What was found
FUSELAGE SKIN WAS CRACKED, BS 468, STRINGER 16R. A REPAIR WAS INSTALLED IAW SRM 53-30-03, FIG 48, DETAIL XI, PROCEDURE VII.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN WAS CRACKED, BS 468, STRINGER 16R. A REPAIR WAS INSTALLED IAW SRM 53-30-03, FIG 48, DETAIL XI, PROCEDURE VII.