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Airframe
Maximum Take-Off Weight: 4,500 kg
Empty Aircraft Weight: 2,700 kg
Useful Load: 1,800 kg (+-4%)
Fuel Consumption / hour: 290 kg ~ 310 kg
Maximam Speed: 168 ~ 169 kt/h = 311 ~ 313 km/h
Cruising Speed:
- 140 kt/h = 259 km/h (with fixed landing gear)(+-4%)
- 150 kt/h = 278km/h (with retractable landing gear)(+-4%)
Range (without additional tank):
- 460 nm = 852 km (with fixted landing gear)
- 500 nm = 926 km (with retractable landing gear)
Maximum Endurance (without additional tank):
- 2.96 ~ 3.17 Hrs
Engine(s)
Two Pratt & Whitney Canada 210A turboshaft engines (1,000 shp x 2 units)
APU mode on left hand side engine
Two anti icing fuel systems and two magnetic chip detectors (one per engine)
Two independent dual-channel FADEC systems (one per engine)
Engine Control Panel
Engine bay group (engine mounts, firewalls, cowlings, drains, exhausts)
Fire detection system
Fire extinguisher system
Fire Detection and Extinguisher Control Panel (1)
Electrical System
DC primary power generation system: 28 V DC provided by two independent 300 starter generators
Avionics/Radios
STANDARD AVIonICS PACKAGE