What was found
CRACK IN RIGHT WING LEADING EDGE PANEL ASSEMBLY INNER (WAFFLED) SKIN 8 INCHES FROM INBOARD EDGE STA XFS 304. STOP DRILLED CRACK AND INSTALLED REPAIR IAW REA D857-53580, REV IR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN RIGHT WING LEADING EDGE PANEL ASSEMBLY INNER (WAFFLED) SKIN 8 INCHES FROM INBOARD EDGE STA XFS 304. STOP DRILLED CRACK AND INSTALLED REPAIR IAW REA D857-53580, REV IR.