As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT FUSELAGE EXTERNAL LONGERON END FITTING AT STA 1521.000 LONGERON 29 FOUND WITH CRACK. HFEC INSPECTION CARRIED OUT PER DAC NDT SPM REVISION 13.06-06-10-01.001, CRACK IS APPROXIMATELY 1 INCH LONG. CRACKED SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. NEW SPLICE REWORKED AS PER DRAWING AEA7643. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.