As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN IS CRACKED AROUND SEVERAL FASTENER HOLES IN THE LAP JOINT LOWER ROW AT STR 14R FROM STA 927 TO STA 951. REPAIRED PER DALFORT AEROSPACE, L.P. XEA X2-53-211 REV 1, DATED 3-16-98, AND BOEING SRM 53-30-3, FIG 42. REF: FAA FORM 8110-3 DATED 3-11-98.