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2014-01-17_REPORT - M1980244 (3)
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2014-01-17_REPORT - M1980244 (3)
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Last modified
8/24/2016 5:39:03 PM
Creation date
1/24/2014 9:23:54 AM
Metadata
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Template:
DRMS Permit Index
Permit No
M1980244
IBM Index Class Name
REPORT
Doc Date
1/17/2014
Doc Name
Final Report - Quality Assurance Monitoring & Test Results Phase 5 Slide Repair
From
Cripple Creek & Victor Gold Mining Company
To
DRMS
Email Name
TC1
Media Type
D
Archive
No
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Cripple Creek & Victor Gold Mining Company <br />Phase 5 Slide Repair <br />Final Report <br />Quality Assurance Monitoring & Test Results <br />January 14, 2014 <br />Rim <br />seven fusion seam destructive samples and two extrusion seam destructive samples <br />of the primary geomembrane for the Phase 5 Slide Repair. <br />ECA constructed approximately 3,489 lineal feet of fusion welded seams and 180 <br />lineal feet of extrusion welded seams for the primary geomembrane. The specified <br />frequency of destructive testing was one test per 500 lineal feet of weld. AMEC <br />identified and ECA obtained destructive samples of the geomembrane panel seams at <br />a frequency of one destructive test sample per 498 lineal feet of fusion welded seams, <br />and one per 90 lineal feet of extrusion welded seams. The test frequencies exceeded <br />project requirements. <br />The summaries of destructive test results for fusion seams for the Phase 5 Slide <br />Repair geomembrane are presented in Appendix J.5. The Geomembrane Panel As- <br />Built Drawing presented in Appendix A shows the destructive test sample locations. <br />6.6 Non - Destructive Testing <br />ECA performed non - destructive seam testing on completed seams and geomembrane <br />repairs. Non - destructive testing for seams included pressure testing of fusion welded <br />seams, and vacuum box testing of extrusion - welded seams and repairs. AMEC <br />monitored and documented the non - destructive testing. <br />Prior to pressure testing of fusion seams, ECA heat sealed both ends of the air <br />channel between the two tracks of the double -wedge weld. A pressure gauge was <br />inserted in one end of the sealed channel, the channel was pressurized to <br />approximately 30 pounds per square inch (psi) using an air pump. After pressure <br />stabilization, AMEC monitored the gauge for a minimum of 5 minutes. The maximum <br />allowable pressure drop was 3 psi. <br />ECA and AMEC verified fusion seam continuity before heat sealing both seam ends, <br />completed pressure testing, and with the gauge left in place, cut the opposite end of <br />the seam. If the gauge pressure dropped to zero, the seam was determined to be <br />continuous. In cases where the seam was found to be discontinuous, the seam was <br />subdivided into shorter sections until continuous seam sections were located and <br />passing pressure tests were performed, or the outer edge of the seam was extrusion <br />welded and vacuum box tested. <br />If a pressure test failed, ECA checked the seam section for leakage, repaired any <br />defects, and re- tested the seam. If ECA was unable to find the leak, the seam was <br />divided into two sections, with each section being tested to locate the area of concern. <br />This subdivision process was repeated until the leak location was identified. If the leak <br />area was not located, ECA reconstructed the seam, and then vacuum tested the <br />repair. <br />ECA tested extrusion welded seam sections with a vacuum box. A soap and water <br />solution was applied to the seam section then the vacuum box was then placed over <br />s:\projects \1568 cc &v -ph v slide repair cqa \11.0 certification report\cc &v roc report. docx 15 <br />
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