As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 1 INCH CRACK IN STIFFENER ON I/B SIDE OF FIXED L/E RIB O/B OF RT WING FORWARD BOTTLE PIN (AFT OF ANTI-ICE DUCT, ACCESS CUTOUT 6402). THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, PAGE 2. A FORMER ANGLE WAS INSTALLED IAW SRM 51-40-3, FIGURE 1 AND 51-10-2, PAGE 2.