As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION WAS REMOVED AT STR 28R BETWEEN BS 500 AND BS 520, RESULTING IN A 5.5 BY 2.25 CUT OUT. THERE IS AN EXISTING STRINGER SPLICE AT BS 490 AND A NEW SPLICE BEING INSTALLED AT BS 510 PER B727 SRM. THE SKIN IS MANUFACTURED FROM MACHINED CLAD 2024-T3 WITH A LOCAL THICKNESS OF .090. AN EXTERNAL REPAIR DOUBLER WAS INSTALLED PER DL ERA 303440-14.