As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER TAKEOFF FROM SUX, SLATS AND FLAPS WOULD NOT RETRACT. SLAT/FLAP MAINTEN ICAS MESSAGE CAME ON. TRIED TO RECYCLE SEVERAL TIMES BUT THE PROBLEM WOULD NOT CLEAR. REPLACED NR 3 RT FLAP (OUTBD) ACTUATOR. IAW A/C MM CHAPTER 27 AND CMP 275215 COMPLETED FLAP/SLAT CONTROL AND DRIVE SYSTEM - FUNCTIONAL TEST IAW CMP 275101 NO DEFECTS NOTED. FLAP CONTROL SURFACES CHECK WITH CLINOMETER ALL DEG WITHIN LIMITS, 12 DEGREES, 20 DEGREES, 40 DEGREES NO DEFECTS.