What was found
UPON REMOVAL OF LT WING PIE SECTION. FOUND CHAFING SPOT 2 INCHES LONG BY 1 INCH WIDE AND .081 DEEP ON STR 19L AT LAP SEAM, STA 720D PLUS 11. REPAIRED DAMAGE PER FEDEX SRM 53-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPON REMOVAL OF LT WING PIE SECTION. FOUND CHAFING SPOT 2 INCHES LONG BY 1 INCH WIDE AND .081 DEEP ON STR 19L AT LAP SEAM, STA 720D PLUS 11. REPAIRED DAMAGE PER FEDEX SRM 53-30-3.