ASTM E 1886 and ASTM E 1996 TEST REPORT. Report No.: A Rendered to: GLASSCRAFT DOOR COMPANY Houston, Texas

Size: px

Start display at page:

Download "ASTM E 1886 and ASTM E 1996 TEST REPORT. Report No.: A Rendered to: GLASSCRAFT DOOR COMPANY Houston, Texas"

Frederick Pitts
5 years ago
Views:

Architectural Testing ASTM E 1886 and ASTM E 1996 TEST REPORT Report No.: A6458.

SERIES/MODEL: Fiberglass Door This report contains in its entirety: Cover Page: 1 page Report Body: 10 pages Sketches: 3 pages

1 Architectural Testing ASTM E 1886 and ASTM E 1996 TEST REPORT Report No.: A Rendered to: GLASSCRAFT DOOR COMPANY Houston, Texas PRODUCT TYPE: Fiberglass In Swing Glazed Double Doors SERIES/MODEL: Fiberglass Door This report contains in its entirety: Cover Page: 1 page Report Body: 10 pages Sketches: 3 pages Drawings: 12 pages Texas Firm F :18:29-06'00' :26:47-05'00' Test Dates: Through: Report Date: Test Record Retention End Date: 01/10/11 01/14/11 02/09/11 01/14/15

2 Page 1 of Report Issued To: GlassCraft Door Company 2002 Brittmoore Street Houston, Texas Test Laboratory: Architectural Testing, Inc Market Loop Southlake, Texas (817) Project Summary: 3.1 Product Type: Fiberglass In Swing Glazed Double Doors 3.2 Series/Model: Fiberglass Door 3.3 Compliance Statement: Results obtained are tested values and were secured by using the designated test method(s). The samples tested met the performance requirements set forth in the referenced test procedures for a +1513/ 1657 Pa (+31.6/ 34.6 psf) Design Pressure with missile impacts corresponding to Wind Zone 4 and Missile Level D. 3.4 Test Dates: 01/10/ /14/ Test Location: Architectural Testing, Inc. test facility in Southlake, Texas. 3.6 Test Sample Source: The test specimens were provided by the client. Representative samples of the test specimens will be retained by Architectural Testing for a minimum of four years from the test completion date. 3.7 Drawing Reference: The test specimen drawings have been reviewed by Architectural Testing and are representative of the test specimen(s) reported herein. Test specimen construction was verified by Architectural Testing per the drawings located in Appendix B. Any deviations are documented herein or on the drawings. 3.8 List of Official Observers: Name Chris Longoria Tony Brown Company Architectural Testing, Inc. Architectural Testing, Inc.

3 Page 2 of Test Specification(s): ASTM E , Standard Test Method for Performance of Exterior Windows, Curtain Walls, Doors and Storm Shutters Impacted by Missile(s) and Exposed to Cyclic Pressure Differentials. ASTM E , Standard Specification for Performance of Exterior Windows, Glazed Curtain Walls, Doors and Storm Shutters Impacted by Wind Borne Debris in Hurricanes. 5.0 Test Specimen Description: 5.1 Product Sizes: Test Specimens #1 #3: Overall Area: Width Height 4.5 m² (48.3 ft 2 ) millimeters inches millimeters inches Overall size / /2 Operable leaf /2 Fixed leaf /2 5.2 Frame Construction: Frame Member Material Description Head & jambs Compressed fiberboard 1 1/4" x 4 5/8" cross section Joinery Type Detail All corners Coped & butted Secured with four #9 x 3" wood screws 5.3 Leaf Construction: Leaf Member Material Other Rails & stiles Fiberglass clad foam core Solid, single pour foam core

4 Page 3 of Test Specimen Description: (Continued) 5.4 Weatherstripping: Description Quantity Location U shaped foam filled vinyl bulb gasket with vinyl tongue insert 1 row Interior face frame jambs U shaped foam filled vinyl bulb gasket with vinyl tongue insert 1 row Interior face frame head U shaped foam filled vinyl bulb gasket with vinyl tongue insert 1 row Interior face astragal Rubber double row bottom door sweep 1 row Threshold face bottom of each leaf 5.5 Drainage: Sloped threshold was utilized. 5.6 Glazing: Glass Type 1 1/8" IG Spacer Type Aluminum box spacer Interior Lite 1/8" tempered Exterior Lite Laminated consisting of 2 pieces of 1/8" tempered (0.090" interlayer) Glazing Method Interior glazed against a fiberglass glass stop to the exterior and a screw in fiberglass glass stop to the interior. The glass was sealed full perimeter on the interior and exterior. Location Quantity Daylight Opening millimeters inches Glass Bite Operable leaf x x 63 1/4 0.50" Fixed leaf x x 63 1/4 0.50" 5.7 Hardware: Description Quantity Location Door hinge 4 per leaf 12" & 28" up from bottom; 9" & 34 1/2" down from top Flush bolt 2 Inserted into top and bottom of astragal 3 point lock set 1 Inserted into lock stile of operable leaf 5.8 Reinforcement: No reinforcement was utilized.

