Architectural Testing ASTM E 1886 and ASTM E 1996 TEST REPORT Report No.: A6457.01 801 18 Rendered to: GLASSCRAFT DOOR COMPANY Houston, Texas PRODUCT TYPE: In Swing Fiberglass Door with Side Lites SERIES/MODEL: Fiberglass Glazed Door This report contains in its entirety: Cover Page: 1 page Report Body: 10 pages Sketches: 3 pages Drawings: 13 pages Texas Firm F-11869 2011.04.04 16:50:03-05'00' 2011.04.05 11:34:30-04'00' Test Dates: Through: Report Date: Test Record Retention End Date: 03/08/11 03/15/11 03/25/11 03/15/15
Page 1 of 10 1.0 Report Issued To: GlassCraft Door Company 2002 Brittmoore Street Houston, Texas 77043 2.0 Test Laboratory: Architectural Testing, Inc. 2865 Market Loop Southlake, Texas 76092 (817) 410 7202 3.0 Project Summary: 3.1 Product Type: In Swing Fiberglass Door with Side Lites 3.2 Series/Model: Fiberglass Glazed 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: 03/08/2011 03/15/2011 3.5 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 Company Gene Denley Clint Barnett Tony Brown GlassCraft Architectural Testing, Inc. Architectural Testing, Inc. www.archtest.com
Page 2 of 10 4.0 Test Specification(s): ASTM E 1886 05, 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 1996 05, 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: Overall Area: Width Height 4.6 m² (49.4 ft 2 ) millimeters inches millimeters inches Overall size 1845 72 5/8 2489 98 Door leaf 914 36 2419 95 1/4 Side panel (x2) 406 16 2419 95 1/4 5.2 Frame Construction: Frame Member Material Description Head and jambs Compressed fiberboard 1 1/4" x 4 5/8" cross section Joinery Type Detail All corners Coped and butted Secured with four #9 x 3" wood screws 5.3 Leaf Construction: Leaf Member Material Other Rails and stiles Fiberglass clad foam core Solid, single pour foam core 5.4 Side Panel Construction: Leaf Member Material Other Rails and stiles Fiberglass clad foam core Solid, single pour foam core 5.5 Drainage: Sloped threshold was utilized. www.archtest.com
Page 3 of 10 5.0 Test Specimen Description: (Continued) 5.6 Weatherstripping: Description Quantity Location U shaped foam filled vinyl bulb gasket with vinyl tongue insert 1 Row Interior face frame jambs and head Rubber double row bottom door sweep 1 Row Threshold face bottom of door leaf 5.7 Glazing: Glass Type 1" IG Spacer Type 5/8" aluminum box spacer Interior Lite 1/8" tempered Exterior Lite Laminated consisting of 2 pieces of 1/8" tempered and 0.090"PVB 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 Door leaf 1 533 x 1600 21 x 63 0.50" Side lite 2 178 x 1600 7 x 63 0.50" 5.8 Hardware: Description Quantity Location Door hinge 4 12" and 28" from bottom; 9" and 34 1/2" from top; attached with two #9 x 3" and two #9 x 1" wood screws 3 point lock set 1 Lock stile of door leaf 5.9 Reinforcement: No reinforcement was utilized. www.archtest.com
Page 4 of 10 6.0 Installation: The specimen was installed into a Spruce Pine Fir wood buck. The rough opening allowed for a 1/4" shim space. Location Anchor Description Anchor Location Side panel jambs #9 x 3" wood screws 2" from corners and 12" o.c. thereafter Side panel head and sill #9 x 3" wood screw Center of side panel Door head and threshold #9 x 3" wood screws 4" from corners and center 7.0 Test Results: The results are tabulated as follows: ASTM E 1886, Large Missile Impact Conditioning Temperature: 24 C (75 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: 15.4 m/s (50.5 fps) Impact Area: Center daylight opening Observations: Missile hit target area, no rupture or penetration Results: Pass Impact #2: Missile Velocity: 15.5 m/s (50.8 fps) Impact Area: Top right corner of daylight opening Observations: Missile hit target area, no rupture or penetration Results: Pass Note: See Architectural Testing Sketch #1 for impact locations. www.archtest.com
