What was found
INSPECTION FOUND A 2 INCH CRACK IN LT WING FLAP RIB AT WS XRS 270 WITH CORROSION AT INBOARD END OF RIB. THE RIB WAS REMOVED IAW SRM 51-30-2. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-10-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN LT WING FLAP RIB AT WS XRS 270 WITH CORROSION AT INBOARD END OF RIB. THE RIB WAS REMOVED IAW SRM 51-30-2. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-10-3.