As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACKS IN STRINGER S16L WHILE PERFORMING INSPECTION OF STRINGER S16L FOUND TWO CRACKS. ONE ABOVE THE DAMAGE ON THE TOP SIDE OF THE STRINGER AND ONE ON THE OUTB'D FACE OF THE STRINGER ALSO IN THE DAMAGED AREA. BOTH CRACKS ARE APPROX. .75' IN LENGTH.<[01] STOP DRILLED CRACKS IN STRINGER 16L IAW EA 23-153-01117 AND SRM 51-10-02.;[02] C/W 23-153-01117-WIP3