As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE LEFT HAND UNDERWING LONGERON AND FUSELAGE SKIN FOUND 03 EACH CRACKS WHICH APPROXIMATELY 1.0" AT STATION 1028 SRINGER 37L APPROXIMATELY 0.3" AT STATION 1030 STRINGER 37L AND APPROXIMATELY 1.5" AT STATION 1033 STRINGER 37L AS MARKED.