What was found
LEFT WING; DEFLECTION CONTROL RIB; INBOARD ATTACH ANGLE TO WEB IS CRACKED AT FASTENER HOLES COMMON TO DEFLECTION CONTROL RIB. A045-005 ; / [01] REMOVED LH WING DEFLECTION CONTROL RIB ATTACH ANGLE IAW SRM 51-40-02; [02] VERIFIED NEW ANGLE TO BE MPN: 115A6260-1 ATAG: A106490 IAW DWG: 115A6200 REV: A; [03] LOCATED AND DRILLED NEW ANGLE IAW DWG: 115A6200 REV: A AND SRM 51-40-05; [04] VERIFIED STEPS 2 AND 3<BR>OK TO INSTALL; [05] INSTALLED ANGLE IAW SRM 51-40-02 AND DWG: 115A6200 REV: A; [06] VERIFIED ITEM 5; [07] C.I.C;ED NEW ANGLE I.A.W MM 51-21-91-620-802; [08] STEP 7 C/W AUDIT DONE