What was found
A 3.625 INCH CRACK FOUND AT RIGHT SECTION 46 SKIN BETWEEN STA 867 & 887 AT LAP JOINT S25R. REMOVED DAMAGE & INSTALLED DOUBLER & TRIPLER REPAIR PER BOEING SRM 53-00-01 FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A 3.625 INCH CRACK FOUND AT RIGHT SECTION 46 SKIN BETWEEN STA 867 & 887 AT LAP JOINT S25R. REMOVED DAMAGE & INSTALLED DOUBLER & TRIPLER REPAIR PER BOEING SRM 53-00-01 FIG 201.