As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INITIAL CRACKED STIFFENER AT AFT PRESSURE BULKHEAD 12 O'CLOCK POSITION AT PASSENGER CABIN. STIFFENER WAS REPLACED IAW SRM 51-30-2 AND SPRING AT EMERGENCY EXIT PRESSURE BULKHEAD DOOR ARM WAS REMOVED AND INSTALLED IAW AMM 53-53-02 AND ADJUSTMENT, CHECK OF AFT ENTRANCE EMERGENCY DOOR MECHANISM MUST BE PERFORMED WITH CARD 5350-01077-0101.