As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING CLIMB NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. OPS CHECKLIST CARRIED OUT. AIRCRAFT WAS RETURNED TO BASE DUE TO SECOND INCIDENT IN 2 DAYS. DURING INSPECTION, NR 1 ANTI ICE VALVE SEALS WERE REPLACED. NR 1 BLEED SHUT OFF VALVE WAS REPLACED IAW MM 36-10-01. HIGH POWER RUNS WERE CARRIED OUT. NO LEAKS FOUND AND NR 1 ENGINE STRUT OVERHEAT LIGHT DID NOT ILLUMINATE AFTER THE 15 MINUTE RUN. NO FURTHER PROBLEM DURING SUBSEQUENT FLIGHT.