As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER FUSELAGE AT FRAME 20+75 MM AND FRAME 20+107 MM AND 67MM ABOVE STRINGER 12L SKIN DENTED. DAMAGE HAS BEEN REPORTED UNDER NON ROUTINE ITEM A1E143, 2-112. REPAIR HAS BEEN ACCOMPLISHED UNDER ETD2016-190-044555, INSTRUCTIONS AND APPROVED.