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PERMFILE47866
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PERMFILE47866
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Entry Properties
Last modified
8/24/2016 10:49:53 PM
Creation date
11/20/2007 1:19:53 PM
Metadata
Fields
Template:
DRMS Permit Index
Permit No
M1980244
IBM Index Class Name
Permit File
Doc Date
9/3/2002
Doc Name
Certifcation Report Phase IVa
From
Cripple Creek & Victor Gold
To
DMG
Media Type
D
Archive
No
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9. if no bubbles appeaz after ten (10) seconds, close the vacuum valve and open the <br />bleed valve, move the box over the next adjoining area with a minimum three (3) <br />inches overlap and repeat the process. <br />i0. Alt areas where soap bubbles appear shall be marked and repaired and then retested. <br />11. Test locations, documentation number, date and tester will be indicated with an <br />indelible marker on the geomembrane for each repair or seam section. The color <br />code for indelible mazkers is to be determined at the pre-construction meetings, and <br />strictly adhered to. <br />C. The following nondestructive test procedures are applicable to fusion seaming and shall be <br />followed by CONTRACTOR. <br />1. Seal one end of the seam to be tested. <br />2. Insert needle or other approved pressure feed device through the sealed end of the <br />channel created by the double wedge fusion weld. <br />3. Energize the air pump to verify the unobstructed passage of air through the channel. <br />4. Seal the other end of the channel. <br />5. Energize the av pump to the pressure of approximately thirty (30) psi, close valve, <br />and sustain pressure for approximately five (5) minutes. <br />6. If loss of pressure exceeds three (3) psi, or pressure does not stabilize, locate faulty <br />azea, repair and retest. <br />. 7. Remove needle or other approved pressure feed device. <br />8. Repair pressure test locations as described in Section 3.11. <br />9. Beginning and ending pressures and times, test locations, documentation number, <br />date and tester will be indicated with an indelible marker on the liner at each test <br />interval location. <br />D. The following procedures shall apply to locations where seams cannot be non-destructively <br />tested, as determined by CERTIFYING ENGINEER: <br />If the seam is accessible to testing equipment prior to final installation, the seam shall <br />benon-destructively tested prior to final installation. <br />2. If the seam cannot be tested prior to final installation, the seaming operations shall be <br />observed by CQA Monitor for uniformity and completeness. <br />E. In the event that seam continuity cannot be demonstrated for anon-destructive test of a fusion <br />seam as outlined above, fire CONTRACTOR shall perform the non-destructive testing over <br />smaller azeas as a means of defining the questionable azea, and shalL• <br />1. Extrusion weld the outside edge of the questionable seam azea and vacuum box test <br />the extrusion weld; or, <br />Z. Cap the questionable area and vacuum test the cap. <br />3.09 DESTRUCTIVE TESTING: <br />Section 02776 Page 17 of 20 October 25, 2000 <br />Geomembrane Golder Associates Revision 8 <br />I \0012201\Oa00\CERTREPOBOZWPPENDSNPPE\993-309902'/]61a8.DOC <br />
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