What was found
ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 20 INCH CORROSION AT STRINGER 26 RIGHT BS 996 TO 1016. REMOVED CORROSION AND INSTALLED NEW STRINGER AND SPLICE, REPAIRED PER SRM 53-10-3, FIG 1. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 20 INCH CORROSION AT STRINGER 26 RIGHT BS 996 TO 1016. REMOVED CORROSION AND INSTALLED NEW STRINGER AND SPLICE, REPAIRED PER SRM 53-10-3, FIG 1. (M)