As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LONGERON 29L IS CORRODED FROM STA 930 TO STA 954. CLEANED UP CORROSION ON L29L FS 930-954 IAW SRM 51-10-04 PAR 35. ORIGINAL THICKNESS .125" REMAINING .121 WITHIN ALLOWABLE LIMITS IAW SRM 53-00-00 FIG 103. FOUND ELONGATE HOLE AT 943 REPAIRED LONGERON AT FS 943 IAW SRM 53-00-05-2R REPAIR 3.