What was found
AFT FUSELAGE TAIL SECTION 1 EACH SKIN CRACK AT RIGHT STA 1265.603 CANT. MARKED. STOP DRILLED CRACK 1/4 INCH. INSTALLED REPAIR DOUBLER PER SRM 53-01 FIG.2, SOLID FASTENER, PERMANENT REPAIR. (LP5245195)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT FUSELAGE TAIL SECTION 1 EACH SKIN CRACK AT RIGHT STA 1265.603 CANT. MARKED. STOP DRILLED CRACK 1/4 INCH. INSTALLED REPAIR DOUBLER PER SRM 53-01 FIG.2, SOLID FASTENER, PERMANENT REPAIR. (LP5245195)