What was found
ROA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 12 INCHES, STRINGER 27L AT BSL 967. INSTALLED STRINGER SPLICE PER SRM 53-10-3. 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-2 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 12 INCHES, STRINGER 27L AT BSL 967. INSTALLED STRINGER SPLICE PER SRM 53-10-3. REPAIRED PER SRM 53-10-3, FIG 1. (M)