What was found
FWD GALLEY DOOR (R1) BEAR STRAP HAS CRACK EMANATING FROM FASTENER HOLE OPPOSITE FITTING LATCH. ; / REPAIR AREA MAIN CABIN PER B737-700 AMM 20-60-07-913-801; [02] REMOVED RAIN GUTTERS FROM FWD AREA OF R1 DOOR CUT OUT BETWEEN S-9R AND S-10R AND AND RAIN GUTTER FROM UPPER AREA OF R1 DOOR CUT OUT PER B737-700 SRM 51-40-02-0G-0; [05] REMOVED SKIN PANEL FROM FWD SIDE OF R1 DOOR CUT OUT BETWEEN STR 10R-AND STR-8R FOR ACCESS TO DAMAGED AREA PER B737-700 SRM 51-40-02-0G-0;[07] REMOVED ALL EXISTING FASTENERS IN THE REPAIR AREA PER B737-700 SRM 51-40-02-OG-0; [11] PERFORMED HFEC ON CUT OUT AT REPAIR AREA OF R1 DOOR BETWEEN STR-8R & STR-10R IAW NDTM PART 6;51-00-00 PROCEDURE 23.NO CRACKS.<BR>[NORTEC 600;B/C 166316 ;CALIB.DUE-10/21];17] STARTED FABRICATION OF REPAIR PARTS DOUBLER ; MATERIAL USED 2024 - T3 CLAD .100; PO# 1727238 & TRIPLER MATERIAL USED 2024 - T3 CLAD .063 PO# 1512405; PER B737-700 SRM 53-10-01-2R-6 REPAIR 6 FIG 202; TABLE 201;[25] COMPLETED FABRICATION OF REPAIR PARTS DOUBLER ; MATERIAL USED 2024 - T3 CLAD .100; PO# 1727238 & TRIPLER MATERIAL USED 2024 - T3 CLAD .063 PO# 1512405; PER B737-700 SRM 53-10-01-2R-6 REPAIR 6 FIG 202; TABLE 201; [26] FABRICATED REPAIR PART FLAT PER B737-700 SRM 51-40-05-0G-0