and gear down (Vso) 69 KCAS 128 km/h g loads Aerobatic Utility - max. positive + 7.0 g + 4.5 g - max. negative – 3.5 g – 2.25 g Max. range 800 nm 1,482 km WEIGHTS Basic empty weight (depending on configuration) 3,792 lb 1,720 kg Max. take-off weight - aerobatic 5,180 lb 2,350 kg - utility 6,283 lb 2,850 kg