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Grob G-120A

The Grob G-120A aircraft is build by Grob Aircraft.

The Grob G-120A is a two seated training and aerobatic low-wing aircraft with a carbon composite airframe, built by Grob Aircraft. The airframe can be stressed to +6 and -4g. Its minimum service life is just over 15,000 flight hours. G-120A provides the good training platform for the full range of conventional high-performance aerobatic maneuvers, including spins, inverted spins, loops, rolls, stall turns, outside turns and recovery from unusual attitudes. The cockpit provides room for students wearing military equipment and helmets. The plane is equipped with movable seats and rudder pedals and an air conditioning system.

Grob G-120A has a seating capacity of 2, side-by-side.

Grob G-120A has an overall length of 8.11 meters (26.5_ft). It has a wing span of 10.18 meters (33.3_ft). The wing area of Grob G-120A is of about 13.3 sq.meters (143.2_sq.ft.).

The piston engine powered Grob G-120A uses 1, Lycoming AEIO-540-D4D5. It has a propeller with 3, blades turning in a constant speed. It can deliver a total power of approximately 194 kilowatts (260.2_shaft horsepower).

Updated On: 18.10.15