What was found
COMP- REPAIR LH VAPOR BARRIER CRACK<[01] MEASUREMENTS.;[02] REMOVED THE DAMAGED PLIES AND PREPARED DAMAGED AREA TO APPLY THE GLASS FABRIC REPAIR PLIES; DRILLED 0.25 INHC DIAMETER STOP HOLES AT THE CRACK END. REF B737 SRM 51-70-04-2R-10 PARAGRAP 4 AND SRM 57-10-10-2R-2 PARAGRAPH 3 A.;[03] VERIFIED REMOVAL OF THE DAMAGED PLIES AND PREPARED DAMAGED AREA TO APPLY THE GLASS FABRIC REPAIR PLIES; DRILLED 0.25 INHC DIAMETER STOP HOLES AT THE CRACK END. REF B737 SRM 51-70-04-2R-10 PARAGRAP 4 AND SRM 57-10-10-2R-2 PARAGRAPH 3 A. OK TO INSTALL THE REPAIR.;[04] REPAIRED DAMAGED AREA AND TAP TEST INSPECTION AT LH VAPOR BARRIER AS PER B737SRM 51-70-04-2R-10 AND NTM 51-05-01 MATERIAL USE RESIN PO#1800112 FIBERGLASS PO#1690463;[05] VERIFIED STEP NO 4. OK TO DRILL HOLES.;[06] LOCATED AND DRILLED REPAIRED VAPOR BARRIER PER REF SRM 51-40-05-0G-0;[07] PRIMER AND TOPCOAT APPLICATION REF TASKCARD #TTG8Q00HH5FG;[08] VERIFIED 6-7.;[09] CORRECTION TO STEP #5.<BR>RII<BR>VERIFIED STEP NO 4. OK TO DRILL HOLES.;[10] (RII) FINAL INSPECTION; WORK PERFORMED.