As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEADING EDGE FLAP DISAGREE. PERFORMED FIM PROC. 27-81-00 FIG 104 CYCLED FLAPS/SLATS SEVERAL TIMES LUBED SLATS RESET TRIPPED ROTARY ACTS. BITE OF FSEU - COULD NOT DUPLICATE ON GROUND. PERFORMED AMM 27-81-00/501 FLAP/SLATS OPERATE NORMAL.