As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 ENGINE LIGHT ON DURING CLIMB AT TAKEOFF POWER. POWER REDUCTION LIGHT 'OUT'. REMOVED AND REPLACED NR 1 ENGINE BLEED VALVE AND REROUTED STRUT OVERHEAT LOOP. PERFORMED LEAK CHECK, LEAK CHECKED OK. NO OVERHEAT LIGHT IAW 727 MM 36-10-00. (M)