AAMA 506-2000 LARGE MISSILE IMPACT
PEERLESS PRODUCTS
SERIES 4130 SINGLE HUNG
REPORT #CCLI-05-058
May 23, 2005
TABLE OF CONTENTS
1.
PROJECT DATA..................................................................................................... 1
2.
SCOPE…................................................................................................................ 1
3.
SUMMARY ............................................................................................................. 1
4.
IMPACT ACCEPTANCE CRITERIA ....................................................................... 2
5.
TEST SPECIMEN ................................................................................................... 2
6.
PERFORMANCE RESULTS................................................................................... 3
7.
CONCLUSION ........................................................................................................ 5
APPENDIXES
APPENDIX A:
PEERLESS PRODUCTS SERIES 4130 SINGLE HUNG DRAWINGS
APPENDIX B:
PHOTOGRAPH
S-UNITED, INC.
A Quality Control Company
AAMA 506-2000 LARGE MISSILE IMPACT
PEERLESS PRODUCTS
SERIES 4130 SINGLE HUNG
REPORT #CCLI-05-058
June 13, 2005
Page 1 of 5
1. PROJECT DATA
Project:
ASTM E 1886 & 1996
Series 4130 Single Hung
Date(s) of Testing:
April 4-5, 2005
Tested For:
Peerless Products, Inc
2403 S. Main, P.O. Box 431
Ft. Scott, KS 66701
Witnessed By:
(All or Partial Viewing)
Coby Jones
Peerless Products Inc.
Jeffrey Crump
Construction Consulting Laboratory, International (CCLI)
Office: (620) 223-4610
2. SCOPE
CCLI was requested to test and report the performance results on a Peerless
Products Series 4130 Single Hung. Tests were performed in accordance with
AAMA 506-2000 “Voluntary Specification for Hurricane Impact and Cycle Testing of
Fenestration Products” using methods ASTM E 1996-99 and ASTM E 1996-03
“Standard Specification for Performance of Exterior Windows, Glazed Curtain Walls,
Doors, and Storm Shutters Impacted by Windborne Debris in Hurricanes” and
ASTM E1886-97 “Standard Test Method for Performance of Exterior Windows,
Curtain Walls, Doors, and Storm Shutters Impacted by Missile(s) and Exposed to
Cyclic Pressure Differentials”. Tests were performed at Construction Consulting
Laboratory, International, (CCLI) in Carrollton, TX.
3. SUMMARY
Three specimens of a Peerless Products Series 4130 Single Hung were large missile
impacted with a Type C missile in accordance with ASTM E 1996-99 and Type D
missile in accordance with ASTM E 1996-03. They were cycled at a Design 73.3 PSF
positive and negative in accordance with ASTM E 1886-97.
CONSTRUCTION CONSULTING LABORATORY, INTERNATIONAL
AAMA 506-2000 LARGE MISSILE IMPACT
PEERLESS PRODUCTS
SERIES 4130 SINGLE HUNG
REPORT #CCLI-05-058
June 13, 2005
Page 2 of 5
4. IMPACT ACCEPTANCE CRITERIA
The test specimen shall resist the large missile impact with no tear formed longer
than 5" (130 mm) or no opening formed through which a 3" (76 mm) solid sphere
can freely pass when evaluated upon completion of missile impacts and test loading
program.
5. TEST SPECIMEN
Product Type:
Series Model:
Specifications:
Design:
Frame Size:
Vent Size:
Configuration:
Aluminum Single Hung, Product Drawings, Appendix A;
Photographs, Appendix B
Peerless Products Series 4130 Single Hung
AAMA 506-2000 / ASTM E 1996-99 Large Type-C Missile /
ASTM E 1996-03 Large Type-D Missile
+73.3 / -73.3
4'-0" x 6'-0"
3'-9½" x 3'-½"
O/X
Refer to Mock-Up drawings in Appendix A. This report is not complete unless
this laboratory symbol is stamped and initialed onto the drawings.
WEATHER-STRIPPING: One row pile of weather strip with integral plastic fin
(0.280" thickness), located at exterior face of sash stiles (0.280" thickness) lateral
face of sash stiles (0.280" thickness) and at the interior face of fixed meeting rail.
One row of bulb vinyl located at the exterior face of sash bottom rail.
