As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INITIAL INSPECTION: CRACK ON FUSELAGE SKIN STA. 1087.060, LONGERON 14R SIDE. PERMANENT REPAIR FUSELAGE SKIN STA. 1087. LONGERON 14R WAS PERFORMED PER ERA 579432-14 REV. ORG. AND ETI 17-19-088 REV. 2 AND PERFORM A GVI WITHIN EVERY CCK (NOT TO EXCEED 24 MONTHS) UNDER LOG PAGE 1152047 . PER ERA 579432-14 REV. ORIGINAL, SECTION I. (LP1154982)