As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER BUSHING REMOVAL, LEFT HAND WING INBOARD FLAP VANE INBOARD TEE FITTING BORE FOUND CORRODED. LEFT HAND WING INBOARD FLAP VANE INBOARD TEE FITTING REMOVED AND REPLACED AS PER AMM 27- 50-22-4. FLAP OPERATION TEST CARRIED OUT AS PER AMM 27-50-00-860-801.