What was found
INSPECTION TYPE:C1 RIGHT WING L/E UPPER SKIN IS CRACKED AT XFS 610. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATED AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW EO DC8-5720-7767-A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE:C1 RIGHT WING L/E UPPER SKIN IS CRACKED AT XFS 610. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATED AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW EO DC8-5720-7767-A.