As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HEAVY MAINTENANCE, SEVERAL CRACKS WERE FOUND AT SUBJECT LOCATION. REFER TO EC A18-517-01. FUSELAGE / CENTER FUSELAGE / CENTER WING BOX / FR 35-36 / LT & RT SIDES / PRESSURE PANEL ATTACHMENT HOLES / CRACK DAMAGE – PERMANENT REPAIR; THIS TIME LIMITED REPAIR HAS BEEN APPROVED VIA REF /3/ RDAS, PENDING DTA WITHIN 6 MONTHS, AND IS CLASSIFIED AS MAJOR (AS A DEVIATION FROM THE REF /5/ EC - WHICH IS A CLASSIFIED AS A MAJOR MODIFICATION).