What was found
ROA - DURING CX-6 CHECK VISUAL INSPECTION, FUOND 1.75 INCH CRACK BS 792 STRINGER 18L FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ROA - DURING CX-6 CHECK VISUAL INSPECTION, FUOND 1.75 INCH CRACK BS 792 STRINGER 18L FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1. (M)