2020 PILATUS PC 9
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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