As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON PAN AT BS 170 AND Z 11.063 ON FWD R1 SERVICE DOOR. HFEC INSPECTION WAS ACCOMPLISHED AND A CRACK OF 0.312" WAS FOUND IAW NDTSPM 06-10-01. THE CRACK WAS STOP DRILL IAW SRM 52-00-00 FIG. 202. NO CRACKS FOUND AFTER STOP DRILL, IAW NDTSPM 06-10-01 .001. REPAIR DOUBLER WAS FABRICATED IAW SRM 52-00-00 FIG. 202 AND INSTALLED IAW SRM 52-00-00 FIG. 202 REPAIR. 3.