As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND FWD BULKHEAD SKIN TO BE GOUGED IN FWD AVIONICS BAY. REMOVED DAMAGE AT FWD BULKHEAD SKIN IN FWD AVIONICS BAY. PERFORMED ULTRASONIC THICKNESS INSPECTION ON THE DAMAGED AREA ON THE FWD PRESSURE BULKHEAD. NOMINAL THICKNESS 0.034" LOWEST PART OF THE DAMAGED 0.024". MADE LAYOUT AND DRILLED HOLES. MADE FILLER FOR FWD BULKHEAD REPAIR WITH 2024-T3 0.032". INSTALLED 94 OUT OF 102 RIVETS.