What was found
INSPECTION FOUND A 1.5 INCH CRACK IN WEB AT STA 358, STRINGER 17L. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW 51-40-3, 51-10-2 AND 53-10-2.
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 WEB AT STA 358, STRINGER 17L. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW 51-40-3, 51-10-2 AND 53-10-2.