As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON LT ENGINE EMS STRUT F1, FWD END TOP OTBD SIDE. REMOVED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. MECHANICALLY MEASURED STRUT MAX MATERIAL LOSS .004". FOUND TO BE WITHIN LIMITS IAW RD 8/4-54-1058. COMPLIED WITH TASK CARD RD 8/4-54-1058.