As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING IB FLAP OB ATTACH FITTING WITH CRACKED AFT IB RUB PLATE.<[01] REMOVED AND REPLACED TRANSMISSION #3 INBOARD FLAP AFT RUB PLATE REF SRM 51-40-02-0G-0 AND AMM 27-51-13-400-803. TORQUE 175289; DUE DATE 31/07/24.<BR>OPERATED TRAILING EDGE FLAP SYSTEM WITH PRIMARY CONTROL REF AMM 27-51-00-860-801.<BR>OPC IS OK;[02] VERIFIED STEP 1