5 Page 4 of Test Specimen Description: (Continued) 5.9 Screen Construction: No screen was utilized. 6.0 Installation: The specimen was installed into a Spruce Pine Fir wood buck. The rough opening allowed for a 1" shim space. Location Anchor Description Anchor Location Jambs Head & threshold #9 x 3" wood screws 12" from corners, 24" on center thereafter; through top and bottom mounting holes of hinges #9 x 3" wood screws 4" from corners, 12" on center thereafter 7.0 Test Results: The results are tabulated as follows: ASTM E 1886, Large Missile Impact Conditioning Temperature: 20 C (68 F) Missile Weight: 4082 g (9.00 lbs) Missile Length: 2.4 m (8' 0") Muzzle Distance from Test Specimen: 4.9 m (16' 0") Test Unit #1: Orientation within ±5 of horizontal Impact #1: Missile Velocity: 15.5 m/s (50.7 fps) Impact Area: Center of lite, operable leaf Observations: Missile hit target area, no rupture or penetration Results: Pass Impact #2: Missile Velocity: 15.5 m/s (50.9 fps) Impact Area: Upper right corner of lite, operable leaf Observations: Missile hit target area, no rupture or penetration Results: Pass Note: See Architectural Testing Sketch #1 for impact locations.

6 Page 5 of Test Results: (Continued) Test Unit #2: Orientation within ±5 of horizontal Impact #1: Missile Velocity: 15.4 m/s (50.5 fps) Impact Area: Bottom right corner of lite, operable leaf Observations: Missile hit target area, no rupture or penetration Results: Pass Impact #2: Missile Velocity: 15.4 m/s (50.8 fps) Impact Area: Center of lite, operable leaf Observations: Missile hit target area, no rupture or penetration Results: Pass Note: See Architectural Testing Sketch #2 for impact locations. Test Unit #3: Orientation within ±5 of horizontal Impact #1: Missile Velocity: 15.4 m/s (50.8 fps) Impact Area: Upper left corner of lite, operable leaf Observations: Missile hit target area, no rupture or penetration Results: Pass Impact #2: Missile Velocity: 15.4 m/s (50.6 fps) Impact Area: Center of lite, operable leaf Observations: Missile hit target area, no rupture or penetration Results: Pass Note: See Architectural Testing Sketch #3 for impact locations.

7 Page 6 of Test Results: (Continued) ASTM E 1886, Air Pressure Cycling Test Unit #1 Design Pressure: +1513/ 1657 Pa (+31.6/ 34.6 psf) Pressure Range Pa (psf) 303 to 757 (6.3 to 15.8) 0 to 908 (0 to 19.0) 757 to 1210 (15.8 to 25.3) 454 to 1513 (9.5 to 31.6) Pressure Range Pa (psf) 497 to 1657 (10.4 to 34.6) 828 to 1325 (17.3 to 27.7) 0 to 994 (0 to 20.8) 331 to 828 (6.9 to 17.3) Number of Cycles POSITIVE PRESSURE Average Maximum Deflection at Indicator mm (inches) Cycle Time (seconds) #1 #2 # (1.14) 19.8 (0.78) 14.0 (0.55) (1.15) 20.3 (0.80) 14.5 (0.57) (1.55) 27.8 (1.09) 19.8 (0.78) (2.33) 40.3 (1.58) 27.5 (1.08) Number of Cycles Permanent Set mm (inches) 6.5 (0.26) 3.0 (0.12) 3.3 (0.13) NEGATIVE PRESSURE Average Maximum Deflection at Indicator mm (inches) Cycle Time (seconds) #1 #2 # (0.42) 37.3 (1.47) 26.3 (1.03) (0.39) 31.0 (1.22) 24.5 (0.96) (0.33) 26.0 (1.02) 22.3 (0.88) (0.31) 21.5 (0.85) 20.8 (0.82) Permanent Set mm (inches) 1.8 (0.07) 4.6 (0.18) 5.8 (0.23) Observations: No additional damage or deglazing was observed. Result: Pass Note: See Architectural Testing Sketch #1 for indicator locations.

8 Page 7 of Test Results: (Continued) ASTM E 1886, Air Pressure Cycling Test Unit #2 Design Pressure: +1513/ 1657 Pa (+31.6/ 34.6 psf) Pressure Range Pa (psf) 303 to 757 (6.3 to 15.8) 0 to 908 (0 to 19.0) 757 to 1210 (15.8 to 25.3) 454 to 1513 (9.5 to 31.6) Pressure Range Pa (psf) 497 to 1657 (10.4 to 34.6) 828 to 1325 (17.3 to 27.7) 0 to 994 (0 to 20.8) 331 to 828 (6.9 to 17.3) Number of Cycles POSITIVE PRESSURE Average Maximum Deflection at Indicator mm (inches) Cycle Time (seconds) #1 #2 # (0.86) 18.5 (0.73) 14.8 (0.58) (1.06) 20.8 (0.82) 16.5 (0.65) (1.18) 24.8 (0.97) 18.8 (0.74) (1.47) 31.8 (1.25) 23.3 (0.92) Number of Cycles Permanent Set mm (inches) 9.5 (0.37) 3.8 (0.15) 0.8 (0.03) NEGATIVE PRESSURE Average Maximum Deflection at Indicator mm (inches) Cycle Time (seconds) #1 #2 # (0.51) 31.5 (1.24) 18.8 (0.74) (0.50) 28.8 (1.13) 18.3 (0.72) (0.46) 23.5 (0.93) 17.0 (0.67) (0.45) 21.8 (0.86) 16.5 (0.65) Permanent Set mm (inches) 7.3 (0.29) 6.0 (0.24) 3.5 (0.14) Observations: No additional damage or deglazing was observed. Result: Pass Note: See Architectural Testing Sketch #2 for indicator locations.

