As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/H NOTCH FLAP FRAME CRACKED REMOVED NOTCH FLAP UP TO AND INCLUDING AMM 27-87-13 PAGEBLOCK 0401 STEP B.(10). ROUTED TO SHEET METAL FOR DRILLING OF NEW NOTCH FLAP. QC MATCH DRILLED NEW PART IAW A300 SRM 51-00-00. FAILED NOTCH FLAP HANGER INSPECTION DURING RII FOR OK TO INSTALL NOTCH FLAP. OPEN