What was found
INSPECTION FOUND A 4 AND 2 INCH CRACK ON CENTER FRAME ON LT SIDE OF NR 2 ENGINE INLET INSIDE PANEL NR 363EL. THE CRACKS WERE STOP DRILLED IAW SRM 51-90-00. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 54-00-01 AND 51-21-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 4 AND 2 INCH CRACK ON CENTER FRAME ON LT SIDE OF NR 2 ENGINE INLET INSIDE PANEL NR 363EL. THE CRACKS WERE STOP DRILLED IAW SRM 51-90-00. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 54-00-01 AND 51-21-01.