As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
GSO - INSPECTION FOUND A .75 INCH CRACK IN AFT UPPER ATTACH ANGLE AND A 1 INCH CRACK IN FORWARD ATTACH ANGLE OF RT PRESSURE PANEL AT BS 663.75. BOTH ANGLES WERE REMOVED. NEW ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 51-10-2. (X)