What was found
(B757-06-3-0328) RIGHT WING APPROX. FSS 228 UNDER #6 SLAT, VERTI CAL STIFFNER AT DUCT ATTACH BRACKET CHAFING DUE TO BRACKET BEING LOOSE AS MARKED. TRANSCRIBED FROM HAECO GSO NR 9280145. AND BOEING DWG 112N2038 REV-. INSTALLED NEW STIFFENER IAW REO-G2 4456, B757-200 SRM 51-40-02 AND BOEING DWG 112N2002 REV D EVALUATED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW B757-200 SRM 57-20-10-1A-2 ORIGINAL THICKNESS .130, DAMAGE DEPTH .100 MATERIA L REMAINING .030. REMOVED VERTICAL STIFFENER IAW B757-200 SRM 51 -40-02. FABRICATED NEW STIFFENER IAW BOEING PL 112N2038 REV D