What was found
INSPECTION FOUND 2.5 INCH CRACK AT CURVED ANGLE AT OUTBOARD SIDE OF LT WING FIXED LEADING EDGE RIB SLAT STA 0. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 51-40-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND 2.5 INCH CRACK AT CURVED ANGLE AT OUTBOARD SIDE OF LT WING FIXED LEADING EDGE RIB SLAT STA 0. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 51-40-3.