What was found
DURING C INSPECTION, FOUND A GROOVE CHAFED INTO THE LEFT SKIN ON THE VERTICAL STAB NEAR THE FAIRING ATTACH BRACKET. REPLACED VERTICAL STAB SKIN PANEL IAW DC-9 SRM CHAPTER 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C INSPECTION, FOUND A GROOVE CHAFED INTO THE LEFT SKIN ON THE VERTICAL STAB NEAR THE FAIRING ATTACH BRACKET. REPLACED VERTICAL STAB SKIN PANEL IAW DC-9 SRM CHAPTER 51-30-2.