What was found
INSPECTION FOUND A 1.5 INCH CRACK IN STRINGER SPLICE AT STA 360, STRINGER 21R. THE SPLICE WAS REMOVED AND A NEW SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 53-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK IN STRINGER SPLICE AT STA 360, STRINGER 21R. THE SPLICE WAS REMOVED AND A NEW SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 53-30-2.