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2009-07-15_REVISION - M1980244 (23)
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2009-07-15_REVISION - M1980244 (23)
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Last modified
6/15/2021 5:52:22 PM
Creation date
7/21/2009 11:01:54 AM
Metadata
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Template:
DRMS Permit Index
Permit No
M1980244
IBM Index Class Name
REVISION
Doc Date
7/15/2009
Doc Name
QA Mon. & Test Results Load Out- Bin Location
From
CC&V
To
DRMS
Type & Sequence
AM9
Media Type
D
Archive
No
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• <br />• <br />• <br />Cripple Creek & Victor Gold Mining Company <br />Cresson Project <br />Quality Assurance Monitoring and Test Results <br />Load Out Bin Relocation <br />July 7, 2009 <br />ameO <br />The summaries of destructive test results for fusion and extrusion seams for the geomembrane <br />are presented in Appendix J-7. Figure 6 shows the destructive test sample locations. <br />6.1.6 Non-Destructive Testing <br />Lonestar performed non-destructive seam testing on completed seams and geomembrane <br />repairs. Non-destructive testing for seams included pressure testing of fusion-welded seams, <br />and vacuum testing of extrusion welded seams and repairs. AMEC monitored and documented <br />the non-destructive testing. <br />Prior to pressure testing of fusion seams, Lonestar heat-sealed both ends of the air channel <br />between the two tracks of the double wedge weld. Lonestar then inserted a pressure gauge in <br />one end of the sealed channel. Lonestar pressurized the air channel to approximately <br />30 pounds per square inch (psi) using an air pump. After pressure stabilization, AMEC <br />monitored the gauge for a minimum of five minutes. The maximum allowable pressure drop <br />was 3 psi. <br />Lonestar 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 the seam. <br />If the gauge pressure dropped to zero, the seam was determined to be continuous. In cases <br />where the seam was found to be discontinuous, the seam was subdivided into shorter sections <br />until continuous seam sections were located and passing pressure tests were performed, or the <br />outer edge of the seam was extrusion welded and vacuum tested. <br />If a pressure test failed, Lonestar checked the seam section for leakage, and repaired and <br />re-tested the seam. If Lonestar was unable to find the leak, the seam was divided into two <br />sections, with each section being tested to locate the area of concern. This subdivision process <br />was repeated until the leak location was identified. If the leak area was not located, Lonestar <br />reconstructed the seam, and then vacuum tested the repair. <br />Lonestar tested extrusion welded seam sections with a vacuum box. Prior to vacuum box <br />testing, Lonestar applied a soap and water solution to the seam section. The vacuum box was <br />then placed over the seam area and energized with a vacuum pump capable of creating a <br />vacuum of not less than 5 psi. Lonestar and AMEC observed the action of the vacuum on the <br />seam for a minimum of ten seconds. Each consecutively tested seam length was overlapped a <br />minimum of 3 inches. If soap bubbles appeared, AMEC marked and documented the leak <br />location. Lonestar then repaired the leak and vacuum tested the repair. This procedure was <br />also followed to test extrusion repairs and extrusion patches. <br />The seam non-destructive test summaries (fusion pressure tests and extrusion vacuum tests) <br />for the geomembrane are presented in Appendix J-6. <br />SAPROJECTS\1125E CCV CQA\H3 - CONSTRUCTION\LOB CERT REPORT\REPORT BODY\LOB CERT REPORT 2009.07.07.DOC <br />22
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