What was found
INSPECTION FOUND FILLET PANEL SUPPORT ANGLE CRACKED AT STA 945, LONGERON 30. THE SUPPORT ANGLE WAS REMOVED AND A NEW SUPPORT ANGLE WAS INSTALLED IAW SRM 51-10-04, 51-10-3, AND 51-30-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FILLET PANEL SUPPORT ANGLE CRACKED AT STA 945, LONGERON 30. THE SUPPORT ANGLE WAS REMOVED AND A NEW SUPPORT ANGLE WAS INSTALLED IAW SRM 51-10-04, 51-10-3, AND 51-30-1.