What was found
DURING 2A INSPECTION THE RT FUSELAGE TO VERTICLE STAB DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE AFFECTED DRAG 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 2A INSPECTION THE RT FUSELAGE TO VERTICLE STAB DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE AFFECTED DRAG ANGLE, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.