What was found
LEFT SIDE OF VERT STAB TO FUSELAGE AFT ATTACH ANGLE APPEARS TO HAVE A CRACK ON THE L/E. COMPLIED WITH REPAIR OF LT AFT ANGLE IAW EO-CR-53MR-164R1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT SIDE OF VERT STAB TO FUSELAGE AFT ATTACH ANGLE APPEARS TO HAVE A CRACK ON THE L/E. COMPLIED WITH REPAIR OF LT AFT ANGLE IAW EO-CR-53MR-164R1.