What was found
INSPECTION FOUND A 1.5 INCH CRACK WITH CORROSION ON LT WING STA XRS 280 FLAP RIB ON LEADING EDGE PANEL FLANGE. THE RIB WAS REMOVED FROM SUPPORT CAP, A NEW RIB 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 1.5 INCH CRACK WITH CORROSION ON LT WING STA XRS 280 FLAP RIB ON LEADING EDGE PANEL FLANGE. THE RIB WAS REMOVED FROM SUPPORT CAP, A NEW RIB WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-10-3.