What was found
INSPECTION FOUND A 1 INCH CRACK IN STRINGER 16L AT STA 500C + 5. REPAIR PARTS WERE INSTALLED IAW SRM 53-00-03, FIGURE 201, REPAIR 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN STRINGER 16L AT STA 500C + 5. REPAIR PARTS WERE INSTALLED IAW SRM 53-00-03, FIGURE 201, REPAIR 1.