What was found
CRACK ON LOWER ANGLE OF AFT PRESSURE BULKHEAD STIFFENER X-54 AND Z 62. THE ANGLE WAS REPLACED IAW SRM 51-30-1, 51-30-5, 51-10-4, 51-10-3 PAR 21 - 14, AND DWG 9915558, REV BA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON LOWER ANGLE OF AFT PRESSURE BULKHEAD STIFFENER X-54 AND Z 62. THE ANGLE WAS REPLACED IAW SRM 51-30-1, 51-30-5, 51-10-4, 51-10-3 PAR 21 - 14, AND DWG 9915558, REV BA.