What was found
CHAFE AREA FWD & AFT OF CRACK, BS 880.60, S1L, LEFT DOSAL FIN SEAT AREA. REMOVED DAMAGED AREA & INSTALLED DOUBLER & TRIPLER, DEFECT SIZE: 2 INCH CRACK AND 12 X 1 INCH CHAFE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CHAFE AREA FWD & AFT OF CRACK, BS 880.60, S1L, LEFT DOSAL FIN SEAT AREA. REMOVED DAMAGED AREA & INSTALLED DOUBLER & TRIPLER, DEFECT SIZE: 2 INCH CRACK AND 12 X 1 INCH CHAFE.