astm e1886 and astm e1996 test report …...astm e1886-13a, standard test method for performance of...

ASTM E1886 and ASTM E1996 TEST REPORT

Report No.: G0057.01-301-44

Rendered to:

ARCADIA INC. Vernon, California

PRODUCT TYPE: OX Fixed Casement

SERIES/MODEL: IPT200

Test Dates: 06/30/16 Through: 07/15/16 Report Date: 09/16/16 Revision Date: 10/11/16 Test Record Retention End Date: 07/15/20

25800 Commercenter DriveLake Forest, CA 92630

www.intertek.com/building p. 949.448.4100f. 717.764.4129

Test Report No.: G0057.01-301-44 Report Date: 09/16/16

Revision 1 Date: 10/11/16 of 13

1.0 Report Issued To: Arcadia Inc. 2301 East Vernon Avenue Vernon, California 90058 2.0 Test Laboratory: Architectural Testing, Inc., an Intertek company ("Intertek-ATI") 25800 Commercentre Dr. Lake Forest, California 92630 949-460-9600 3.0 Project Summary:

3.1 Product Type: OX Fixed Casement

3.2 Series/Model: IPT200

3.3 Compliance Statement: Results obtained are tested values and were secured by using the designated test methods. The specimens tested met the performance requirements set forth in the referenced test procedures for a ±4597 Pa (±96.0 psf) Design Pressure with missile impacts corresponding to Missile Level D and Wind Zone 3.

3.4 Test Dates: 06/30/16 – 07/15/16

3.5 Test Record Retention End Date: All test records for this report will be retained until July 15, 2020.

3.6 Test Location: Intertek-ATI test facility in Lake Forest, California.

3.7 Test Specimen Source: The test specimens were provided by the client. Representative samples of the test specimens will be retained by Intertek-ATI for a minimum of four years from the test completion date.

3.8 Drawing Reference: The test specimen drawings have been reviewed by Intertek-ATI and are representative of the test specimens reported herein. Test specimen construction was verified by Intertek-ATI per the drawings located in Appendix B. Any deviations are documented herein or on the drawings.

3.9 List of Official Observers:

Name Company Greg Millward Arcadia Inc. Charles Presley Intertek-ATI Jarod Hardman Intertek-ATI



4.0 Test Specifications:

ASTM E1886-13a, Standard Test Method for Performance of Exterior Windows, Curtain Walls, Doors, and Impact Protective Systems Impacted by Missile(s) and Exposed to Cyclic Pressure Differentials ASTM E1996-14a, Standard Specification for Performance of Exterior Windows, Curtain Walls, Doors, and Impact Protective Systems Impacted by Windborne Debris in Hurricanes

5.0 Test Specimen Description:

5.1 Product Sizes: Test Specimens #1 - #3:

Overall Area: 4.1 m² (43.85 ft2)

Width Height

millimeters inches millimeters inches

Overall size 2529 99-9/16 1611 63-7/16

Vent 872 34-5/16 1531 60-1/4

5.2 Frame Construction:

Frame Member Material Description

Head Aluminum Thermally broken compensation channel, Part No. WTR-03, see attached drawing #D-1 and D-3.

Head Aluminum Compensation channel stop, Part No. WWR-04, snap fit into head compensation channel, see attached drawing #D-1.

Sill Aluminum Thermally broken sill starter, Part No. WWR-05, see attached drawing #D-4.

Jamb Aluminum Thermally broken compensation channel, Part No. WTR-01, see attached drawing #D-5 and D-7.

Jamb Aluminum Thermally broken compensation channel, Part No. WTR-02, see attached drawing #D-5 and D-7.

Head Aluminum

Thermally broken extrusion, Part No. WTH-01, inserted into head compensation channel and secured with channel stop, see attached drawing #D-1.

Sill Aluminum Thermally broken extrusion, Part No. WTH-01, inserted over sill starter, see attached drawing #D-4.



5.0 Test Specimen Description: (Continued)

5.0 Frame Construction: (Continued)

Frame Member Material Description

Jamb Aluminum

Thermally broken extrusion, Part No. WTH-01, inserted into jamb compensation channel and secured with channel stop, see attached drawing #D-5 and D-7.

