As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON FUSELAGE SKIN AT STA Y=1418 BETWEEN LONGERON 2 AND 3LT WITH A LENGTH OF 0.593 INCH. CRACK REMOVED, REPAIR DOUBLERS & FILLERS WERE FABRICATED AND INSTALLED IAW ER/A 514799-14AD REV ORIGINAL. REPAIR WAS IDENTIFIED IAW PS 900-5-1, NR 4.