What was found
FWD PIT TRANSITON PANELS CORRODED AT FASTENER HOLES FROM STA 500C TO 500I <[01]. L/H TRANSITION PANEL FROM STA 500C TO STA 500I EVALUATED ORIG. MAT. THK. = 0.040'; RMV. MAT. = 0.040'; REM. MAT. THK.= 0.00' AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2; TOOL I.D T8224L; CAL. DUE DATE: 02/DEC/25. REMOVED; FABRICATED REPAIR PARTS USING BAC1496-444 7075-T6; PO: 1107340.1; APPLIED ALODINE; PRIMER; CIC; INSTALLED NUTPLATES AND INSTALLED TO AIRCRAFT IAW B737-800 SRM 53-00-53-2R-5. & BAC DWG 1496-444.;[02] VERIFIED L/H TRANSITION PANEL FROM STA 500C TO STA 500I EVALUATED ORIG. MAT. THK. = 0.040'; RMV. MAT. = 0.040'; REM. MAT. THK.= 0.00' AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2; TOOL I.D T8224L; CAL. DUE DATE: 02/DEC/25. REMOVED; FABRICATED REPAIR PARTS USING BAC1496-444 7075-T6; PO: 1107340.1; APPLIED ALODINE; PRIMER; CIC; INSTALLED NUTPLATES AND INSTALLED TO AIRCRAFT IAW B737-800 SRM 53-00-53-2R-5. & BAC DWG 1496-444.;[03] VERIFIED L/H TRANSITION PANEL FROM STA 500C TO STA 500I EVALUATED ORIG. MAT. THK. = 0.040'; RMV. MAT. = 0.040'; REM. MAT. THK.= 0.00' AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2; TOOL I.D T8224L; CAL. DUE DATE: 02/DEC/25. REMOVED; FABRICATED REPAIR PARTS USING BAC1496-444 7075-T6; PO: 1107340.1; APPLIED ALODINE; PRIMER; CIC; INSTALLED NUTPLATES AND INSTALLED TO AIRCRAFT IAW B737-800 SRM 53-00-53-2R-5. & BAC DWG 1496-444.