What was found
DURING 2A INSPECTION THE LT VERTICLE STAB TO FUSELAGE LT DRAG ANGLE WAS FOUND TO HAVE A 20MM CRACK AT FRAME 76. MAINTENANCE R & R THE AFFECTED LT 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 LT VERTICLE STAB TO FUSELAGE LT DRAG ANGLE WAS FOUND TO HAVE A 20MM CRACK AT FRAME 76. MAINTENANCE R & R THE AFFECTED LT DRAG ANGLE, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.