What was found
ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 40 INCH CORROSION BS 967 TO 1006 STRINGER 27L. REMOVED CORRODED STRINGER AND INSTALLED STRINGER 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 40 INCH CORROSION BS 967 TO 1006 STRINGER 27L. REMOVED CORRODED STRINGER AND INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3 FIG 1. (M)