What was found
FUSELAGE SKIN DENT AT STR 28, BS 450. REMOVED INTERNAL FRAME STRUCTURE AND DAMAGED PORTION OF STR 28L PER B747 SRM 53-10-03, FIG 3; 53-10-20, FIG 11;51-10-02, PGS 7-8;51-10-01, PG 9; 51-30-02, PGS 2, 3, 8, 9.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN DENT AT STR 28, BS 450. REMOVED INTERNAL FRAME STRUCTURE AND DAMAGED PORTION OF STR 28L PER B747 SRM 53-10-03, FIG 3; 53-10-20, FIG 11;51-10-02, PGS 7-8;51-10-01, PG 9; 51-30-02, PGS 2, 3, 8, 9.