What was found
INSPECTION FOUND A 2 INCH CRACK IN NR 1 ENGINE NOSE COWL VERTICAL STIFFENER L-ANGLE. THE CRACKED ANGLE WAS REMOVED, A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 54-11-01 AND 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN NR 1 ENGINE NOSE COWL VERTICAL STIFFENER L-ANGLE. THE CRACKED ANGLE WAS REMOVED, A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 54-11-01 AND 51-31-01.