As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
HIGH PRESSURE DOOR 192DR UPPER STOP PAD WORN INTO CHORD REMOVED LOWER SEAL. REMOVED DAMAGED STOP PAD. MEASURED CHORD DAMAGE. CHORD IS .125 INCH THICK CHORD WEAR IS .25" DIA. X .021" DEEP. CHORD DAMAGE IS OUT OF LIMITS OF SRM 53 30 71 AD1 FIG 105C. REPAIRED WORN CHORD AS PER EA 700 53EA 04417 RE-INSTALLED SEA AS PER SRM 51 40 02.