As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON SETTLEMENT AREA OF RUB STRIP FUSELAGE SKIN BTW STA Y=870 RH TO 896.5 RH AND LONGERON 27RH FUSELAGE. SUMMARY OF NRC 00737: CORROSION LEVEL 2. FUSELAGE SKIN BTW STA Y=870RH TO 896.5RH AND LONGERON 27RH WAS REPAIRED PER B717 SRM 53-20-70-2R PROCEDURE 1. PERFORM AN EXTERNAL VISUAL INSPECTION INITIAL AT 8,000 CYCLES AND REPETITIVE EVERY 8,000 CYCLES PER B717 SRM 53-20-70-2R REPAIR 1 PAR 7. (LP #0320030)