As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 6 INCH CORROSION STRINGER 26R BS 797 FUSELAGE SKIN. REMOVED CORROSION AND INSTALLED DOUBLER. REPAIRED PER SRM 53-30-3 FIG 6. CORROSION TASK NR C53-100-01, CORROSION LEVEL 2. (M)