As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 294 AND STRINGER 7 LEFT. REMOVED CRACK SECTION OF STRINGER WEB, FABRICATED NEW SECTION AND INSTALLED PER SRM. REPAIRED PER BOEING DRAWING 65-17684 AND SRM 53-10-1 AND 51-30-2 PAGE 5. (M)