What was found
INSPECTION FOUND A 1 INCH CRACK IN INTERNAL DOUBLER STRAP OF NR 2 ENGINE NOSE COWL THROUGH ACCESS PANEL NR 7403 UPPER RT SIDE. THE NR 2 ENGINE NOSE COWL WAS REMOVED AND REPLACED IAW MM 71-10-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN INTERNAL DOUBLER STRAP OF NR 2 ENGINE NOSE COWL THROUGH ACCESS PANEL NR 7403 UPPER RT SIDE. THE NR 2 ENGINE NOSE COWL WAS REMOVED AND REPLACED IAW MM 71-10-01.