Page 5 of 10 7.0 Test Results: (Continued) Test Unit #2: Orientation within ±5 of horizontal Impact #1: Missile Velocity: 15.4 m/s (50.6 fps) Impact Area: Bottom left corner of daylight opening Observations: Missile hit target area, no rupture or penetration Results: Pass Impact #2: Missile Velocity: 15.5 m/s (50.7 fps) Impact Area: Center of daylight opening 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 (50.6 fps) Impact Area: Top right corner of daylight opening Observations: Missile hit target area, no rupture or penetration Results: Pass Impact #2: Missile Velocity: 15.5 m/s (50.7 fps) Impact Area: Center of door hinge jamb Observations: Missile hit target area, no rupture or penetration Results: Pass Note: See Architectural Testing Sketch #3 for impact locations. www.archtest.com
Page 6 of 10 7.0 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 #3 3500 1.59 13 (0.50) 12 (0.48) 9 (0.34) 300 2.01 14 (0.57) 14 (0.54) 9 (0.37) 600 1.74 20 (0.80) 19 (0.75) 12 (0.49) 100 2.61 25 (0.97) 23 (0.92) 15 (0.60) Number of Cycles Permanent Set mm (inches) 4 (0.14) 3 (0.12) 3 (0.10) NEGATIVE PRESSURE Average Maximum Deflection at Indicator mm (inches) Cycle Time (seconds) #1 #2 #3 50 2.66 17 (0.68) 25 (0.97) 7 (0.26) 1050 1.66 17 (0.66) 22 (0.85) 6 (0.25) 50 2.35 16 (0.64) 20 (0.78) 6 (0.23) 3350 1.62 15 (0.59) 15 (0.61) 5 (0.20) Permanent Set mm (inches) 5 (0.21) 4 (0.15) 3 (0.11) Observations: No additional damage or deglazing was observed. Result: Pass Note: See Architectural Testing Sketch #1 for indicator locations. www.archtest.com
Page 7 of 10 7.0 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 #3 3500 1.69 10 (0.39) 10 (0.39) 9 (0.34) 300 1.97 12 (0.46) 12 (0.46) 10 (0.38) 600 1.84 17 (0.65) 16 (0.64) 13 (0.50) 100 2.44 22 (0.88) 23 (0.89) 17 (0.65) Number of Cycles Permanent Set mm (inches) 2 (0.08) 2 (0.09) 2 (0.08) NEGATIVE PRESSURE Average Maximum Deflection at Indicator mm (inches) Cycle Time (seconds) #1 #2 #3 50 2.67 10 (0.41) 21 (0.81) 10 (0.41) 1050 1.61 10 (0.40) 19 (0.75) 10 (0.40) 50 2.41 9 (0.35) 15 (0.59) 9 (0.35) 3350 1.60 9 (0.34) 14 (0.54) 9 (0.34) Permanent Set mm (inches) 2 (0.09) 3 (0.12) 3 (0.11) Observations: No additional damage or deglazing was observed. Result: Pass Note: See Architectural Testing Sketch #2 for indicator locations. www.archtest.com
Page 8 of 10 7.0 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 #3 3500 1.74 29 (1.13) 23 (0.91) 15 (0.58) 300 2.23 21 (0.81) 15 (0.60) 10 (0.39) 600 1.84 23 (0.92) 18 (0.72) 11 (0.44) 100 2.47 23 (0.89) 20 (0.77) 21 (0.81) Number of Cycles Permanent Set mm (inches) 2 (0.06) 3 (0.10) 2 (0.07) NEGATIVE PRESSURE Average Maximum Deflection at Indicator mm (inches) Cycle Time (seconds) #1 #2 #3 50 2.38 10 (0.39) 16 (0.63) 4 (0.16) 1050 1.28 10 (0.41) 18 (0.70) 5 (0.18) 50 2.48 9 (0.36) 14 (0.57) 4 (0.16) 3350 1.58 8 (0.32) 11 (0.43) 4 (0.14) Permanent Set mm (inches) <1 (0.01) <1 (0.01) <1 (0.01) Observations: No additional damage or deglazing was observed. Result: Pass Note: See Architectural Testing Sketch #3 for indicator locations. www.archtest.com
Page 9 of 10 General Note: Upon completion of testing, the specimens met the requirements of Section 7 of ASTM E 1996. 8.0 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 www.archtest.com
Page 10 of 10 Tape and film were used to seal against air leakage during structural testing. In our opinion, the tape and film did not influence the results of the test. 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 (13) This report produced from controlled document template ATI 00498, issued 12/28/10. www.archtest.com
Appendix A Sketches
1 2 1 2 3 Sketch #1 Specimen #1 Indicator locations Impact locations
1 2 2 1 3 Sketch #2 Specimen #2 Indicator locations Impact locations
1 1 2 2 3 Sketch #3 Specimen #3 Indicator locations Impact locations
Appendix B Drawings