What was found
CLT - MAJOR REPAIR - Q6 CHECK - A .1875" CRACK ON FUSELAGE DOOR FRAME AT BS 294.5, STR 17R. INSTALLED DOUBLER REPAIR IAW SRM 51-70-11 FIG 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - MAJOR REPAIR - Q6 CHECK - A .1875" CRACK ON FUSELAGE DOOR FRAME AT BS 294.5, STR 17R. INSTALLED DOUBLER REPAIR IAW SRM 51-70-11 FIG 1.