ML20059E790
| ML20059E790 | |
| Person / Time | |
|---|---|
| Site: | Salem, Cooper, Arkansas Nuclear, Waterford  |
| Issue date: | 01/22/1990 |
| From: | Croak B ATI |
| To: | |
| Shared Package | |
| ML20059E770 | List: |
| References | |
| 89-020-3, 89-20-3, NUDOCS 9311030351 | |
| Download: ML20059E790 (79) | |
Text
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, germs;r7.wi FINAL REPORT 89-020-3 ASTM E-72 LOAD TESTING OF 2 HR SOLID STUD WALL January 22,1990 Referencing :
Architectural Testing Inc.
Test Report No. ATI-7008-3 9311030351 930714 PDR ADDCK 05000272 ,
F PDR- L.
.. ARCHITECTURAL .:
M0 WCWGE PLACE
- YORK PA17402
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- Ftt0NE717 646 7700 BUILDING CONSTRUCTION PANEL TEST REPORT 3]
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Rendered to:
a, PROMAT,1NC. ,,
Village Center Drive ,
Reading, Pennsylvania 19607 a n
Report No: ATI-7008 3 Test Dates: 10 89 J$ '
Thtu: 12 89 Mr t
Report Date: 01 90 ilENERAL TEST SPECIMEN DESCRIPTION: Three layer, solid wall sections consisting of three layers of Promat-H panels as supplied by Promat,Inc., Reading, Pennsylvania .
REFERENCED DRAWINGS: Promat, Inc. AAD-186 (modified), AAD-189, AAD-1(M $.
(modified); Architectural Testing, Inc. 7008 Sheets 1 through 4 TEST METHODS:
S ASTM E72-80 " Standard Methods of Conducting Strength Tests of Panels for Building Construction." l ASTM E564-76 " Standard Method of Static Lead Test for Shear Resistance '
of Framed Walls for Buildings."
TEST PROCEDURE: ASTM E72-80 is broken down into five types of test to be conducted f on wall sections. They are as follows: ~:
Section 9: Compressive Imad (designated in this report as Test A).
Section 10: Tensile Load (designated in this report as Test B). ,
Section 11: Transverse Load (designated in this report as Test C). -!
Section 13: Concentrated Load (designated in this report as Test D). ;
i Section 14: Racking load (designated in this report as Test E).
Eleven wall sections were fabricated per the client's specifications, to satisfy the sample !
requirements. The test sample size varied for the racking load test. A detailed description "
of the test specimen and the test apparatus will follow. All wall sections were constructed at (SeeArchitectural Testing, Inc.
Promat, Inc. 5R89-020-3; (ATI)toby attached thisDavid report Haines and PhotoofNos.
Promat, Inc.
I through 4. and ATI p)erson TEST A: Compressive load Test Three wall sections were fabricated in accordance with details on Promat, Inc. Drawings :
Inc. connections instead of nails. The No. AAD-186 wall sections as modified consisted of tw'oby Architectural 20mm Testing,ium silicate boards, one on each face, Promat-H calc and one 25mm board in the center. >
t i
- ATI-7008-3 i Page 2 of 4 ;;
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The test specimens as described above were installed into a steel test fixture as detailed on ATI Drawing 7008 Sheet 1. Two 3/8" thick by 1" wide 68"long steel bars with wooden spacers attached were used to hold the test panel plum sliding the bars through item 9 i I
on the referenced drawing. Three "ENERPAC" RCS 20 ydraulic cylinders were placed ,
beneath the cylinderitem 3 of and the the of bottom same drawing the steel I-beam and steel item 3). The sp(acers to fill cyhnders were the such spaced space betwe that there was one cylinder at each end and one at the center of the test panel. The hydraulic cylinders were connected to a manifold which in turn was connected to a a, "GNERPAC" P-391 hydraulic hand-pump. Each hydraulic cylinder had a 1-3/4" stroke and a 4.43 sq. in. effective cylinder area. !
w Four compressometers and two deflectometers were attached to the test specimen per the Q, referenced test method with a 88" effective span length. All gauges were set at zero, then loads were applied at 20 bar increments which is eqmvalent to a total load on the specimen
- of 3,854 pounds. All gauges were read as soon as each load was reached, five mmutes at -
each load, as soon as each load was removed, and again five minutes after each load was removed. The incremental loading was continued until failure of the wall section was observed. (See Photo Nos.5 through 11.) 3 TEST B: Tensile Load Test Three wall sections with the same fabrication details as those for the compressive load test were constructed for the tensile load test.
