As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RH ENGINE STRUT BOX ASSEMBLY AFT END EXTERNAL SURFACES ARE CORRODED AT NAC STA 273-282; NAC LBL 3-7; NAC WL 119-130. / REMOVED CORROSION FROM #2 PYLON STRUT ASSY.; AFT END; I/B LOWER FITTING IAW SRM 51-10-02-0G-0. ORIGINAL 'T' .125'; REMAINING 'T' .108'; LOSS OF .017'. DAMAGE OUT OF LIMITS IAW SRM 54-50-71-1A-2. REPAIRED AREA IAW EA 190926 REV. IR AND SWA EA 1-754-2457 REV. IR.