As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACKS ON FUSELAGE SKIN (2 EA) ON STA Y1154 BTW L3 LH AND L3 RH (UPPER SECTION) AT FUSELAGE. SUMMARY OF NRC 00072: FUSELAGE SKIN ON STA Y1154 BTW L3 LH AND L3 RH (UPPER SECTION) WAS REPAIRED PER ERA 615858-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. REPETITIVE INSPECTIONS: ACCOMPLISH SECTION II WITHIN 24 MONTHS AFTER SECTION I WAS PERFORMED AND REPETITIVELY EVERY 24 MONTHS THEREAFTER. LP #0251086. (LP #0255820)