As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON PAN FWD/AFT INTERNAL UPPER EDGE AT LH FWD PASSENGER DOOR (L1). SUMMARY OF NRC 00095: PAN FWD/AFT INTERNAL UPPER EDGE AT LH FWD PASSENGER DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 3. IN THE PROCESS, DOOR REMOVAL/INSTALL WAS NEEDED AND IT WAS PERFORMED PER B717 AMM B717 AMM 52-11-01. (LP #0092179)