What was found
2.5 INCH CRACK DISCOVERED AT BS 574 ABOVE STRINGER 18R. REPAIR COMPLIED WITH IAW SRM 53-30-3 DETAIL XI AND XIX FIGURE 48.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
2.5 INCH CRACK DISCOVERED AT BS 574 ABOVE STRINGER 18R. REPAIR COMPLIED WITH IAW SRM 53-30-3 DETAIL XI AND XIX FIGURE 48.