What was found
R/H UPPER MAIN CORE COWL UPPER FWD I/B CORNER IS BENT AND DEBONDING.FOUND CRACK IN DEBONDING FWD I/B CORNER LENGTH IS 1.437" & .010"W. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED CUTOUT ON DAMAGE ON OUTER SKIN P/N 228-50142-607 THAT MEASURES 2.5"L X .775"W REF ASAP EA# AWAC CRJ272-01774 REV A DTD 12/29/2021. HFEC ACCOMPLISHED WITH NO INDICATIONS NOTED REF CRJ 200 NDTM PART 1 51-20-06 REV 43. INSTALLED SPIGOT PLATE AND DOUBLER REPAIR WITH REPAIR IDENTIFIED AS NUMBER SRS118 FER ASAP EA# AWAC-CRJ272-01774 REV A DTD 12/29/ 2021.