As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE EGT OVER LIMIT DURING CLIMB, THRUST EGT EXCEEDED LIMITS. EGT WENT CLOSE TO 670 CELSIUS DEGREES FOR 10 SECONDS THEN REDUCED TO LOWER EGT. R & R HPC 10 STAGE SOLENOID VALVE IAW AMM 75-32-53. PERFORMED FUNCTIONAL TEST IAW AMM 75-32-53-700-010A AND FOUND NORMAL. THE ACFT RETURNED TO NORMAL OPERATION.