1992


Guimbal Cabri G2


Ultralight helicopters





  • Guimbal Cabri G2
  • Guimbal Cabri G2

First flew in 1992, the Cabri is a two-seat light helicopter powered by a Lycoming O-360-J2A piston engine. Entered serial production in 2005.

As of June 2019, the global fleet of Cabri G2 have flown over 260,000 flight hours and Guimbal’ factory in Aix en Provence, France has completed the 250th helicopter


Specifications Cabri G2


Engine 1 x Lycoming O-360-J2A 145 shp
Capacity 1 + 1
Length (m) 6.31
Height (m) 2.37
Blades 3
Rotor diam. (m) 7.2
Disc area (m2) 41
Weight (kgs)     Max: 700
Speed (km/h) Cruise: 160
Range (km) 700
Ceiling (m) 3900
Rate/Climb (m/min)
blueprints


  Derivatives & Versions of Cabri G2


ModelYearHistory
AH VSR700

2018
2018 A light military rotary-wing tactical unmanned aerial vehicle, the VSR700 is being developed jointly by Airbus Helicopters and Helicopteres Guimb ...






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