What was found
CLT - INSPECTION VISUALLY FOUND A CRACK THROUGH RIVET .1875 INCH UP AND .125 INCH DOWN LOCATED AT FUSELAGE SKIN AT STATION 251 AND STRINGER 11L. INSTALLED DOUBLER AS PER BOEING SRM 53-30-03 AND USAIR EO NR 22870. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - INSPECTION VISUALLY FOUND A CRACK THROUGH RIVET .1875 INCH UP AND .125 INCH DOWN LOCATED AT FUSELAGE SKIN AT STATION 251 AND STRINGER 11L. INSTALLED DOUBLER AS PER BOEING SRM 53-30-03 AND USAIR EO NR 22870. (M)