What was found
LEFT WING I/B MAIN FLAP TRAILING EDGE WEDGE HAS LARGE DELAMINATION. (MARKED)<[01] REMOVED DELAMINATED LEFT WING I/B MAIN FLAP TRAILING EDGE WEDGE PER SRM 51-40-02.;[02] INSTALLED LEFT WING I/B MAIN FLAP TRAILING EDGE WEDGE IAW SRM 51-40-02. INFO REFERENCE BOEING DRAWING # 113A2550.;[03] INSTALLED LEFT WING I/B MAIN FLAP TRAILING EDGE WEDGE IAW SRM 51-40-02. INFO REFERENCE BOEING DRAWING # 113A2550. REFERENCE FASTENER TORQUE VALUES IAW SRM 51-40-04.;[04] STEP 2. OF ' CORRECTIVE ACTION ' HAS INCOMPLETE REFERENCE. SHOULD READ : INSTALLED LEFT WING I/B MAIN FLAP TRAILING EDGE WEDGE IAW SRM 51-40-02. INFO REFERENCE BOEING DRAWING # 113A2550. REFERENCE FASTENER TORQUE VALUES IAW SRM 51-40-04.;[05] INSTALLED LEFT WING I/B MAIN FLAP TRAILING EDGE WEDGE IAW SRM 51-40-02. INFO REFERENCE BOEING DRAWING # 113A2550. REFERENCE FASTENER TORQUE VALUES IAW SRM 51-40-04.;[06] INSTALLED LEFT WING I/B MAIN FLAP TRAILING EDGE WEDGE IAW SRM 51-40-02. INFO REFERENCE BOEING DRAWING # 113A2550. REFERENCE FASTENER TORQUE VALUES IAW SRM 51-40-04. C/W INSPECTION