Specifications
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Two-seat helicopter certified by EASA (Europe), FAA (USA), TCCA (Canada), CASA (Australia), NZCAA (New-Zealand), SACAA (South Africa), CAAV (Vietnam), CAAC (China) and ANAC (Brazil). Electronic CDI ignition Digital engine governor Two-axis electric trim with Pilot & Copilot control High-energy crash-certificated stroking seats Vibration absorbing system Disc rotor brake with overhead control Four-point harnesses with inertia reel Cabin heater Dual cabin vents Keyless entry and starting lock Fast - removal Copilot controls Easy-to-adjust Pilot pedals (Copilot optional) Handling wheels Carry-on cabin flight bag Multi-function vehicle & engine monitor featuring: • Smart power indicator • High precision capacitive fuel gage • Fuel flow with displays: - Flight time remaining, - Instant fuel flow, - Average fuel flow, • Self-closing / self-testing chip detectors - MGB & TGB • Automatic carburetor heater • Carbon monoxide detector • Flight time counter • Flight log • Stopwatch • Engine parameters The standard Day-VFR equipment includes one COM, an Intercom, a mode S transponder and a 406 MHz ELT Night-VFR suite (optional - depends on national requirements) Different configurations with a choice of GPS, VOR, second COM Standard headset sockets: NATO & LEMO Add. Weight Night VFR / day VFR avionics 0 to 3 kg (0 to 6.6 lbs) Max gross weight 700 kg (1540 lbs) Smart iPad holder w. power supply 0.4 kg (0.90 lbs) Empty weight 430 kg* Fully-integrated pop-out floats 20 kg (44 lbs) (w. automatic activation) Belly cargo hook (220 kg capacity) 1.2 kg (2.6 lbs) Heated pitot Multi - purpose bearpaws Digital PFD / HSI (Aspen) IGE hover ceiling ISA, maximum gross weight (3.5 lbs) IGE hover ceiling ISA, two 77kg (170 lbs) people and 2-hour fuel Document updated in March 2017 (*): These data are given on a fair basis but are not contractual. Individual aircraft characteristics may vary slightly.