As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER FUSELAGE EXTERNAL SKIN HAS WEAR IN AREA OF DORSAL FIN CONTACT APPROX STA 860 TO 908 LT SIDE AND 860 TO 880 RT SIDE. MAJOR REPAIR. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND INTERNAL STRAP DOUBLER REPAIR PER SRM 53-60-01 REPAIR 9.