What was found
INSPECTION FOUND A 1 INCH CRACK IN LONGERON 30 FILLET PANEL SUPPORT ANGLE AT STA 970. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN LONGERON 30 FILLET PANEL SUPPORT ANGLE AT STA 970. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-4.