What was found
INSPECTION FOUND A 1 INCH CRACK IN HORIZONTAL WEB UNDER REV INTERLOCK VALVE/CYLINDER ON TOP OF NR 1 PYLON. THE WEB WAS REMOVED IAW SRM 51-31-01. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-20-01 AND 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN HORIZONTAL WEB UNDER REV INTERLOCK VALVE/CYLINDER ON TOP OF NR 1 PYLON. THE WEB WAS REMOVED IAW SRM 51-31-01. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-20-01 AND 51-31-01.