What was found
CRACK IN THE FUSELAGE SKIN AT THE LEFT AFT ENTRY DOOR CUTOUT LOWER FORWARD CORNER. REPAIRED DAMAGE PER SRM 53-30-3 FIG. 24.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN THE FUSELAGE SKIN AT THE LEFT AFT ENTRY DOOR CUTOUT LOWER FORWARD CORNER. REPAIRED DAMAGE PER SRM 53-30-3 FIG. 24.