What was found
BS 280 CIRCUMFERENTIAL JOINT HAS CORROSION BETWEEN STRINGERS 23 AND 26R. REMOVED CORROSION IAW 51-42-06-001-001-A01, 51-21-06-001-001-A01. RECEIVED AND COMPLIED WITH EA 32-2016-081, REV ECTC.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
BS 280 CIRCUMFERENTIAL JOINT HAS CORROSION BETWEEN STRINGERS 23 AND 26R. REMOVED CORROSION IAW 51-42-06-001-001-A01, 51-21-06-001-001-A01. RECEIVED AND COMPLIED WITH EA 32-2016-081, REV ECTC.