As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
*SUPPLEMENTAL SDR* 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. COMPLETED REMAINING STEPS OF LEFT NOTCH FLAP REF AMM. 27-87-13-401 AND REINSTALLED NOTCH FLAP ACT. REF AMM. 27-88-15 OPS AND LEAK CKS. GOOD. WITNESSED OPS CHECKS AND VERIFIED CONTROL TRAVEL PER GMM REQUIREMENTS 04-02.