As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
***CORROSION*** ON FUSELAGE SKIN; UNDER VERTICAL FIN; AT B.S. 1016-1036; L.B.L. 12 - R.B.L. 12; W.L. 306.5. / REMOVED & TREATED CORRODED SKIN; UNDER VERTICAL FIN; AT BS - 1016-1036; RBL12-LBL12; W.L. 306.5 PER EA 21-153-00944 REV. IR AND ER 21-01595 REV. IR.