As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TWO SIMILAR DEFORMATIONS ON SKIN PANEL (BOTH RHS AND LHS) BETWEEN C51 AND C52, P39-40. REPAIR PERFORMED BY DRESSING BACK THE DENTS, PERFORMING ROTOTEST AND HFEC AND INSTALLING HL11VF5 FASTENERS IAW EA 6-53-15-103318 AND RAS 046898/014/2006.