What was found
INSPECTION FOUND A .5 INCH CRACK IN ATTACHMENT ANGLE ON STRINGER 16L BETWEEN STA 348.2 AND 351.2. THE ATTACHMENT ANGLE WAS REPLACED IAW ECRA 5311-01375.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN ATTACHMENT ANGLE ON STRINGER 16L BETWEEN STA 348.2 AND 351.2. THE ATTACHMENT ANGLE WAS REPLACED IAW ECRA 5311-01375.