What was found
CRACKED STIFFENER ON AFT PRESSURE BULKHEAD BETWEEN LONGERONS 7RT AND 8 RT AT PASSENGER CABIN. STIFFENER WAS REPLACED IAW SRM 51-41-05 DWG 9915558, REV BA CRACK L= 0.750".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED STIFFENER ON AFT PRESSURE BULKHEAD BETWEEN LONGERONS 7RT AND 8 RT AT PASSENGER CABIN. STIFFENER WAS REPLACED IAW SRM 51-41-05 DWG 9915558, REV BA CRACK L= 0.750".