As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A .5 INCH CRACK THROUGH RADIUS OF RT WING ROOT FORWARD FILLET PANEL SUPPORT ANGLE. THE CRACK WAS LOCATED AT STA 540, 10 INCHES BELOW LOWER CAP OF FORWARD SPAR ADJACENT TO FORWARD END OF HINGED RAM AIR DUCT ACCESS PANEL. THE ANGLE WAS REPAIRED IAW ECRA 5350-01227.