What was found
AIRCRAFT 6701, FWD CABIN STRUCTURE HAS SMALL CHAFE MARKS AT BS 333 BETWEEN S8L - S10L. REMOVED DAMAGE FROM ATTACH PLATE (STRUT) ON FWD CABIN STRUCTURE STA 333 BTW STR 8-10L & EVALUATED, ORIG. MAT.063. REMOVED MAT .015 REM. MA .048 FOUND TO BE OUT LIMITS IAW SRM 53-00-07-1A. REMOVED, FABRICATED & INSTALLED NEW STRUT PLATE IAW SRM 51-40-02 AND DWG 141N8315 REV V AND REV K. REMOVED DAMAGE FROM FRAME 333.5 BETWEEN STR.8 AND STR.10 IAW B757 SRM 51-10-02. EVALUATED BLEND AREA ON FRAME BTW INTERCOSTAL 2 AND 3, ORIGINAL THICKNESS .090" REMOVED .013" REMAINING AT LOWEST AREA .077" FOUND TO BE OUT OF ALLOWABLE LIMITS IAW B757 SRM 53-00-07-1A. ACCOMPLISHED BLEND REPAIR IAW ER/A 618225-14 REV ORIG SECTION I.