What was found
DURING SCHEDULED ROUTINE INSP, DISCOVERED LT WING FUSELAGE CLOSING ANGLE CRACKED 1.0 INCH AT FS 288.0. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED ROUTINE INSP, DISCOVERED LT WING FUSELAGE CLOSING ANGLE CRACKED 1.0 INCH AT FS 288.0. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE.