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, CORROSION WAS DETECTED ON LONGERON 36 END FITTING BETWEEN FUSELAGE STATION 8 AND 10. REPAIR ACCOMPLISHED REMOVAL OF END FITTING, FABRICATION AND INSTALLATION NEW END FITTING IN ACCORDANCE WITH DOUGLAS DRAWING 9755865 AND ENGINEERING ORDER 53-DC8-1792.