What was found
DURING C INSPECTION, FOUND THE VERTICAL STABILIZER SKIN GOUGED, CRACKED AND PUNCTURED ON RIGHT SIDE NEAR THE JACK SCREW. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTERS 51-30-2, 51-30-5 AND 51-10-8.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C INSPECTION, FOUND THE VERTICAL STABILIZER SKIN GOUGED, CRACKED AND PUNCTURED ON RIGHT SIDE NEAR THE JACK SCREW. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTERS 51-30-2, 51-30-5 AND 51-10-8.