What was found
DETECTED 2 INCH CRACK AT FWD ENTRY DOOR LOWER AFT CORNER. VERIFIED CRACK HFEC INSP IAW 737 NTM PT 6 737 SRM 51-00-00 FIG 23, STOP DRILLED CRACK IAW 737 SRM 51-10-1. INSTALLED PERMANENT REPAIR IAW EO 53-44-01 AND DWG 65C27257.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DETECTED 2 INCH CRACK AT FWD ENTRY DOOR LOWER AFT CORNER. VERIFIED CRACK HFEC INSP IAW 737 NTM PT 6 737 SRM 51-00-00 FIG 23, STOP DRILLED CRACK IAW 737 SRM 51-10-1. INSTALLED PERMANENT REPAIR IAW EO 53-44-01 AND DWG 65C27257.