What was found
CRACK ON STIFFENER OF AFT PRESSURE BULKHEAD AT 12HRS POSITION. STIFFENER WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4 AND 51-10-3 PAR 21 AND 14 AND DWG 9915562, REV "P". DIMENTION CRACK IS 0.750".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON STIFFENER OF AFT PRESSURE BULKHEAD AT 12HRS POSITION. STIFFENER WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4 AND 51-10-3 PAR 21 AND 14 AND DWG 9915562, REV "P". DIMENTION CRACK IS 0.750".