As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON LEFT WING UPPER EXTERNAL PLATING ADJACENT TO THE REAR SPAR AT STATION XW120. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGE AREA, FABRICATION AND INSTALLATION A REPAIR FILLER AND AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH FAA DER APPROVED DRAWING E22-R01 AND ENGINEERING ORDER 57-DC8-827.