What was found
AFT PRESSURE BULKHEAD, 1 INCH CRACK AT TOP OF STIFFENER LOCATED ABOVE CENTER OF VAULT DOOR OPENING ON FORWARD SIDE OF AFT PRESSURE BULKHEAD. INSTALLED NEW STIFFENER PER SRM 51-01-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT PRESSURE BULKHEAD, 1 INCH CRACK AT TOP OF STIFFENER LOCATED ABOVE CENTER OF VAULT DOOR OPENING ON FORWARD SIDE OF AFT PRESSURE BULKHEAD. INSTALLED NEW STIFFENER PER SRM 51-01-00.