As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER FUSELAGE AREA OF DORSAL FIN-GOUGED AT APPROX STA 856 TO 861 LT SIDE ON DORSAL RUB STRIP. INSTALLED REPAIR DOUBLER IAW EC/RA 5331-01686. DIP ISSUED TO ACCOMPLISH A PERMANENT REPAIR PRIOR TO FEBRUARY 25, 2015. PLANNING TO CONTACT ENGINEERING AFTER NOV 25, 2014 BUT BEFORE DEC 25, 2014 FOR PERMANENT REPAIR.