As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND 2 EACH CRACKS IN FUSELAGE SKIN APPROX AT STA 1760 LT SIDE MID POINT VERTICALLY. ONE CRACK APPROX 2 INCHES LONG BETWEEN L13L AND L14L AND ONE CRACK APPROX 1 INCH LONG BETWEEN L14L AND L15L. CRACKS WILL BE REPAIRED IAW DWG 53-09405-1.