What was found
INSPECTION FOUND A 3 INCH CRACK IN I/B RIB OF RIGHT FLAP WEDGE ASSEMBLY NR 6. THE CRACK WAS DRILLED OUT AND A NEW RIB WAS INSTALLED IAW SRM 51-10-3, 51-30-2, AND 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 3 INCH CRACK IN I/B RIB OF RIGHT FLAP WEDGE ASSEMBLY NR 6. THE CRACK WAS DRILLED OUT AND A NEW RIB WAS INSTALLED IAW SRM 51-10-3, 51-30-2, AND 51-30-5.