What was found
31J - CORROSION WAS FOUND ON THE T-ANGLE ABOVE THE NOSE WHEELWELL ACCESS PANEL AT FS 227.8, LT SIDE. THE T-ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED USING FILLERS AND DOUBLERS IAW SRM 53-10-8. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
31J - CORROSION WAS FOUND ON THE T-ANGLE ABOVE THE NOSE WHEELWELL ACCESS PANEL AT FS 227.8, LT SIDE. THE T-ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED USING FILLERS AND DOUBLERS IAW SRM 53-10-8. (X)