As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ELONGATED HOLES ON EXTERNAL SKIN AND LOWER FLANGER AT STR 36LT AND ELONGATED HOLES ON VERTICAL FLANGE OF THE STR 35 LT BETWEEN FRAME 24 TO FRAME 25 AT LOWER FUSELAGE. PERFORM PERMANENT REPAIR STRINGER 35 LT AND 36LT IAW SRM 53-00-13 PARA 4.A FIGURE 201. THE REPAIR ON EXTERNAL SKIN OF ELONGATED HOLES IS DOCUMENTED ON ERA 537648-14.