What was found
INSPECTION FOUND ANGLE CRACKED THROUGH LOWER ACCESS PANEL NR 7406 OF NR 2 ENGINE NOSE COWL. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-5, AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND ANGLE CRACKED THROUGH LOWER ACCESS PANEL NR 7406 OF NR 2 ENGINE NOSE COWL. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-5, AND 51-30-2.