What was found
RIGHT WING TO FUSELAGE UPPER ATTACH ANGLE APPEARS TO HAVE A ONE INCH CRACK BY THE RIVET BETWEEN FRAMES 48-49. REPAIRED THE ATTACH ANGLE IAW SRM 53-23-12.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING TO FUSELAGE UPPER ATTACH ANGLE APPEARS TO HAVE A ONE INCH CRACK BY THE RIVET BETWEEN FRAMES 48-49. REPAIRED THE ATTACH ANGLE IAW SRM 53-23-12.