As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON APPROACH TO SUA A SPLIT FLAP CONDITION WAS REPORTED. THE AIRCRAFT LANDED WITHOUT INCIDENT. SUBSEQUENT INVESTIGATION REVEALED A SEPARATION OF THE SWAGED END FITTING TO THE FLAP ACTUATOR CAUSING A BIND IN THE LEFT FLAP SYSTEM. P/N 12325Y116 FLAP DRIVE CABLE ASSEMBLY WAS REPLACED WITH NEW AND AN OVERHAULED FLAP ACTUATOR P/N 50-521198-3 WAS REPLACED AS A PRECAUTION.