HARDWARE: One (1) ultra lift balance per stile. One (1) cam lock 9" from each
end of sash top rail, total of two (2). Keepers at fixed meeting rail. Plastic sash
guide attached to top of each sash stile by #8 x ¾" screws. Tilt latch screw at
each end of sash top rail. Pivot bar at each end of sash bottom rail. Windlock at
center of each stile.
GLASS: Sealed insulating glass: 2 pcs. ¼" annealed glass at exterior, ½"
aluminum air space, 1/8" annealed glass x .090" PVB inner layer laminate x 1/8"
annealed glass located at interior, with an overall thickness of 1.09".
CONSTRUCTION CONSULTING LABORATORY, INTERNATIONAL
AAMA 506-2000 LARGE MISSILE IMPACT
PEERLESS PRODUCTS
SERIES 4130 SINGLE HUNG
REPORT #CCLI-05-058
June 13, 2005
Page 3 of 5
GLAZING: Interior glazed with silicone at the exterior face of glass, silicone heel
bead and aluminum snap in glazing bead with glazing gasket sealed in place at
the interior face of glass.
WEEP ARRANGEMENT: One (1) 1" x 3/16" weep hole located 3" from each end
of sill center leg.
SEALANT: Narrow joint seam sealer at all frame and sash corners. Narrow joint
seam sealer at fixed interlock-to-frame jamb connections.
REINFORCEMENT: None.
OTHER FEATURES: Frame and sash members thermally broken. Frame
corners are coped, butted, and attached with two (2) #8 x ¾" SMS per connection.
Sash corners are coped, butted, and attached with two (2) #8 x ¾" SMS per
connection. Fixed interlock attached to frame jambs with three (3) #8 x ¾" SMS
per connection.
INSTALLATION: Test specimen installed in a #2 (2” x 8”) spf #2 wood test buck
with #12 x 2½" screws spaced 4” from each end and 12” O.C. at frame interior
jambs and 8” from each end and 1 at center of frame head and sill.
Date Tests Started:
Date Tests Completed:
Testing Performed at:
April 4, 2005
April 5, 2005
Construction Consulting Laboratory, International
6. PERFORMANCE RESULTS
*For gateway performance results see CCLI Report #04-139
Method: ASTM E 330-02
Title of Test
Test Method
Uniform Structural ASTM E 330-02
-Positive
-Negative
-Permanent Set
Measured
Allowed
135.0 PSF
135.0 PSF
0.0625"
135.0 PSF
135.0 PSF
0.182"
Specification: ASTM E 1886-97 / ASTM E 1996-99 Missile Level Type C and
ASTM E 1996-03 Missile Level Type-D (#2 yellow pine weighing 9 lbs 3 ozs
and measured 8'- 2" overall).
CONSTRUCTION CONSULTING LABORATORY, INTERNATIONAL
AAMA 506-2000 LARGE MISSILE IMPACT
PEERLESS PRODUCTS
SERIES 4130 SINGLE HUNG
REPORT #CCLI-05-058
June 13, 2005
Page 4 of 5
Test Specimen 1
Par No
Speed
5.3.1.1
50.9fps
5.3.2.1
50.1fps
Test Specimen 2
Par No
Speed
5.3.1.2
50.2fps
5.3.2.2
50.2fps
Test Specimen 3
Par No
Speed
5.3.1.3
50.7fps
5.3.3.6
50.4fps
Rotation
0º
0º
Title of Test
Center of Glass
Upper Right Corner
Measured
No Penetration
No Penetration
Allowable
See Section 5
See Section 5
Title of Test
Lower Left Corner
Center of Glass
Measured
No Penetration
No Penetration
Allowable
See Section 5
See Section 5
Title of Test
Upper Right Corner
Center of Meeting Rail
Measured
No Penetration
No Penetration
Allowable
See Section 5
See Section 5
Rotation
0º
0º
Rotation
0º
0º
TEST SPECIMEN
TEST SPECIMEN
TEST SPECIMEN
- Indicates 2nd Impact to Specimen.
The laboratory temperature was maintained at 66º F for the duration of testing.
Test specimens were stored in the lab prior to testing and the skin temperature of
the aluminum was recorded at 68º F.
Visual inspections performed on the test specimens revealed there were no
penetrations through the laminate and no separation of vision-to-frame glazing at
the conclusion of the large missile impact tests.
