What was found
INSPECTION FOUND A 4 CRACK IN FLANGE OF LT NR 1 SLAT OUTBOARD END RIB. THE WEB AND RIB WERE REMOVED IAW SRM 51-31-10. A NEW RIB WAS INSTALLED IAW 51-31-10 AND 51-21-01. SKIN WAS INSTALLED IAW SRM 51-01-10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 4 CRACK IN FLANGE OF LT NR 1 SLAT OUTBOARD END RIB. THE WEB AND RIB WERE REMOVED IAW SRM 51-31-10. A NEW RIB WAS INSTALLED IAW 51-31-10 AND 51-21-01. SKIN WAS INSTALLED IAW SRM 51-01-10.