What was found
AFT CABIN R/H I/B CREASEBEAM UPPER SURFACE CORROSION AT STA 945-952 RBL 53-56 WL 208. MRKD<[01] BLENDED CORROSION ON CREASE BEAM(INNER CHORD) FROM STA. 945 TO STA. 952 AT RBL 54? PER SRM 51-10-02. REMOVED .043? OF MATERIAL. REMAINING THICKNESS IS .037?. DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-70-15-1A-1. REMOVED INNER CHORD FROM STA. 887+7? TO STA. 1006; RBL 54 PER SRM 51-40-02 FOR PART REPLACEMENT.;[02] VERIFIED WORK IN C/A #1 BLENDED CORROSION ON CREASE BEAM (INNER CHORD) FROM STA. 945 TO STA. 952 AT RBL 54? PER SRM 51-10-02. REMOVED .043? OF MATERIAL. REMAINING THICKNESS IS .037?. DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-70-15-1A-1. REMOVED INNER CHORD FROM STA. 887+7? TO STA. 1006; RBL 54 PER SRM 51-40-02 FOR PART REPLACEMENT;[03] REMOVED AND REPLACED INNER CHORD (P/N 147A8540U8) FROM STA. 887+7? TO STA. 1006; RBL 54' PER SRM 51-40-02.;[04] INSPECTED WORK IN C/A #3 REMOVED AND REPLACED INNER CHORD (P/N 147A8540U8) FROM STA. 887+7? TO STA. 1006; RBL 54' PER SRM 51-40-02 (RII);[05] R/R R/H CREASE BEAM INNER CHORD (Z-ANGLE) IAW SRM 51-40-02.;[06] C/W INSPECTION. REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]