1.Allocating all components and inspection for damages performed according PARTS LIST 357M8 Flap T/E 2.Folowing the DWG 357M8 and instruction for assembly of the L/H wing T/E Flap, internal and external structural components joined and drilled through the pilot holes for initial pre- assembly of the Flap. 3. Final geometry check of L/H wing T/E Flap assembly performed. 4. All holes in the structural parts drilled to final diameter and deburred as per the drawing 357M8
