What was found
DURING ROUTING C-CHECK INSPECTION, A ONE INCH CRACK WAS FOUND ON THE AFT PRESSURE BULKHEAD CIRCUMFERENTIAL MOUNT ANGLE AT FUSELAGE STATION 1766, STIFFENER 3 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED ANGLE, FABRICATION AND INSTALLATION OF A NEW MOUNT ANGLE IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY DC-8 SRM 53-2-0, 51-1-8, 51-1-21 AND ENGINEERING ORDER 51-DC8-719.