What was found
DURING SCHEDULED ROUTINE INSP, DISCOVERED LT WING TO FUSELAGE CLOSING ANGLE CRACKED 1.65 INCHES. STOP DRILLED END OF CRACK AND INSTALLED REPAIR ANGLE. NOTE: ATA CODE UPDATED TO 5300.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED ROUTINE INSP, DISCOVERED LT WING TO FUSELAGE CLOSING ANGLE CRACKED 1.65 INCHES. STOP DRILLED END OF CRACK AND INSTALLED REPAIR ANGLE. NOTE: ATA CODE UPDATED TO 5300.