As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON REMOVAL OF RT T/E SKIN PANEL, FOUND CAP ANGLE CRACKED. REMOVED DAMAGED RT T/E SKIN PANEL CAP ANGLE IAW SRM 51-42-21. LOCATED AND DRILLED UP NEW SERVICEABLE CAP ANGLE IAW SRM 51-40-11 AND INSTALLED SAME IAW SRM 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (SDR CLOSED)