What was found
SKIN PITTING AND ANOMALIES BS 907 - BS 927 STR 6L - STR 7L / [01] REMOVED SKIN PITTING AND ANOMALIES FROM FUSELAGE SKIN AT BS 907-927; STR 6L-7L IAW SRM 51-10-02-0;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] ACCOMPLISHED UT INSPECTION OF BLENDED AREA LOWEST THICKNESS AT ORIGINAL .048 IS .045. .071 IS .066; .080 IS .074; .090 IS .086; .100 IS .095; .125 IS .124 IAW 737 NDTM PART 4; 51-00-00 PROCEDURE 2 TOOL# ATS842 CAL DUE 01/2023.;[04] EVALUATED DAMAGE IN AREA OF L=19.5'XW=8.5'XD=.048 IS .045. .071 IS .066; .080 IS .074; .090 IS .086; .100 IS .095; .125 IS .124. DAMAGE FOUND TO BE IN LIMITS IAW SRM 53-00-01-1A-1;[05] SRM REFERENCE MISSING LEAD MECHANIC VALIDATION.;[06] VERIFIED APPLICABILITY OF SRM 53-00-01-1A-1;[07] VERIFIED CORRECTIVE ACTION ITEM 4-6; IN LIMITS ALL AREAS; OK TO PROCEED.;[08] SKIN PANEL TO BE REPLACED ON FAULT TTG8Q00CRFNS;[09] VERIFIED CORRECTIVE ACTION 8. VERIFIED MEASUREMENT TABLE