As promised, we are posting some major design changes, that will be incorporated in production aircraft versus prototype.

Wing dihedral from 4 to 6 degrees

Original 4 degrees

Wing 3D documentation and laminate plan according to new design (bigger flap and aileron area, different flap design, optimised laminate plan and location of hardware) is finished.
We are starting production of wing for static test with load cases for CS-LSA certification on Monday 27th February, test is planned for mid March.
We promise to publish test video and pictures as soon as it is done.