What was found
INSPECTION FOUND A 1 INCH CRACK IN LT WING LEADING EDGE INTERNAL RIB AT SLAT STA ZERO. THE CRACK WAS STOP DRILLED. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN LT WING LEADING EDGE INTERNAL RIB AT SLAT STA ZERO. THE CRACK WAS STOP DRILLED. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.