What was found
90 DEGREE FITTING WAS CRACKED ON THE END OF LONGERON 28 RIGHT, BOTTOM OF FLOOR PANEL SUPPORT BOTTOM SIDE F.S. 756. REPLACED SUPPORT IAW DC-9 SRM 51-30-1 AND 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
90 DEGREE FITTING WAS CRACKED ON THE END OF LONGERON 28 RIGHT, BOTTOM OF FLOOR PANEL SUPPORT BOTTOM SIDE F.S. 756. REPLACED SUPPORT IAW DC-9 SRM 51-30-1 AND 51-30-5.