What was found
ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AFT ENTRY DOOR CUT OUT FORWARD LOWER CORNER FUSELAGE SKIN (STRINGER 17L BS 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-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AFT ENTRY DOOR CUT OUT FORWARD LOWER CORNER FUSELAGE SKIN (STRINGER 17L BS 950). REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 24. (M)