What was found
ON 2C CHECK, THE LOWER FUSELAGE SKIN WAS FOUND TO BE CORRODED AT FUSELAGE FRAME 21, BETWEEN STRINGERS 20R AND 21R. THE SKIN WAS REPAIRED PER EMB 120 SRM 53-00-01, PG 202.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ON 2C CHECK, THE LOWER FUSELAGE SKIN WAS FOUND TO BE CORRODED AT FUSELAGE FRAME 21, BETWEEN STRINGERS 20R AND 21R. THE SKIN WAS REPAIRED PER EMB 120 SRM 53-00-01, PG 202.