What was found
LEFT WING BOTTOM SKIN PANEL NR 2, SKIN CRACKED I/B OF RIB 11, AFT OF REAR SPAR, WRI 57-10 9572, W/C T 6-5710-91017. STOP DRILLED CRACK, AND PERFORMED HFEC INSPECTION IAW A310 NTM 51-10-08 PT6, TO CONFIRM NO CRACK PAST STOP DRILLED AREA. INSTALLED SKIN DOUBLER IAW BA AIRBUS DWG R57249152, REF: E.A. 6-5710-91017, WINGS LT WING BOTTOM SKIN PANEL NR 2 SKIN, CRACK INBD OF RIB 11, AFT OF REAR SPAR.