What was found
NUMBER 2 PYLON AFT SIDE OF STRUT, LT & RT STIFFENERS CRACKED. OLD STIFFENERS REMOVED. NEW STIFFENERS FABRICATED IAW DWG 313T3380 & INSTALLED IAW SRM 51-40-02. PROTECTIVE COATING APPLIED IAW SRM 51-20-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NUMBER 2 PYLON AFT SIDE OF STRUT, LT & RT STIFFENERS CRACKED. OLD STIFFENERS REMOVED. NEW STIFFENERS FABRICATED IAW DWG 313T3380 & INSTALLED IAW SRM 51-40-02. PROTECTIVE COATING APPLIED IAW SRM 51-20-01.