What was found
R/W PANEL 661BB HAS PULLED FASTENER HOLE (MARKED)<[01] IDENTIFIED PANEL IAW SRM 57-51-01-0I-1 FIGURE 3 TABLE 3 ITEM 9<BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 PAR.4 B(5)<BR><BR>DAMAGE TO BE REPAIRED IAW SRM 51-70-04-2R-9 AS DIRECTED BY SRM 57-51-01-2R-1 PAR.4 C TABLE 202<BR><BR>REMOVED DAMAGE FROM (52EA) FASTENER HOLES; ALL MEASURING 0.5' DIA; CLEANED; WITH NO CONTAMINATION NOTED IAW SRM 51-70-04-2R-9 PAR.4 A-C FIGURE 201;[02] VALIDATED APPLICABILITY OF DAMAGE TO BE REPAIRED IAW SRM 51-70-04-2R-9.;[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2<BR><BR>VERIFIED MEASUREMENTS TABLE<BR><BR>VALIDATED REPAIR PER SRM 51-70-04-2R-9;[04] APPLIED SLURRY MIXTURE OF CHOPPED FIBERS AND LAMINATING RESIN BMS8-301 CL1 LOT#JH2EAA8895 TO FASTENER HOLES; AND SET TO CURE USING HOT BONDER ID: NCX000523 DUE:06/2023 IAW SRM 51-70-04-2R-9 PAR.4 D-F;[05] CURED SLURRY; SANDED FLUSH AND CLEANED REPAIR AREAS IAW SRM 51-70-04-2R-9 PARAGRAPH 4.G-I.;[06] UPON CURE OF SLURRY MIX; MULTIPLE DISBONDS WERE FOUND ON ENTIRE PANEL. A NEW PANEL WILL BE REQUIRED TO REPLACE THIS PANEL DUE TO A/C SCHEDULE. NEW PANEL WAS RECEIVED (P/N: 115A3721-14); AND ALL ATTACH HOLES WERE MATCH DRILLED USING TEMPLATE ALL IAW DRAWING 115A3721 SHEET 5 & DRAWING 115A7311 SHEET 7 ; AND SRM 51-20-07-0G-0 PARA'S 4 - 6.;[07] UPDATED PARTS REMOVAL INFO.;[08] APPLIED TOPCOAT TO THE TOOLSIDE OF THE PANEL IAW BOEING PL 115A3721-14;[09] PANEL REPLACED WITH NEW PANEL. JOB COMPLETE.