The LCA LH 212 Delta is a two-seat Italian piston engine ultralight helicopter first flown in 2010.
The tail rotor, mounted on the starboard side of the boom, has its two blades protected from ground strikes by a long, curved tubular bumper.
[1] A governor sets the throttle in the absence of pilot input and trim is applied electrically.
[1] A 84.5 kW (113 hp) Rotax 914 turbocharged, liquid cooled, flat four piston engine with narrow rectangular cheek radiators is mounted behind the seats and partly exposed at the rear, driving a two blade main rotor.
[1] The first flight was in 2010 and marketing began in September 2011 at the Blois international ultra light show.