What was found
DURING CX-1 CHECK VISUAL AND EDDY CURRENT INSPECTION FOUND A .25 INCH CRACK IN AFT CARGO DOOR SKIN AT THE AFT UPPER CORNER FOR HANDLE. INSTALLED DOUBLER PR SRM 52-00-01 FIG 202. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CX-1 CHECK VISUAL AND EDDY CURRENT INSPECTION FOUND A .25 INCH CRACK IN AFT CARGO DOOR SKIN AT THE AFT UPPER CORNER FOR HANDLE. INSTALLED DOUBLER PR SRM 52-00-01 FIG 202. (M)