What was found
INSPECTION FOUND A 1.25 INCH CRACK IN STRINGER 15R AND A 2 INCH CRACK IN STRINGER 15L AT STA 720B. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-10-00, 53-10-3, AND 51-10-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.25 INCH CRACK IN STRINGER 15R AND A 2 INCH CRACK IN STRINGER 15L AT STA 720B. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-10-00, 53-10-3, AND 51-10-2.