As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ACCEPTANCE INSPECTION, FOUND THE RIGHT ENGINE PYLON UPPER FUSELAGE ATTACH ANGLE CRACKED. REPLACED THE RT UPPER PYLON TO FUSELAGE ATTACH ANGLE IAW DC-9 SRM CHAPTER 51-30-2 AND 51-30-5 AND REPAIRED ONE CRACK IAW ABX REA D954-16695-MR.