What was found
FLIGHT COMPARTMENT PNL 211AF CORRODED ON BOTTOM SIDE ; DOT#01 A-186 / [01] REMOVED CORROSION IAW B737-700 SRM 51-10-02 PARA 15. VERIFIED ORIGINAL MAT THICKNESS .063'; REMAINING THICKNESS .038'; LOSS OF .025' NO ALLOWABLE LIMITS FOUND.; [02] VERIFIED ITEM 1; [03] DRILLED UP NEW PANEL P/N 141A5133-15 A57758 IAW SRM <BR>51-40-05-0G-0; [04] VERIFIED PART EFFECTIVITY AND LOCATE & DRILL C/W<BR>OK TO PAINT C/W; [05] PAINTED NEW PANEL 211AF IAW AMM 51-21-99-701; [06] INSPECTED ITEM 5; [07] OK TO INSTALL PANEL 211AF; [08] INSTALL NEW PANEL 211AF IAW SRM 51-40-02-0G-0; [09] VERIFIED ITEM 8.<BR>AUDITED