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