As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT AFT CREW DOOR FRAME FR73A TO FR75A, STRINGER 11 LONGITUDINAL BEAM NDT FOUND CRACK INDICATION FROM 5 FASTENER HOLES. REMOVE THE COVER PLATE AND DOOR FRAME BEAM IAW SRM51-40-21. DRILL FASTENER HOLES ON THE NEW PART IAW SRM51-40-40. INSTALL THE NEW PART AND RELATED PARTS IAW SRM51-40-21.