As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON FUSELAGE SKIN BETWEEN STA 886 - STA 888; STRINGER 25L. / [01] VERIFIED APPLICABILITY IAW SRM 53-00-01-1A-5;[15] AS PER EA 22-153-00763; THE DAMAGE IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING ACTION REQUIREMENTS.;[16] INSPECTION COMPLETE