What was found
DURING 4A INSPECTION, THE LT AFT FUSELAGE TO VERTICLE STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. DRAG ANGLE REPLACED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING 4A INSPECTION, THE LT AFT FUSELAGE TO VERTICLE STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. DRAG ANGLE REPLACED.