What was found
CRACK IN AFT PRESSURE BULKHEAD SKIN AT 6 O'CLOCK POSITION BELOW PLUG DOOR JAMB 1.083 LONG. REMOVED EXITING REPAIR, VERIFIED LENGTH OF CRACK AND INSTALLED REPAIR IAW 51-30-2 AND 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN AFT PRESSURE BULKHEAD SKIN AT 6 O'CLOCK POSITION BELOW PLUG DOOR JAMB 1.083 LONG. REMOVED EXITING REPAIR, VERIFIED LENGTH OF CRACK AND INSTALLED REPAIR IAW 51-30-2 AND 51-30-5.