As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THERE IS A CRACKED VERTICAL ANGLE AT THE RIGHT OVERWING TO BODY FAIRING SUPPORT AT STA 1421. REMOVED ANGLE IAW SRM 51-31-01 VOL II. FABRICATED IAW DWG AUB 7051; REV " C ". HEAT TREATED IAW TPS 1003 REV " A ". LOCATED & DRILLED HOLES IAW SRM 51-31-01 VOL II. ALODINED & PRIMED IAW SRM 51-21-01 PGS 21 & 24 VOL II. INSTALLED NEW ANGLE IAW SRM 51-31-01; VOL II.