What was found
INSPECTION FOUND A .5 INCH CRACK IN STRINGER SPLICE BETWEEN STA 1521 AND 1541, STRINGER 1L. THE SPLICE WAS REMOVED AND REPLACED IAW SRM 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN STRINGER SPLICE BETWEEN STA 1521 AND 1541, STRINGER 1L. THE SPLICE WAS REMOVED AND REPLACED IAW SRM 51-31-01.