2020 PILATUS PC 9


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    Aircraft Summary


    General

    Year
    2020
    Manufacturer
    PILATUS
    Model
    PC-9
    Serial Number
    NA
    Condition
    New
    Description
    Since its launch in 1986, the PC-9 has established itself as a leader among turboprop trainers, offering superior training value for air forces around the world. Noted for its aerodynamic yet stable handling qualities, it has all the right attributes to develop the skills of student pilots from ab initio through basic training, and with sufficient power for the more demanding advanced phases of training. Recent upgrades to the PC-9 M include large primary and secondary flight displays to transform the aircraft into a true glass-cockpit trainer. With this modern cockpit environment, high performance and agile handling, the PC-9 M is an ideal training platform for the wide range of training syllabi in use today.

    Airframe

    Airframe Notes
    PERFORMANCE The PC-9 M, 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 1,300 ft 397 m Landing distance over 50 ft (15 m) obstacle at sea level 2,255 ft 687 m Max. rate of climb, sea level 3,880 ft/min 19.7 m/sec Max. operating speed (Vmo) 320 KEAS 593 km/h Max. cruise speed (VH) - at sea level 271 KTAS 502 km/h - at 10,000 ft 298 KTAS 552 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 860 NM 1,593 km WEIGHTS Basic empty weight (depending on configuration) 3,926 lb 1,781 kg Max. take-off weight - aerobatic 5,180 lb 2,350 kg - utility 7,055 lb 3,200 kg


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