What was found
FUSELAGE UPPER LOBE INTERIOR SKIN IS CRACKED ON BOTH SIDES OF STRINGER AT SKATE ANGLE FASTENERS AT BS 1097, STR 1, LBL 1 - RBL 1. REMOVED DAMAGE AND INSTALLED DOUBLER IN REFERENCE TO SRM 53-30-3, PG 12.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE UPPER LOBE INTERIOR SKIN IS CRACKED ON BOTH SIDES OF STRINGER AT SKATE ANGLE FASTENERS AT BS 1097, STR 1, LBL 1 - RBL 1. REMOVED DAMAGE AND INSTALLED DOUBLER IN REFERENCE TO SRM 53-30-3, PG 12.