What was found
INSPECTION FOUND FUSELAGE STRINGER 24L CORRODED FROM FS 970 TO 1000. THE CORRODED SECTION OF STRINGER WAS REMOVED IAW SRM 51-10-6. STRINGER REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-2 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE STRINGER 24L CORRODED FROM FS 970 TO 1000. THE CORRODED SECTION OF STRINGER WAS REMOVED IAW SRM 51-10-6. STRINGER REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-2 AND 51-30-2.