What was found
FUSELAGE EXTERNAL SKIN AT FR 61, STRINGER 19L HAD CORROSION. REMOVED CORROSION BY BLENDING ON SKIN AT FR 61, STR 19L. FOUND TO BE WITHIN LIMITS. IAW 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 FR 61, STRINGER 19L HAD CORROSION. REMOVED CORROSION BY BLENDING ON SKIN AT FR 61, STR 19L. FOUND TO BE WITHIN LIMITS. IAW SRM 53-21-01-AD, PG 121.