What was found
DURING A-CHECK INSPECTION, THE LT FUSELAGE TO VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED BETWEEN FRAMES 75 - 76 AT ONE RIVET. 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 A-CHECK INSPECTION, THE LT FUSELAGE TO VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED BETWEEN FRAMES 75 - 76 AT ONE RIVET. MAINTENANCE R & R THE AFFECTED DRAG ANGLE, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.