As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/E FLAP DISAGREE EICAS ON FLAP EXTENSION. AFTER COMPLETION OF TEST FLIGHT, INSPECTED ALL LEADING EDGE SLAT DRIVE ROTARY ACTUATOR OVERLOAD INDICATORS FOR A TRIPPED CONDITION. ACCOMPLISHED CHECK FOR OVERLOAD. NO TRIPPED ROTARY ACTUATORS FOUND. CREW STATED SYSTEM WORKED NORMAL.