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Specifications

Specifications
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Specifications

Product catalog summary
Specifications & Features
  • The Cabri G2 is a two-seat helicopter certified by multiple international aviation authorities including EASA, FAA, and others.
  • Key features include electronic CDI ignition, a digital engine governor, two-axis electric trim, and high-energy crash-certified stroking seats.
  • Safety features comprise a vibration absorbing system, rotor brake, four-point harnesses with inertia reel, and a CO sensor.
  • Comfort and convenience are enhanced with a cabin heater, dual cabin vents, keyless entry, and removable copilot controls.
  • The helicopter is equipped with a multi-function vehicle and engine monitor, featuring a multiple limit indicator, engine parameters, and a high precision capacitive fuel gauge.
  • Standard day VFR equipment includes a VHF, intercom, ADS-B OUT transponder, and ELT, with optional night-VFR suite available.
Main Characteristics
  • The helicopter features a three-bladed main rotor with composite blades and a shrouded tail rotor.
  • The main structure is made from autoclaved carbon fiber/epoxy honeycomb sandwich.
  • It is powered by a Lycoming O-360-J2A engine, providing 180 hp flat-rated to 160 hp for takeoff and 145 hp continuous.
  • The helicopter includes an anticrash fuel tank with a capacity of 170 L and a luggage compartment of 200 L.
Performance
  • Maximum gross weight is 700 kg, with an empty weight of 430 kg.
  • Maximum cruise speed is 100 KIAS, with a VNE at sea level of 130 KIAS.
  • Hover ceiling IGE at max gross weight is 5000 ft, and 7500 ft with two 77 kg people and 2 hours of fuel.
Main Optional Equipment
  • Options include night VFR/day VFR avionics, fully integrated pop-up floats, cargo hook, heated pitot, multi-purpose chin mount, bearpaws, IR blocking windows, and air conditioning.
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Catalog excerpts

Specifications-1

SPECIFICATIONS & FEATURES Two-seat helicopter certified by EASA (Europe), FAA (USA), TCCA (Canada), CASA (Australia), NZCAA (New Zealand), SACAA (South Africa), CAAV (Vietnam), CAAC (China), ANAC (Brazil), UK CAA (United Kingdom), CAAM (Mongolia), CAAI (Israel) and CAAT (Thailand). BASE EQUIPMENT Electronic CDI ignition Digital engine governor Two-axis electric trim High-energy crash-certified stroking seats Vibration absorbing system Rotor brake Four-point harnesses with inertia reel Cabin heater Dual cabine vents Keyless entry and starting lock Removable copilot controls Easy-to-adjust pilot pedals (copilot option) Handling wheels Carry-on cabin flight bag Multi-function vehicule and engine monitor featuring: Multiple Limit Indicator Engine parameters High precision capacitive fuel gage Multi-mode fuel flow indicator MGB & TGB chip detector Automatic carburetor heating system CO sensor Flight log AVIONICS Standard day VFR equipment including one VHF, an intercom, an ADS-B OUT transponder and an ELT Night-VFR suite (optional - depending on local authority requirements) Cristal Panel (Garmin G500H TXi and Mid-Continent SAM) Aspen EFD 1000 (Digital PFD / HSI) Various configurations with a choice of Garmin GPS, ADS-B IN transponder, VOR, CDI, second VHF and gyros Headset sockets: NATO & LEMO Power supply Pilot and Copilot iPad support

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