As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
A CRACK WAS FOUND ON RIGHT BODY GEAR INBOARD AFT DOOR- AFT EDGE CLOSEOUT BEAM WEB. THE SRM 52-80-02 FIGURE 101 DETAIL IV - ALLOWABLE DAMAGE 3 DOESN'T ALLOW FOR A CRACK ON INBOARD AFT DOOR- AFT EDGE CLOSEOUT RIB WEB EO 4452A173 FAA 8110-3 DATED 07JAN13 ALLOWS FOR A TIME LIMITED REPAIR IAW SRM 52-80-02-1A-3 FIGURE 101 DETAIL XI.&NBSP.