What was found
DURING SCHDULED ROUTINE STRUCTURAL INSP, DISCOVERED RT WING TO FUSELAGE CLOSING ANGLE CRACKED 2.0 INCHES AT FORWARD END. STOP DRILLED CRACK AND INSTALLED 13.5 INCH REPAIR ANGLE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHDULED ROUTINE STRUCTURAL INSP, DISCOVERED RT WING TO FUSELAGE CLOSING ANGLE CRACKED 2.0 INCHES AT FORWARD END. STOP DRILLED CRACK AND INSTALLED 13.5 INCH REPAIR ANGLE.