The Guimbal Cabri G2 is a two-seat light piston helicopter designed and manufactured by Hélicoptères Guimbal in France. Developed as a modern trainer and utility rotorcraft, it incorporates advanced safety features, composite materials, and crash-resistant systems typically found on larger turbine helicopters. The Cabri G2 was conceived by former Eurocopter engineer Bruno Guimbal to address the needs of flight schools and private owners seeking a reliable, low-maintenance, and safety-focused aircraft in the light piston category.
The Cabri G2 first flew in April 2005, received European certification in December 2007, and entered production shortly thereafter. It features a fully articulated three-blade main rotor system made of composite materials, a fenestron-type enclosed tail rotor for enhanced safety, and a robust skid landing gear. Power is provided by a Lycoming O-360-J2A four-cylinder piston engine producing 145 horsepower, driving the helicopter to a maximum cruise speed of approximately 100 knots. The aircraft’s maximum takeoff weight (MTOW) is 1,543 pounds, with a useful load of around 529 pounds.
In standard configuration, the Cabri G2 accommodates two occupants in a side-by-side cockpit, optimized for training with dual controls, excellent visibility, and modern avionics. The design prioritizes safety with features such as energy-absorbing seats, a crash-resistant fuel system, and a low vibration level due to its advanced rotor technology.
With a maximum range of approximately 380 nautical miles and endurance exceeding 5 hours, the Cabri G2 has become a popular choice for ab initio training, private ownership, and specialized missions requiring a compact yet highly capable light helicopter.
