What was found
DUE TO CRACK FINDING IN THE L/H BS 663 FRAME FITTING; THE R/H FRAME FITTING IS BEING REPLACED (PICKLE FORK) PN 144A2400-38. ASSY P/N 144A2400-36#B / [01] STARTED REMOVE FASTENERS RH FRAME STA 663 LH IAW B737-700 SRM 51-40-02;[02] VERIFIED ACTION 1;[03] REMOVED LH UPPPER PICKLE FORK SPLICE INBD PLATE; FWD PICKLE FORK WEB PLATE; INBD FWD AND AFT SPLICE STRAPS IAW SRM 51-40-02;[04] REMOVED RH PICKLE FORK IAW SRM 51-40-02-0G-0;[05] VERIFIED ACTION 4;[06] ACCOMPLISHED OPEN HOLE HFEC IAW B737 NDT P6 51-00-00 P16<BR><BR>ACCOMPLISHED COUNTERSINK HFEC IAW B737 NDT P6 53-30-00 P3<BR><BR>TOOL 36303 DUE 16DEC22<BR>NO CRACKS NOTED;[07] RECIEVED SHIM P/N 11A0150-19 MILLED TO .160' FROM BACKSHOP W/O# 44141-0000-0007 IAW BOEING DWG 110A0150 REV B.;[08] VERIFIED STEP 7 <BR>OK TO TREAT AND PRIME;[09] APPLIED CHEMICAL CONVERSION AND PRIMER TO -19 SHIM IAW AMM 51-21-41-370-803 AND AMM 51-21-72-370-804 AND BOEING DWG # 11A10150 REV B.;[10] VERIFIED STEP 9 C/W;[11] LH UPPPER PICKLE FORK SPLICE INBD PLATE; FWD PICKLE FORK WEB PLATE; INBD FWD AND AFT SPLICE STRAPS REMOVED IN STEP 3 ARE REMOVED AND INSTALLED ON FAULT TTG8Q00EPRK0;[12] VERIFIED STEP 11 C/W;[13] REFER TO EA 22-153-02730 SUMMARY REQUIREMENT; BARCODE: TTG8Q00FGKJE;[14] 'REPLACED THE RH STA 663.75 FRAME FITTING (PICKLE FORK) PER EA 22-153-02730;[15] VERIFIED STEP 14;[16] REPLACED THE RH STA 663.75 FRAME FITTING (PICKLE FORK) PER EA 22-153-02730;[17] AUDIT C/W