As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REPAIR LT L/E WING BETWEEN WINGTIP LENS AND NR 1 SLAT. REMOVED PANEL & RIB AT LT L/E WING BETWEEN WINGTIP & NR 1 SLAT IAW SRM 51-30-2. HEAT TREATED RIB FROM 2024-0 .040" TO 2024-T4 IAW FASI ENG REPORT NR2-371-53-801 REV A. NEW RIB MATERIAL USED 2024-0 .040" PO F29146179, DIM 22.1250" X 5.5" IAW SRM 57-20-2, FIG 1 & 51-20-01. TREATED AND PRIMED NEW RIB IAW SRM 51-10-2. INSTALLED NEW RIB & PANEL IAW SRM 51-30-2.