What was found
BS 1022, STRINGER 14R, SKIN HAS A TWO INCH HORIZONTAL CRACK HFEC VERIFIED IAW NDT SPM 06-10-01.001 PROCEDURE 1. INSTALLED REPAIR IAW PRI 543585-14, REVISION 2, AND ER/A 543585-14 REV.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
BS 1022, STRINGER 14R, SKIN HAS A TWO INCH HORIZONTAL CRACK HFEC VERIFIED IAW NDT SPM 06-10-01.001 PROCEDURE 1. INSTALLED REPAIR IAW PRI 543585-14, REVISION 2, AND ER/A 543585-14 REV.