As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION WAS FOUND ON DOUBLER AT E/E COMPARTMENT ON INTERNAL FUSELAGE SKIN PANEL STA Y=215 TO STA Y=221 BTW LONGERON 28R AND 29R. SUMMARY OF NRC 00626: CORROSION LEVEL 2. DOUBLER ON INTERNAL FUSELAGE SKIN PANEL STA Y=215 TO STA Y=221 BTW LONGERON 28R AND 29R WAS FABRICATED PER DWG 9923686 REV D AND REPLACED PER B717-200 SRM 51-41-02-0G. (LP #0653581)