What was found
INSPECTION FOUND A 1.5 INCH CRACK IN ANGLE AT STA 1183 BETWEEN STRINGER 18R AND 19R, RBL 45. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.
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 ANGLE AT STA 1183 BETWEEN STRINGER 18R AND 19R, RBL 45. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.