As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
A CRACK WAS FOUND IN THE FUSELAGE SKIN PANEL AT BS 1725, STR 7R. A REPAIR WAS ACCOMPLISHED IAW SECTION I OF ERA 522079-14AD. ACCOMPLISH REPETITIVE INSPECTIONS OF THE INSTALLED REPAIR IAW SECTION II OF ERA 522079-14AD PRIOR TO 30,000 TOTAL FLIGHT CYCLES AND REPEAT AT EVERY 6,000 FLIGHT CYCLE INTERVALS THEREAFTER. REFER TO SCEPTRE 1339717 FOR ER/A 522079-14AD SECT I WORK DETAILS.