What was found
C-CHECK, CRACK IN FUSELAGE LT SIDE APPROX 9 AFT AND PARALLEL TO WING SCAN LIGHT (TEMP REPAIR INSTALLED) BS 520 BETWEEN STR 16 & 17 LT. REMOVED EXISTING REPAIR DOUBLER, FABRICATED AND INSTALLED PERMANENT REPAIR IAW SRM 53-30-3 FIG 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C-CHECK, CRACK IN FUSELAGE LT SIDE APPROX 9 AFT AND PARALLEL TO WING SCAN LIGHT (TEMP REPAIR INSTALLED) BS 520 BETWEEN STR 16 & 17 LT. REMOVED EXISTING REPAIR DOUBLER, FABRICATED AND INSTALLED PERMANENT REPAIR IAW SRM 53-30-3 FIG 1.