The same test fixture was used as for the compressive load test with the addition of six l and bottom plate of the test i 5/16" diameter panel which securedby it2"tolong machine the fixture. boltswere The bolts andspace washers per top' at 2,l/2* from one end every 8.7" The hydraulic cylinders were placed on top or nem 3 on ATI Drawing 7008 Sheet 1. The cylinders were spaced the same as they were for Test A. The same cylinders ;
i and pump that was used for Test A was used for the tensile load test.
Four extensometers and two deflectometers were attached to the test specimen per the referenced test method with a 87-1/2" effective span length. All gauges were set to zero, then loads were applied at 20 psi increments which is equivalent to a total load on the ,
- specimen of 266 pounds. .All gauges were read as soon as each load was reached, five ,
minutes at each load, as soon as each load was removed, and again five minutes after each '
load was removed. The incremental loading was continued until failure of the wall section was observed. (See Photo Nos. 5 through 11.)
TEST C: Transverse Load Three wall sections with the same fabrication details as Test A and Test B, except the wood I stud perimeter and steel angles were omitted, were constructed for the transverse load test.
- The test specimens were installed into a wooden test fixture as detailed on ATI Drawing 7008 Sheet 2. A 3/8" thick by 1" wide by 52" long steel bar with wooden spacers attached was used to hold the test panel in the test fixture with the ends of the bar held by the brackets shown as item 9 on the referenced drawing. The exterior perimeter of the test i specimen was sealed using polyethylene and tape so as to create an airtight seal. The test fixture was located against a flat lexan test wall and secured in place. A vacuum pump was used to create a positive pressure differential thus, causing a load to be apphed to the exterior side of the test panel. The test specimen rested on a free-floating roller (item 7 on referenced drawing) and was in contact with two fixed cylinders, one top and one bottom (item 6 on referenced drawing). ,
i
h ATI-7008-3 Page 3 of 4 j It
-4 ;
Two dial indicators were used to measure deflection of the test panel and were located at {
the horizontal rnidspan 1/2" from ends. All gauges were set to zero, then loads were 4 applied at 5 psf increments which is equivalent to total load on the specimen of 160 munds.
The indicators were read as soon as each load was reached, five minutes at each 'oad, as .
soon as each load was removed, and again five minutes after each load was removed. He ":
incremental Photo Nos.12 and loading
- 13. w)as continued until failure of the wall section was obser TEST D: Concentrated Load The same three wall sections that were used for the transverse load test were used for the i concentrated load test per the referenced specification. j The test specimens were placed flat on the cement floor beneath the test fixture detailed ,
on ATI Drawing 7008 Sheet 3. One "ENERPAC" RCS 201 hydraulic cylinder was centered ,
above the 1" diameter rod (item 8 on drawing) and ap, plied a load on'the aluminum plate (item 7 on drawing). The aluminum base and cross piece (item 5 and 6 on drawing) held the rod vertical while the load was being applied. A "ENERPAC' P-392 hydraulic hand-pump was connected to the cylinder to apply the load. The hydraulic cylinder had a 1-3/4" stroke and a 4.43 sq. in. effective cylinder area.
Dial calipers were used to measure identification of the panel facing material. A 1000 ,,
mound load was applied to the plate (item 7 on drawing) with the rod (item 8 on drawing) '
ocated on the center of the panel then again with the rod located halfway between the edge and center of the panel. Identification readings were taken, when possible, under load and after the load was removed. (See Photo Nos.14 and 15.)
TEST E: Racking Imad Test Two wood studded wall sections were fabricated in accordance with details on Promat, Inc.
drawing No. AAD-189 and AAD-104, as modified by Architectural Testing, Inc.
i The test specimens as described above were installed into a test fixture as detailed on ATI Drawine /008 Sheet 4. The test panel was fastened to the steel "1" beam (see referenced drawing') via twelve 5/16" diameter by 3-1/2"long machine bolts and washers spaced at 2-1/2" from one end then every 8.7" for the next seven bolts, then 11-3/4",7-3/4", and 14". A "ENERPAC" RC 106 hydraulic cylinder was mounted in a bracket (item 6 on drawing) in such a fashion as to apply loads to the upper left corner of the test panel. The cylinder was attached to a "ENERPAC" P-391 hydraulic hand pump. The hydraulic cylinder had a 6-
~
1/8" stoke and a 2.24 sq. in. effective cylinder area.
