As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK INDICATION FOUND AT TWO HOLES COMMON TO THE VERTICAL STABILIZER FRONT SPAR LIGHT AND RT CHORDS, AT LOWER SKIN PANEL. THE TWO DAMAGED HOLES ARE EXACTLY SITUATED AT THE UPPER MOST LOCATION OF THE SKIN PANEL (6TH HOLE FROM BOTTOM OF THE INSPECTION AREAS ON BOTH SIDES). REPAIRED ON ER/A 478044-14 ORIG: VERTICAL STABILIZER / FRONTSPAR / RT AND LT CHORD / ZFS=52 / FATIGUE CRACKS.