As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON CIRCUMFERENTIAL AT BS 930 STRINGER 13L. INSTALLED FUSELAGE FRAME REPAIR AT BS 930 BETWEEN STRINGER 11 AND STRINGER 12, AND BETWEEN STRINGER 13 AND STRINGER 14 LEFT. MATERIAL USED, 7075-T6, .125 INCH, 14.5 INCH BY 1.25 INCH. REPAIR INSTALLED IAW SB 727-52-0162. (M)