Intermediate vertical

Aluminum

Thermally broken extrusion, Part No. WTT-02, inserted between head and sill extrusion and secured the head and sill, see attached drawing #D-6.

Head, sill, and jambs

Aluminum Glass stop, Part No. WWB-14, snap fit into head, sill and jamb around fixed lite, see attached drawing #D-6, D-5, and D-4.

Joinery Type Detail

All compensation channel corners

Flush Sealed with silicone sealant.

All frame corners Mitered Secured with aluminum corner key, Part No. WWM-01.

5.3 Vent/Sash Construction:

Sash Member Material Description


Aluminum Thermally broken extrusion, Part No. WTZ-02, see attached drawing #D-5 and D-6.

Vent Member Material Description


Aluminum Thermally broken extrusion, Part No. WTZ-02, see attached drawing #D-5 and D-6.


Aluminum Glass stop, Part No. WWB-14, snap fit into vent frame, see attached drawing #D-5 and D-6.

Joinery Type Detail

All corners Mitered Secured with aluminum corner key, Part No. WWM-01.



5.0 Test Specimen Description: (Continued) 5.4 Reinforcement:

Drawing Number Location Material

E-1

Directly above each jamb and one above center locking stile, secured to head with two 3/8" x 3" Hex head wood screws per block.

Aluminum

5.5 Weatherstripping:

Description Quantity Location

Hollow bulb gasket, Part No. 5051 1 row Full span of head compensation channel at interior leg of extrusion, see attached drawing #D-1 and D-3.

Hollow bulb gasket, Part No. 5051 1 row Full span of compensation channel stop at head and jambs, see attached drawing #D-1, D-3, D-5, and D-7.

Hollow bulb gasket, Part No. 5169 1 row Full perimeter of vent frame at interior leg, see attached drawing #D-1, D-2, D-5, and D-6.

Hollow bulb gasket, Part No. 5169 1 row Full perimeter of vent at exterior leg, see attached drawing #D-1, D-2, D-5, and D-6

Hollow bulb gasket, Part No. 5051 2 rows Full span of sill starter at interior and exterior leg of extrusion, see attached drawing #D-2, D-4.

Hollow bulb gasket, Part No. 5051 1 row Full span of jamb compensation channel at interior leg of extrusion, see attached drawing #D-5 and D-7.



5.0 Test Specimen Description: (Continued) 5.6 Glazing: No conclusions of any kind regarding the adequacy or inadequacy of the glass

in any glazed test specimen(s) can be made.

Glass Type

Spacer Type Interior Lite Exterior Lite Glazing Method

1-5/16" IG

Aluminum – Dual Seal

spacer (A-D2)

1/4" clear heat strengthened –

0.090 Sentryglass –

1/4" clear heat strengthened

1/4" clear heat

strengthened

Wet sealed at interior side with structural silicone sealant and secured at exterior face with snap in glazing bead Part No. E-260L

Location Quantity Daylight Opening

Glass Bite millimeters inches

Casement 1 760 x 1413 29-15/16 x 55-5/8 3/4"

Fixed lite 1 1468 x 1470 57-13/16 x 57-7/8 3/4"

5.7 Drainage:

Drainage Method Size Quantity Location

Weep hole 1" x 1/8" 2 Notch in the snap in legs of the glazing bead of the bottom rail to drain the glazing pocket.

Gasket interrupt 1" 2 Gasket was removed directly in front of weep holes to allow for drainage of the vent pocket.

5.8 Hardware:

Description Quantity Location

Cam lock 3

Located approximately 8" from each end of the jamb stile of the casement and mid-span of the jamb stile, secured with two #8 x 1/2" Phillips flat head screws per lock.

Keeper 3 Located directly opposite cam lock on jamb and secured with two #8 x 1/2" Phillips flat head screws per keeper.

5.9 Screen Construction: No screen was utilized.



6.0 Installation: The specimen was installed into a Pine buck. The rough opening allowed for a 1/4" shim space. The exterior perimeter of the window was sealed with silicone sealant.

Location Anchor Description Anchor Location

Head and jambs 1/4" x 2" Hex head wood screw 16" on center spacing through head and 24" on center spacing through jambs.

Sill 1/4" x 2" Hex head wood screw 10" on center spacing through center framing.



