What was found
FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR ANGLE PER AARD 53-10-00-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR ANGLE PER AARD 53-10-00-2.