What was found
DURING "C" CHECK INSPECTION, FUSELAGE EXTERIOR BETWEEN STA 1690 & STA 1734 AND L-26L THRU L-28L SKIN WITH CORROSION. REPAIRED FUSELAGE TAIL SECTION PLATING BETWEEN FS 1696 TO FS 1766 AND L-24L TO L-28L IN ACCORDANCE WITH DRAWING NR AIPSAC-N784AL-03/05, SHEETS 1 THRU 5, DATED 08/21/05. ISSUED FAA FORM 8110-3, DATED 01/06/06, APPROVING THIS REPAIR.