What was found
LEFT WING SPAR AREA, TOP SKIN STIFFENER AT WIAX 13-9 HAS A CRACK. MATERIAL ID FOR THE REPAIR IS 7075-T6 0.110 60-7018 EXTRUSION PO 566980.6 IAW A300-600 SRM 57-51-11, FIG 207 AND DWG NR A57241059. FABBED REPAIR ANGLE IAW A300-600 SRM 57-51-11, FIG 207. ALODINED AND PRIMED IAW A300-600 SRM 1-21-10, PG 3, AND 51-23-10, PG 24. INSTALLED REPAIR IAW A300-600 SRM 57-51-11, FIG 207 AND SRM 51-40-21, PG 7.