As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT OUTBOARD FLAP LOWER PART INBOARD TEE ANGLE CRACKED 1.500 AT XFS.164.000. REMOVED CRACKED TEE ANGLE IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 581-1-8B. INSTALLED NEW TEE ANGLE ON LT OUTBOARD FLAP LOWER PART, AT XFS.164.000 IAW SRM 51-3-0 PG 1.