What was found
INSPECTION FOUND A .25 INCH CRACK IN STRINGER 1L BETWEEN STA 1088 AND 1117. THE STRINGER SPLICE WAS REMOVED AND REPLACED IAW SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK IN STRINGER 1L BETWEEN STA 1088 AND 1117. THE STRINGER SPLICE WAS REMOVED AND REPLACED IAW SRM 51-30-2.