As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING CLIMB IT WAS OBSERVED THAT THE NR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON. IAW OPS CHECKLIST, SYSTEM CHECK CARRIED OUT AND FLIGHT CONTINUED WITHOUT INCIDENT. AFTER LANDING, INSPECTION WAS CARRIED OUT AND THE HIGH PRESSURE MODULATING AND SHUTOFF VALVE WAS FOUND LEAKING. THE VALVE WAS REPLACED. LEAK CHECK CARRIED OUT AND CHECKED SERVICEABLE IAW MM 26-12-41.