What was found
INSPECTION FOUND A .5 INCH CRACK IN LT INTERIOR FUSELAGE FRAME AT FS 910 AT STRINGER 15L. THE CRACKED AREA WAS TRIMMED OUT, A REPAIR WAS INSTALLED IAW SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN LT INTERIOR FUSELAGE FRAME AT FS 910 AT STRINGER 15L. THE CRACKED AREA WAS TRIMMED OUT, A REPAIR WAS INSTALLED IAW SRM 51-30-2.