What was found
INSPECTION FOUND A HOLE CHAFED THROUGH VERTICAL STABILIZER SKIN AT UPPER LT SIDE ABOVE RUDDER FAIRING. A FREEZE PLUG AND DOUBLER WERE INSTALLED IAW EA 9-5532-2-A0792.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A HOLE CHAFED THROUGH VERTICAL STABILIZER SKIN AT UPPER LT SIDE ABOVE RUDDER FAIRING. A FREEZE PLUG AND DOUBLER WERE INSTALLED IAW EA 9-5532-2-A0792.