As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EXTERIOR 1 INCH FUSELAGE CRACK AT BS 375 AT STRINGER 15L. TRIMMED OUT DAMAGE. HFEC INSPECTED THE EDGE OF THE TRIM. ENLARGED TRIMMED AREA BY .040 INCH INSURANCE CUT. HFEC ROTARY AND SURFACE PROBLE INSPECTED FASTENER HOLES ALONG STRINGER 15R UNDER THE REPAIR COMMON TO LAP MODIFICATION. REPAIR COMPLETED IAW ECO 33360 AND BOEING SB 737-53A1177. (M)