As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE C-CHECK, A CRACK WAS FOUND ALONG THE AFT PRESSURE BULKHEAD WEB APPROXIMATELY 1.2 INCHES LONG JUST ABOVE WL 263 AND LBL 26.83, BS 1183. THE CRACK WAS STOP DRILLED USING A 0.187 INCH HOLE. THE CRACK WAS THEN NDT TO ENSURE CRACK LIMITATION. REPAIR DOUBLER INSTALLED USING FLIGHT VEHICLES, INC., DRAWING 53-98301-1 REV NEW DATED 6-9-98 BY AAR IN OKLAHOMA CITY. (X)