As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WORN FUSELAGE SKIN AT STA Y=994 & LONG 23 - 25 (ADJACENT TO AFT DOOR JAMB). SUMMARY OF NRC 00013: FUSELAGE SKIN AT STA Y=994 & LONG 23 - 25 (ADJACENT TO AFT DOOR JAMB) WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 10 REPAIR 10. PERFORM VISUAL INSPECTION AT 8,000 CYCLES AND REPETITIVE VISUAL INSPECTION EVERY 8,000 CYCLES PER B717 SRM 53-20-15-2R PROCEDURE 10 REPAIR 10 FIG 202 STEP 7. (LP #0244014)