What was found
AFTER REMOVAL OF BRACKET, CORROSION WAS FOUND ON INTERNAL DOUBLER SKIN. Y= 21192-21617, STR= 27R-28R. BLENDED CORROSION IAW SRM 51-10-03 & 51-12-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER REMOVAL OF BRACKET, CORROSION WAS FOUND ON INTERNAL DOUBLER SKIN. Y= 21192-21617, STR= 27R-28R. BLENDED CORROSION IAW SRM 51-10-03 & 51-12-01.