As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 5311-I-16524-NG (AD - INSP - FUSELAGE - INSPECTION OF BS 1016 AFT PRESSURE BULKHEAD CENTER DOME APEX - GROUP 2; INDICATION OF A CRACK (HFEC) AT BL0 RIGHT LOWER FASTENER. AFTER PAINT REMOVAL USING PART 6 51-00-00 PROCEDURE 23 INDICATION OF CRACK STILL PRESENT AND VISUALLY CRACK CAN BE SEEN RADIATING FROM ABOUT 1 O'CLOCK APPROXIMATELY 1/8 INCH. DAMAGE ON AFT PRESSURE BULKHEAD WAS REPAIRED IAW EA 26-153-00239-WIP1 THRU EA 26-153-00239-WIP4 AND FINAL EA 26-153-00239.