As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) ON CLIMB NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. THRUST REDUCED AND LIGHT EXTINGUISHED. RETURNED. MAINTENANCE INSPECTION FOUND RIGHT ANTI-ICE DUCT SEPARATED FROM ANTI-ICE VALVE. DUCT REPLACED GROUND RUN, SYSTEM CHECKED SERVICEABLE.