What was found
INSPECTION FOUND A 2 INCH CRACK IN LT WING RIB AT LEADING EDGE STA XORS 655. A REPAIR CLIP WAS FABRICATED AND INSTALLED IAW SRM 57-20-00, 51-20-00, 51-21-01, AND 51-33-01.
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 RIB AT LEADING EDGE STA XORS 655. A REPAIR CLIP WAS FABRICATED AND INSTALLED IAW SRM 57-20-00, 51-20-00, 51-21-01, AND 51-33-01.