9 Page 8 of Test Results: (Continued) ASTM E 1886, Air Pressure Cycling Test Unit #3 Design Pressure: +1513/ 1657 Pa (+31.6/ 34.6 psf) Pressure Range Pa (psf) 303 to 757 (6.3 to 15.8) 0 to 908 (0 to 19.0) 757 to 1210 (15.8 to 25.3) 454 to 1513 (9.5 to 31.6) Pressure Range Pa (psf) 497 to 1657 (10.4 to 34.6) 828 to 1325 (17.3 to 27.7) 0 to 994 (0 to 20.8) 331 to 828 (6.9 to 17.3) Number of Cycles POSITIVE PRESSURE Average Maximum Deflection at Indicator mm (inches) Cycle Time (seconds) #1 #2 # (1.00) 21.8 (0.86) 16.0 (0.63) (1.11) 24.3 (0.95) 17.3 (0.68) (1.46) 27.0 (1.06) 20.5 (0.81) (1.80) 33.5 (1.32) 28.8 (1.13) Number of Cycles Permanent Set mm (inches) 7.8 (0.31) 3.8 (0.15) 0.8 (0.03) NEGATIVE PRESSURE Average Maximum Deflection at Indicator mm (inches) Cycle Time (seconds) #1 #2 # (0.47) 29.5 (1.16) 16.8 (0.66) (0.46) 27.8 (1.09) 16.3 (0.64) (0.42) 24.8 (0.97) 15.5 (0.61) (0.39) 19.8 (0.78) 14.3 (0.56) Permanent Set mm (inches) 2.8 (0.11) 3.0 (0.12) 2.8 (0.11) Observations: No additional damage or deglazing was observed. Result: Pass Note: See Architectural Testing Sketch #3 for indicator locations.

10 Page 9 of 10 General Note: Upon completion of testing, the specimens met the requirements of Section 7 of ASTM E Test Equipment: Cannon: Constructed from steel piping utilizing compressed air to propel the missile Missile: 2x4 Southern Pine Timing Device: Electronic Beam Type Cycling Mechanism: Computer controlled centrifugal blower with electronic pressure measuring device Deflection Measuring Device: Linear transducers Tape and film were used to seal against air leakage during structural testing. opinion, the tape and film did not influence the results of the test. In our

Page 10 of 10 The service life of this report will expire on the stated Test Record Retention End Date, at which time such materials as drawings, data sheets, samples of test specimens, copies of

If test specimen contains glazing, no conclusions of any kind regarding the adequacy or inadequacy of the glass in any glazed test specimen(s) can be made.

11 Page 10 of 10 The service life of this report will expire on the stated Test Record Retention End Date, at which time such materials as drawings, data sheets, samples of test specimens, copies of this report, and any other pertinent project documentation, shall be discarded without notice. If test specimen contains glazing, no conclusions of any kind regarding the adequacy or inadequacy of the glass in any glazed test specimen(s) can be made. This report does not constitute certification of this product nor an opinion or endorsement by this laboratory. It is the exclusive property of the client so named herein and relates only to the specimen(s) tested. This report may not be reproduced, except in full, without the written approval of Architectural Testing, Inc. For ARCHITECTURAL TESTING, Inc. Tony Brown Technician John H. Waskow, P.E. Director of Regional Operations Shawn G. Collins, P.E. Laboratory Support Engineer TB:jw/cmd Attachments (pages): This report is complete only when all attachments listed are included. Appendix A: Sketches (3) Appendix B: Drawings (12) This report produced from controlled document template ATI 00498, issued 12/28/10.

12 Appendix A Sketches

13 Operable leaf 3 Sketch #1: Specimen 1 Indicator locations Impact locations

14 Operable leaf Sketch #2: Specimen 2 Indicator locations Impact locations

15 Operable leaf Sketch #3: Specimen 3 Indicator locations Impact locations

16 Appendix B Drawings

ASTM E 1886 and ASTM E 1996 TEST REPORT. Report No.: A Rendered to: GLASSCRAFT DOOR COMPANY Houston, Texas

Architectural Testing ASTM E 1886 and ASTM E 1996 TEST REPORT Report No.: A6839.01 801 18 Rendered to: GLASSCRAFT DOOR COMPANY Houston, Texas PRODUCT TYPE: In Swing Fiberglass Double Doors with Speak Easy