What was found
AFT ACCESSORY COMP INTERNAL FUSELAGE AFT CANTED STA 1200.019 L SIDE UPPER CORNER HAS CRACK. DRILLED STOP HOLE ON END OF CRACK PER REF BOEING SB 717-53-0006 CONDITION 3 OPTION 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT ACCESSORY COMP INTERNAL FUSELAGE AFT CANTED STA 1200.019 L SIDE UPPER CORNER HAS CRACK. DRILLED STOP HOLE ON END OF CRACK PER REF BOEING SB 717-53-0006 CONDITION 3 OPTION 1.