7.0 Test Results: The results are tabulated as follows:

ASTM E1886, Large Missile Impact

Conditioning Temperature: 26.7°C (80°F) Missile Weight: 4082 g (9.0 lbs) Missile Length: 2.4 m (8'0") Muzzle Distance from Test Specimen: 4.3 m (14' 0")

Test Unit #1: Orientation within ±5° of horizontal

Impact #1: Missile Velocity: 15.3 m/s (50.3 fps)

Impact Area: Center of casement

Observations: Missile hit target area, glass broke, no penetration.

Results: Pass



Impact Area: Lower right corner of casement


Results: Pass



Impact Area: Top left corner of casement


Results: Pass

Note: See Intertek-ATI Sketch #1-3 for impact locations.



7.0 Test Results: (Continued)

ASTM E1886, Air Pressure Cycling Test Unit #1 Design Pressure: ±4597 Pa (±96.0 psf)

POSITIVE PRESSURE

Pressure Range

Pa (psf)

Number of Cycles

Average Cycle Time

(seconds) Observations

919 to 2298 (19.2 to 48.0)

3500 2.54 Ok, no damage.

0 to 2758 (0.0 to 57.6)


2298 to 3677 (48.0 to 76.8)


1379 to 4597 (28.8 to 96.0)


NEGATIVE PRESSURE

Pressure Range

Pa (psf)

Number of Cycles

Average Cycle Time


1379 to 4597 (28.8 to 96.0)


2298 to 3677 (48.0 to 76.8)


0 to 2758 (0.0 to 57.6)


919 to 2298 (19.2 to 48.0)


Result: Pass



7.0 Test Results: (Continued)

ASTM E1886, Air Pressure Cycling Test Unit #2 Design Pressure: ±4597 Pa (±96.0 psf)

POSITIVE PRESSURE

Pressure Range

Pa (psf)

Number of Cycles

Average Cycle Time


919 to 2298 (19.2 to 48.0)


0 to 2758 (0.0 to 57.6)


2298 to 3677 (48.0 to 76.8)


1379 to 4597 (28.8 to 96.0)


NEGATIVE PRESSURE

Pressure Range

Pa (psf)

Number of Cycles

Average Cycle Time


1379 to 4597 (28.8 to 96.0)


2298 to 3677 (48.0 to 76.8)


0 to 2758 (0.0 to 57.6)


919 to 2298 (19.2 to 48.0)


Result: Pass



7.0 Test Results: (Continued) ASTM E1886, Air Pressure Cycling Test Unit #3 Design Pressure: ±4597 Pa (±96.0 psf)

POSITIVE PRESSURE

Pressure Range

Pa (psf)

Number of Cycles

Average Cycle Time


919 to 2298 (19.2 to 48.0)


0 to 2758 (0.0 to 57.6)


2298 to 3677 (48.0 to 76.8)


1379 to 4597 (28.8 to 96.0)


NEGATIVE PRESSURE

Pressure Range

Pa (psf)

Number of Cycles

Average Cycle Time


1379 to 4597 (28.8 to 96.0)


2298 to 3677 (48.0 to 76.8)


0 to 2758 (0.0 to 57.6)


919 to 2298 (19.2 to 48.0)


Result: Pass

General Note: Upon completion of testing, the specimens met the requirements of Section 7 of ASTM E1996.



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

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. Intertek-ATI will service this report for the entire test record retention period. Test records such as detailed drawings, datasheets, representative samples of test specimens, or other pertinent project documentation, will be retained by Intertek-ATI for the entire test record retention period. 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 Intertek-ATI. For ARCHITECTURAL TESTING, INC.: ____________________________________ ____________________________________ Charles Presley Jarod S. Hardman Technician Laboratory Manager JSH:ss Attachments (pages): This report is complete only when all attachments listed are included. Appendix A: Sketches (3) Appendix B: Drawings (12)



Revision Log

Rev. # Date Page(s) Revision(s)

0 09/16/16 N/A Original report issue.

1 10/11/16 6, Drawing #1 Correct IG measurement, update drawing packet cover page.

This report produced from controlled document template ATI 00498, revised 06/19/15.

