As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE-C, AFT CARGO DOOR CUTOUT FWD DR HINGE 2EA HOLES CRACK AT FUSELAGE SKIN CRACK LENGTH : .0625 INCH AND 0.040 INCH. AFT CARGO DOOR CUTOUT FWD DOOR HINGE AREA. DOUBLERS REMOVED AND INSTALLED IAW SRM 51-30-02 FROM CRACKED SHIM REPLACED ONLY IAW SRM 51-10-01 PG9 AFT HFEC INSPECTION IAW NTM PART 6 51-00-00 FIG 16 AND 4. NO CRACK FOUND ON SKIN.