What was found
INSPECTION FOUND A 1.7 INCH CRACK IN T-ANGLE AT LOWER AFT INTERNAL CORNER OF MID CARGO DOOR. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.7 INCH CRACK IN T-ANGLE AT LOWER AFT INTERNAL CORNER OF MID CARGO DOOR. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5.