As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MFEC INSPECTION OF THE AFT PRESSURE DOME WEB AT THE STIFFENER 16R LAP JOINT REVEALED 2 CRACKS IN THE AFT WEB PIECE. BHEC INSPECTION REVEALED 3 MORE CRACKED HOLES. THE DAMAGED SECTION OF WEB WAS REMOVED WITH A CUT OUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 096897-14.