What was found
ROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 1.25 INCH CRACK AFT ENTRY DOOR CUT OUT FORWARD LOWER CORNER FUSELAGE SKIN STRINGER 17L, BL 950. REMOVED CRACK AND INSTALLED DOUBLER, 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-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 1.25 INCH CRACK AFT ENTRY DOOR CUT OUT FORWARD LOWER CORNER FUSELAGE SKIN STRINGER 17L, BL 950. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 24. (M)