What was found
DURING 4A INSPECTION, THE RT VERTICLE STAB TO FUSELAGE ATTACH ANGLE WAS FOUND TO HAVE A CRACK EXTENDING 22.43MM. MAINTENANCE R & R THE AFFECTED ANGLE, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING 4A INSPECTION, THE RT VERTICLE STAB TO FUSELAGE ATTACH ANGLE WAS FOUND TO HAVE A CRACK EXTENDING 22.43MM. MAINTENANCE R & R THE AFFECTED ANGLE, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.