What was found
INSPECTION FOUND A .125 INCH CRACK IN FRAME UPPER FLANGE IN FORWARD CARGO PIT AT FS 500A, STRINGER 23L. THE CRACKED AREA WAS REMOVED IAW SRM 53-10-4. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-4 AND 53-10-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .125 INCH CRACK IN FRAME UPPER FLANGE IN FORWARD CARGO PIT AT FS 500A, STRINGER 23L. THE CRACKED AREA WAS REMOVED IAW SRM 53-10-4. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-4 AND 53-10-2.