As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A CRACK ON THE INBOARD SIDE OF L/E CAVITY BULKHEAD LOWER ANGLE APPROXIMATELY TWENTY INCHES AFT OF KRUEGER FLAP HINGE LINE AT LT WING LEADING EDGE STA 130. THE ANGLE WAS REMOVED AND A NEW REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30, 51-10-2, AND MM 51-20-11.