What was found
DURING CARGO LOADING AT ANC 1.25 INCH BY 2 INCH HOLE PUNCTURED IN BS 506.5 FUSELAGE SKIN BETWEEN STR 20L AND 21L. REPAIRED PER SRM 53-30-3, FIG 1 M-54 NR 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CARGO LOADING AT ANC 1.25 INCH BY 2 INCH HOLE PUNCTURED IN BS 506.5 FUSELAGE SKIN BETWEEN STR 20L AND 21L. REPAIRED PER SRM 53-30-3, FIG 1 M-54 NR 1.