What was found
FORWARD ENTRY DOOR HAS INTERNAL CRACK IN RADIUS, FORWARD JAMB AT LOWER SIDE OF NUMBER 2 STOP BRACKET SUPPORT STRUCTURE. STOP DRILLED CRACK, DYE-CHECK CONFIRMED, INSTALLED DOUBLER UNDER SRM 52-05-00 FIG 31 (SHEET 3).
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FORWARD ENTRY DOOR HAS INTERNAL CRACK IN RADIUS, FORWARD JAMB AT LOWER SIDE OF NUMBER 2 STOP BRACKET SUPPORT STRUCTURE. STOP DRILLED CRACK, DYE-CHECK CONFIRMED, INSTALLED DOUBLER UNDER SRM 52-05-00 FIG 31 (SHEET 3).