As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE UPPER SKIN CRACKED 2 PLACES,SKIN CRACK 1:ON FRAME 75 AT PREVIOUS REPAIR ON FIRST FASTENER BELOW STR 2L. SKIN CRACK 2: ON STR 2L JUST AFT OF FRAME 75....FIX: COMPLETED REPAIRS ON CRACKS AT LH FR75 AT STR 2L IAW EMB SRM 53-31-01 AND EO1-53-19-0322. NOTE: A/C IN HVY CHECK