What was found
DURING INSPECTION, THE RIGHT AFT FUSELAGE SKIN WAS FOUND TO BE DAMAGED AT FRAME 80 AND STRINGER 9L. THE RIGHT AFT FUSELAGE SKIN AT FRAME 80 AND STRINGER 9L WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-009769.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, THE RIGHT AFT FUSELAGE SKIN WAS FOUND TO BE DAMAGED AT FRAME 80 AND STRINGER 9L. THE RIGHT AFT FUSELAGE SKIN AT FRAME 80 AND STRINGER 9L WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-009769.