What was found
CORROSION ON #2 ENG LH CORE COWL SKIN BETWEEN NSTA 222 AND NSTA 230.(<P>1. REPAIR THE DAMAGE AREA IAW EI #T2025A54M-198, REV 0 AND REF DWG #314T4210 SH 20 REV D, 314T4210 SH 18 REV C AND 314T4210 SH 1 REV C. 2. JOB COMPLETED.</P>)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON #2 ENG LH CORE COWL SKIN BETWEEN NSTA 222 AND NSTA 230.(<P>1. REPAIR THE DAMAGE AREA IAW EI #T2025A54M-198, REV 0 AND REF DWG #314T4210 SH 20 REV D, 314T4210 SH 18 REV C AND 314T4210 SH 1 REV C. 2. JOB COMPLETED.</P>)