As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HFEC INSPECTIN PER D6-7170 PART 6, 51-00-00, INSPECTION FOUND BS 2231 FRAME CRACK INDICATION AT STRINGER 25L. CRACK CONFIRMED. CRACK AREA TRIMMED OUT. FILLERS AND STRAP DOUBLERS FABRICATED. INSTALLED PER SRM 51-30-02 AND STANDARD PRACTICES. REF SB 747-53A2450. (M)