What was found
ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 68 INCH CORROSION AT STRINGER 27 LEFT BS 948 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 68 INCH CORROSION AT STRINGER 27 LEFT BS 948 TO 1016. REMOVED CORROSION AND INSTALLED NEW STRINGER AND SPLICE, REPAIRED PER SRM 53-10-3, FIG 1. (M)