What was found
RIGHT WING TO FUSELAGE UPPER AREA PANEL 677CT LOWER SUPPORT ANGLE HAS (8EA) ELONGTED HOLES. INSTALL NEW SPAR . NEW PART WAS INSTALLED IAW SRM 51-40-21-001.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING TO FUSELAGE UPPER AREA PANEL 677CT LOWER SUPPORT ANGLE HAS (8EA) ELONGTED HOLES. INSTALL NEW SPAR . NEW PART WAS INSTALLED IAW SRM 51-40-21-001.