As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON SLAT RETRACTION AFTER TAKEOFF, NR 5 SLAT INDICATED DOWN. CYCLED SLATS AND NR 5 REMAINS AMBER ON BOTH FORWARD AND AFT PANELS. RETURNED TO ORD. *S/D* REPLACED LEADING EDGE FLAP POSITON SWITCH NR 5 PER 27-85-01. OPERATIONALLY CHECKS NORMAL.