As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FLAP ASYMMETRY JUST BEFORE FINAL APPROACH. OUT OF RIG FLAP LEVER TRANSMITTER. SUBJECT TRANSMITTER WAS RIGGED PER APPLICABLE MAINTENANCE MANUAL. FLAP SYSTEM WAS OPS CHECKED PER APPLICABLE MAINTENANCE MANUAL AND ALL OPS CHECKS WERE GOOD. A BITE CHECK WAS ACCOMPLISHED ON THE FLAP/SLAT ELECTRONICS UNIT (FSEU) PER APPLICABLE MAINTENANCE MANUAL AND NO FAULTS WERE FOUND.