What was found
LEFT WING LEADING EDGE INTERNAL UPPER SURFACE DOUBLER HAS FOUR CRACKS AT THE EDGE OF THE STIFFENING INDENTATIONS, LOCATED APPROXIMATELY 5-14 INCHES INBOARD OF THE NUMBER TWO SLAT OUTBOARD TRACK. STOPPED DRILLED FOUR CRACKS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING LEADING EDGE INTERNAL UPPER SURFACE DOUBLER HAS FOUR CRACKS AT THE EDGE OF THE STIFFENING INDENTATIONS, LOCATED APPROXIMATELY 5-14 INCHES INBOARD OF THE NUMBER TWO SLAT OUTBOARD TRACK. STOPPED DRILLED FOUR CRACKS.