What was found
FUSELAGE STRINGER CRACKED AT STA 500, STR 19L. DETECTED DURING ROUTINE C-CHECK INSPECTION. SUSPECT CAUSE BY STRESS LOADS FROM BAGGAGE LOADING. ROUTINE MAINTENANCE INSPECTIONS SHOULD DETECT ANY FURTHER DAMAGE. CONTROL NR 9519RI625.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE STRINGER CRACKED AT STA 500, STR 19L. DETECTED DURING ROUTINE C-CHECK INSPECTION. SUSPECT CAUSE BY STRESS LOADS FROM BAGGAGE LOADING. ROUTINE MAINTENANCE INSPECTIONS SHOULD DETECT ANY FURTHER DAMAGE. CONTROL NR 9519RI625.