Test Report No.: G0057.01-301-44 Report Date: 09/16/16 Revision 1 Date: 10/11/16

Appendix A

Sketches


Sketch #1

Test Specimen #1 impact location


Sketch #2



Sketch #3



Appendix B

Drawings

IPT200 HURRICANE IMPACT WINDOW

MOCK UP

SYSTEM: SERIES IPT200 HURRICANE IMPACT WINDOW FOR 1 5/16" GLAZING

TEST PROCEDURES: TEST SPECIMENS TO BE EVALUATED PER THE FOLLOWING:

ASTM E 1886-13a, STANDARD TEST FOR PERFORMANCE OF EXTERIOR WINDOWS, CURTAIN

WALLS, DOORS AND STORM SHUTTERS IMPACTED BY MISSLE(S) AND EXPOSED TO CYCLIC

PRESSURE DIFFERENTIALS.

ASTM E 1996-14a, STANDARD SPECIFICATION FOR PERFORMANCE OF EXTERIOR WINDOWS,

GLAZED CURTAIN WALLS, DOORS, AND STORM SHUTTERS BY WIND BORNE DEBRIS IN

HURRICANES.

MOCK UP GENERAL RULES

OX CASEMENT FOR 1 5/16" GLAZING

C-1

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E-1

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EXTERIOR INTERIOR


D-1

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EXTERIOR INTERIOR


D-2

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EXTERIOR INTERIOR


D-3

jhardman

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EXTERIOR INTERIOR


D-4

jhardman

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EXTERIOR

INTERIOR


D-5

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EXTERIOR

INTERIOR


D-6

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EXTERIOR

INTERIOR


D-7

jhardman

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WTR03WWR04 WWR05

WTR01 WWR02 WTH01

WWB14

CUSTOM 1" X 3/8" X 5 1/2"

ALUM. SPACER

SB2 CUSTOM 1 11/16" X 1 1/4"

X 5 1/2" ALUM. SHEAR BLOCK


P-1

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WTZ02 WTT02


P-2

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IPT200 X/0 STORM IMPACT WINDOW MOCK UP BILL OF MATERIALS (OUTSIDE GLAZED)

ITEM DESCRIPTION

1. WTR03 (THERMALLY BROKEN COMPENSATING HEAD CHANNEL) 2. WWR04 (COMPENSATING HEAD CHANNEL STOP) 3. WTH01 (THERMALLY BROKEN WINDOW SECTION) 4. WWB14 (GLAZING BEAD) 5. WWR05 (SILL STARTER) 6. WTR01 (THERMALLY BROKEN COMPENSATING JAMB CHANNEL) 7. WTR02 (COMPENSATING JAMB CHANNEL STOP) 8. WTH03 (THERMALLY BROKEN WINDOW SECTION) 9. WTZ02 (THERMALLY BROKEN WINDOW SECTION) 10. WTT02 (THERMALLY BROKEN WINDOW SECTION) 11. 5051 (BULB GASKET) 12. D4-5169 (BULB GASKET) 13. E260L (GLAZING GASKET) 14. 1/4” X 3/8” GLAZING SPACER TAPE 15. DOW CORNING 983 STRUCTURAL SILICONE SEALANT FOR STRUCTURAL SEALS 16. WWM01 (ALUM. CORNER KEY) 17. 1/4” X 2” WOOD SCREWS (PERIMETER FASTENERS) 18. 3/8” X 3” WOOD SCREWS (SHEAR BLOCK FASTENERS) 19. THERMOPLASTIC SHIMS 20. GLASS SETTING BLOCKS/SPACERS 21. DOW CORNING 1199 SEALANT (INTERNAL & PERIMETER SEALS) 22. 1 5/16” OVERALL THICKNESS INSULATING GLASS

MAKE-UP: 6mm CLEAR HEAT STRENGTHENED – ½” LPX CLEAR ANO. SPACER – 6mm CLEAR HEAT STRENGTHENED/.090 SENTRYGLAS PLUS INTERLAYER/6mm CLEAR HEAT STRENGTHENED (LAMINATED)

23. SB2 CUSTOM FABRICATED 1 11/16” X 1 1/4” X 5 1/2” ALUM. SHEAR BLOCK 24. CUSTOM FABRICATED 1” X 3/8” ALUM. SPACER

jhardman

G0057-r0

astm e1886 and astm e1996 test report …...astm e1886-13a, standard test method for performance of...

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