What was found
INSPECTION FOUND A 1 INCH CRACK IN CURVED ANGLE INSIDE LT WING INBOARD FIXED LEADING EDGE AT STA 130. A DOUBLER WAS 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 CURVED ANGLE INSIDE LT WING INBOARD FIXED LEADING EDGE AT STA 130. A DOUBLER WAS INSTALLED IAW SRM 51-40-3.