What was found
DURING TURNAROUND CHECK, FOUND FUSELAGE FRAME TORN AT BS 560 RT BETWEEN STRINGERS 15 AND 16 BY UNKNOWN SOURCE. REPAIRED IAW SRM 51-40-03 FIG 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING TURNAROUND CHECK, FOUND FUSELAGE FRAME TORN AT BS 560 RT BETWEEN STRINGERS 15 AND 16 BY UNKNOWN SOURCE. REPAIRED IAW SRM 51-40-03 FIG 1.