What was found
LEFT WING UPPER FIXED L/E BETWEEN NR 3 & NR 4 SLATS, COMPOSITE PANEL HAS A APPROXIMATELY EIGHT INCH CRACK. REMOVED DAMAGE, BONDED REPAIR PLIES, TAP TEST GOOD, APPLIED CONDUCTIVE COATING, PRIME & PAINT, INSTALLED TWO LOCK FASTENERS IN STIFFENER BETWEEN SLAT NR 3 & NR 4. CONDUCTIVE TEST CHECK GOOD.