As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 1.875 INCH CRACK IN FORWARD GALLEY DOOR CUTOUT LOWER CORNER FUSELAGE FRAME SKIN, STA 330, L17R. AN INTERIM REPAIR WAS PERFORMED IAW ECRA 5331-01286 AND A DIP WAS ISSUED TO ACCOMPLISH A REPEAT INSPECTION WITH AN INTERVAL NOT TO EXCEED 60,000 FLIGHT CYCLES AND AT SUBSEQUENT INTERVALS NOT TO EXCEED 24,000 FLIGHT CYCLES.