As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
#1 ENGINE NOSE COWL HAS CORROSION AT 12 O'CLOCK POSITION APPROX. 10INCHES FROM LE (MARKED) / [01] REMOVED .011? MATERIAL FROM ORIGINAL THICKNESS OF .071? FOUND TO BE OUT OF LIMITS IAW SRM 54-10-01?1A.;[02] C/W INSPECTION.;[03] REMOVED AND REPLACED NOSE COWL PER AMM 71-11-01.;[04] C/W INSPECTION.;[05] REMOVED AND REPLACED #1 ENGINE INLET COWL PER AMM 71-11-01.;[06] C/W INSPECTION.