As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
KRUEGER FLAP 16 HAS CRACK APPROX 6 IN AT UPPER OTBD CORNER. REMOVED KRUEGER FLAP PER MM. ACCOMPLISHED PRE-INSTALLATION INSPECTION OF NR 16 KRUEGER FLAP ATTACH POINTS ON ACFT. INSTALLED FLAP AND TORQUED BOLTS UP TO STEP 3.E.(9) PG 406 MM. COMPLETED INSTALLATION OF NR 16 L/E FLAP FROM ITEM 3(E)9.