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AC4 CS-LSA Characteristics two-seated high wing aircraft. MTOW 600 kg . payload 235 kg .100 PS injection engine Rotax motor typ 912 iS (Sport)

The Lightwing AG was founded in 2000 with the aim to develop light aircraft to build and distribute. Since 2011, the introduction of CS-LSA rules by EASA Lightwing working on the EASA approval of in-house development AC4 CS-LSA. " Simple, robust and inexpensive, equipped according to the prior art "is supposed to be the new aircraft.

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