What was found
RIGHT FUSELAGE UPPER AFT CORNER OF NR 3 A/C COMPARTMENT. DOOR CUT OUT HAS A .200 INCH CRACK EXTENDING OUT OF FASTENERS HOLE, END OF CRACKED CRACK, REPAIR COMPLIED WITH IAW SRM 53-50-00 FIG 3 A SHEET 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT FUSELAGE UPPER AFT CORNER OF NR 3 A/C COMPARTMENT. DOOR CUT OUT HAS A .200 INCH CRACK EXTENDING OUT OF FASTENERS HOLE, END OF CRACKED CRACK, REPAIR COMPLIED WITH IAW SRM 53-50-00 FIG 3 A SHEET 3.