As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON LT HORIZ STAB FRONT SPAR UPPER CHORD, STAB STA 4.5 BLENDED CORROSION, ORIGINAL THICKNESS IS .120 INCHES. MATERIAL REMOVED .052 INCHES. MATERIAL REMAINING .088 INCH REPAIRED UPPER CHORD REF EA NR 7-5510-114204 DATED 7-11-08. THIS IS CLASSIFIED AS A MAJOR REPAIR.