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, CRACKS WERE DETECTED ON THE FORWARD BULKHEAD LOWER STIFFENER AT FUSELAGE STATION -156. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTUAL REPAIRE MANUAL AND ENGINEERING ORDER 53-DC8-1771.