What was found
GSO - INSPECTION FOUND THE SKIN BULGED AT LAP JOINT STRINGER 19L STA 940 TO 950. THE DAMAGED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-10-6, 53-30-3 AND 51-30-2. (W)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
GSO - INSPECTION FOUND THE SKIN BULGED AT LAP JOINT STRINGER 19L STA 940 TO 950. THE DAMAGED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-10-6, 53-30-3 AND 51-30-2. (W)