As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TYPICAL CRACK FOUND AT R1 DOOR STUB FRAME JUST ABOVE SEAL DEPRESSOR. CRACK LENGTH : 0.781'.<[01] REMOVED AND REPLACED STUB FRAME AT R1 DOOR SURROUND STRUCTURE SRM 51-40-02-0G-0 AND DWG:141A8370;[02] (RII) FINAL INSPECTION; VERIFIED STEP #1.