What was found
INSPECTION FOUND A .5 INCH CRACK IN STRINGER 16L BETWEEN STA 500C AND 500D. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 53-30-03.
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 16L BETWEEN STA 500C AND 500D. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 53-30-03.