What was found
DURING C CHECK, EXTERNAL FUSELAGE SKIN FOUND CORRODED BETWEEN FR 92 - 95 , STRINGER 14 LEFT TO BOTTOME CENTER LINE. REMOVED CORROSION, BLEND AREA AND INSTALLED REPAIR DOUBLE PER SRM 53-51-11-300-002 AND ER/A 14-586361. LP 1547461
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C CHECK, EXTERNAL FUSELAGE SKIN FOUND CORRODED BETWEEN FR 92 - 95 , STRINGER 14 LEFT TO BOTTOME CENTER LINE. REMOVED CORROSION, BLEND AREA AND INSTALLED REPAIR DOUBLE PER SRM 53-51-11-300-002 AND ER/A 14-586361. LP 1547461