As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION PITTING ON LT ENGINE EMS STRUT F1 AFT INBD SIDE. REMOVED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. PERFORMED UT THICKNESS IAW NTM 51-00-04-910-801 PT 1. MIN REMAINING THICKNESS .062" FOUND TO BE IN LIMITS IAW DWG 85415014, REV D.