What was found
FUSELAGE EXTERNAL SKIN AT , LT, AT FR 61, STR 19L HAS CORROSION. REMOVED CORROSION BY BLENDING ON FUSELAGE EXTERNAL SKIN AT, LT, AT FR 61, STR 19L. FOUND TO BE WITHIN LIMITS. IAW EMB 145 SRM 53-21-01-AD PG. 121
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE EXTERNAL SKIN AT , LT, AT FR 61, STR 19L HAS CORROSION. REMOVED CORROSION BY BLENDING ON FUSELAGE EXTERNAL SKIN AT, LT, AT FR 61, STR 19L. FOUND TO BE WITHIN LIMITS. IAW EMB 145 SRM 53-21-01-AD PG. 121