What was found
NUMBER 8 SLAT TWO {2} SCREWS INSTALLED ON THE LEADING EDGE SKIN AT THE AFT END 32 INCHES FROM THE OUTBOARD END. REMOVED FASTENERS AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NUMBER 8 SLAT TWO {2} SCREWS INSTALLED ON THE LEADING EDGE SKIN AT THE AFT END 32 INCHES FROM THE OUTBOARD END. REMOVED FASTENERS AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.