What was found
DISCOVERED 1.25 INCH SKIN CRACK APPROX 2 INCHES FWD OF BS 540 BETWEEN STRINGER 1 & 2L. REPAIRED IAW SRM 53-30-3 FIG 48 DETAIL XXIII PROCEDURE III & VII.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DISCOVERED 1.25 INCH SKIN CRACK APPROX 2 INCHES FWD OF BS 540 BETWEEN STRINGER 1 & 2L. REPAIRED IAW SRM 53-30-3 FIG 48 DETAIL XXIII PROCEDURE III & VII.