As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EXTERIOR UPPER FUSELAGE BS 1450 SPLICE BETWEEN STR 3L AND 4L HAS A BLENDED OUT AREA. TRIMMED OUT DAMAGED SKIN. HFEC INSPECTED SURROUNDING FASTENER HOLES AND TRIMMED OUT AREA. INSTALLED REPAIR DOUBLERS AND FILLERS. PLANNING TO CONTACT ENGINEERING AFTER 30000 TOTAL CY, BUT BEFORE 32000 CY TO ACCOMPLISH INSPECTION BEFORE 36000 CYCLES.