What was found
ROA - DURING CX-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND .0625 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER FUSELAGE SKIN. STOP DRILLED CRACK AND INSTALLED DOUBLER. REPAIRED PER TYPICAL REPAIR 53-10-19 REV A. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ROA - DURING CX-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND .0625 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER FUSELAGE SKIN. STOP DRILLED CRACK AND INSTALLED DOUBLER. REPAIRED PER TYPICAL REPAIR 53-10-19 REV A. (M)