Specification: ASTM E 1886-97
Load Direction
Sequence
Range
Cycle Time
CONSTRUCTION CONSULTING LABORATORY, INTERNATIONAL
Cycles
Damage
AAMA 506-2000 LARGE MISSILE IMPACT
PEERLESS PRODUCTS
SERIES 4130 SINGLE HUNG
REPORT #CCLI-05-058
June 13, 2005
Page 5 of 5
73.3 PSF
Positive
Cycle 1
Cycle 2
Cycle 3
Cycle 4
0.2 P max to 0.5 P max
0 to 0.6 P max
0.5 P max to 0.8 P max
0.3 P max to 1.0 P max
< 3 seconds
< 3 seconds
< 3 seconds
< 3 seconds
3500
300
600
100
None
None
None
None
Load Direction
73.3 PSF
Negative
Sequence
Cycle 1
Cycle 2
Cycle 3
Cycle 4
Range
0.3 P max to 1.0 P max
0.5 max to 0.8 P max
0 to 0.6 P max
0.2 P max to 0.5 P max
Cycle Time
< 3 seconds
< 3 seconds
< 3 seconds
< 3 seconds
Cycles
50
1050
50
3350
Damage
None
None
None
None
Visual inspections performed on the test specimens revealed there were no
penetrations through the laminate and no separation of vision-to-frame glazing at
the conclusion of the cyclic pressure differentials.
Detailed extrusion and assembly drawings indicating measured wall thickness and
corner construction are on file and have been compared to the test sample
submitted. These records will be retained at CCLI for a period of four years.
7. CONCLUSION
The test specimen, Peerless Products Series 4130 Single Hung, complied with
AAMA 506-2000 and the large missile impact requirements of ASTM E 1996-99
using a Type-C large missile and ASTM E1996-03 using a Type-D large missile
and cyclic pressure differentials of 73.3 PSF positive and negative noted in ASTM
E 1886-97. The above results were achieved by using the designated test
methods and indicate compliance with the above specification. This report does
not constitute certification of this product.
Respectfully submitted,
CONSTRUCTION CONSULTING LABORATORY, INTERNATIONAL
____________________
JEFFREY W. CRUMP
TESTING TECHNICIAN
______________________
W ESLEY A. W ILSON
LABORATORY MANAGER
CONSTRUCTION CONSULTING LABORATORY, INTERNATIONAL
AAMA 506-2000 LARGE MISSILE IMPACT
PEERLESS PRODUCTS
SERIES 4130 SINGLE HUNG
REPORT #CCLI-05-058
May 23, 2005
APPENDIXES
CONSTRUCTION CONSULTING LABORATORY, INTERNATIONAL
AAMA 506-2000 LARGE MISSILE IMPACT
PEERLESS PRODUCTS
SERIES 4130 SINGLE HUNG
REPORT #CCLI-05-058
May 23, 2005
APPENDIX A
PRODUCT DRAWINGS
DRAWING
DIE #
BILL OF MATERIALS
4130 SINGLE HUNG
JAMB
MEETING RAIL
STILE
SASH TOP RAIL
SASH BOTTOM RAIL
FRAME SILL
FRAME HEAD
GLAZING BEAD
041-079
041-080
041-083
041-159
041-160
041-351
041-077
091-088
CONSTRUCTION CONSULTING LABORATORY, INTERNATIONAL
AAMA 506-2000 LARGE MISSILE IMPACT
PEERLESS PRODUCTS
SERIES 4130 SINGLE HUNG
REPORT #CCLI-05-058
May 23, 2005
APPENDIX B
PHOTOGRAPH
CONSTRUCTION CONSULTING LABORATORY, INTERNATIONAL
AAMA 506-2000 LARGE MISSILE IMPACT
PEERLESS PRODUCTS
SERIES 4130 SINGLE HUNG
REPORT #CCLI-05-058
May 23, 2005
PHOTOGRAPH 1
Series Model:
Specifications:
Design:
Frame Size:
Vent Size:
Configuration:
Peerless Products Series 4130 Single Hung
AAMA 506-2000 / ASTM E 1996-99 Large Type-C Missile /
ASTM E 1996-03 Large Type-D Missile
+73.3 / -73.3
4'-0" x 6'-0"
3'-9½" x 3'-½"
O/X
- END OF REPORT CONSTRUCTION CONSULTING LABORATORY, INTERNATIONAL