As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND CRACKED SKIN AND CORRODED STRINGER AT STA 1089 AT STR 28L. TRIMMED OUT DAMAGED TOP SKIN AND FABRICATED DOUBLER FROM 2024-T3 .060" AND INSTALLED PER SRM 53-30-3 FIG 3 CAT B. REPAIR MUST BE REINSPECTED AT 45000 CYCLES THRESHOLD STARTS AT DATE OF REPAIR. RII ACCOMPLISHED AND VERIFIED DONE IAW SRM 53-30-3. A/C APPROVED.