What was found
ROA - DURING CX-6 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 1.5 INCH CRACK AFT ENTRY DOOR CUT OUT FORWARD LOWER CORNER (STRINGER 17L, BS 950) FUSELAGE SKIN. REMOVED CRACK AND INSTALLED REPAIR, REPAIRED PER SRM 53-30-3, FIG 24. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ROA - DURING CX-6 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 1.5 INCH CRACK AFT ENTRY DOOR CUT OUT FORWARD LOWER CORNER (STRINGER 17L, BS 950) FUSELAGE SKIN. REMOVED CRACK AND INSTALLED REPAIR, REPAIRED PER SRM 53-30-3, FIG 24. (M)