What was found
DURING A SCHEDULED INSPECTION, WE FOUND STR 6612026-3 CRACKED WHERE IT IS ATTACHED TO THE AFT CANTED FUSELAGE BULKHEAD. THE CRACK IS THE LENGTH OF VERTICAL LEG AND STARTS AT THE END OF THE STR EXCURSION BULB AREA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A SCHEDULED INSPECTION, WE FOUND STR 6612026-3 CRACKED WHERE IT IS ATTACHED TO THE AFT CANTED FUSELAGE BULKHEAD. THE CRACK IS THE LENGTH OF VERTICAL LEG AND STARTS AT THE END OF THE STR EXCURSION BULB AREA.