Three dial indicators were used to measure deflection and were located per Figure 7 of ASTM E72. The test procedure used was ASTM E564 since the objective was to measure the performance of the com were applied incrementally [nlete see test resultswall system.
for actual All indicators were set to zero th increments section was observed. Indicator readings were observed at each crement m)time and each until failure the load was removed. (See Photo No.16.)
TEST RESULTS: The following pages represent the data collected during the course of testing. De first section summanzes graphically the test results while the second section represents the raw data collected. Photo Nos.17 through 20 depict typical failures of the test panels.
t ATI-7008-3 Page 4 of 4 A copy of this report will be retained by ATI for a period of four years.- This report '
is the exclusive property of the client so named herein and is applicable to the sample tested. Results obtamed are tested values and do not constitute an opinion or endorsement i by this laboratory.
ARCHITECTURAL TESTING,INC. ;
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Project Manager Reviewed by:
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Trarsvers.e Load Data St+et i i Trent Tests ! i AT: t 7X3 IERO 1 (0) 3,138 r IERO 2 t0) 3.066 :
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i ran at Lead 51 0.082 0.111 1 0.097 : 3.220 3.197 4esn e Lea: 5l 0.027 -0.0E1 ; -0.027 : 3.165 3.005 '[ 5 M n a4:er Fem:voi 5l 0.012 0.029 ! 0.021 3.150 3.115
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- Fe t .e tsas 15 . 0.044 0.20s : 0.125 , 3.15: 3.292 l 5 ;r. a+ter Eea. mal 15 ; 0.0:3 0.20B i 0.116 * !. lei 3.244 -f
. ; -, .j F+; r Lced 20 0.21 0.563 : 0.457 : 3. 4M :.347 r
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A11-7008-3 Promat,Inc. Date: 09/19/89 Technician: Bruce W. Croak CONCENTRATED LOAD DATA SHEET ; PANEL NUMBER: SW-D1 o Identincation (in inches) STRONG WEAK LOAD AREA AREA COMMENT 1000 lbs. Under Load 0.120" 0.160" Set 0.015" 0.015" P PANEL NUMHER: SW-D2 identification (in inches) STRONG WEAK , LOAD AREA AREA COMMENT 1000 lbs. Under Imad 0.150" 0.180" Set 0.010" 0.015" PANEL NUMBER: SW-D3 Identification (in inches) STRONG WEAK LOAD AREA AREA COMMENT 1000 lbs. Under Imad 0.130" 0.125" Set 0.010" 0.012" h C . !
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t e f 3 ATI-700S-3 ! Promat, Inc. l Date: 09/19/89 i Technician: Bruce W. Croak i I f CONCENTRATED LOAD DATA SHEET l PANEL NUMHER: SW-D1 ;l Identification (in inches) STRONG WEAK i LOAD AREA AREA COMMENT l l 1000 lbs. Under Load 0.120" 0.160" l i t Set 0.015" 0.015" ; l PANEL NUMRER: SW-D2 C Identification (in inches) STRONG WEAK AREA COMMENT LOAD AREA 1000 lbs. Under Loaa 0.150" 0.180" > i Set 0.010" 0.01("
- r PANEL NUMBER: SW-D3 -
Identification (in inches) 'l STRONG WEAK l LOAD AREA AREA COMMENT .t 1000 lbs. Under Load 0.130" 0.125" ;
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Set 0.010" 0.012" f i 1
Ra: king 1. cad Test Da u S5eet Fromat Tests ATI # 7002 Test Date: i2/6/97 Fanel 8: 5W + 1 num+mumemommum, mums, mum ummummmm i msnm
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teer.t wa: 20 0.00 0.005 0.001 0.0(2 O 003 ; 0. f.25 0.010 1 0.012 l 5 ran af te- Eewal 200 0.0'C 0.005 0.001 0.002 . 0.003 ; 0.025 0.0D 0.018 :
., , , , f hp L:a:: 220 * ;.052 0.%7 0.011 0.Mo i 0.035 0.155 0.220 : 0.135 l 5 P:r et Load 220 0.37 0.0s 0.011 0.05 : 0.036 : 0.155 0.2:0 ; 0.15e -
- e m e L ,ed 22; t . X4 0.005 0.000 0.002 l 0.iYG :- 0.020- 0.015 0.012 !
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i Ccar ess:on toad Data Sheet ; Frcr,at 'ests ; AT: # 7003 i Tes Ste: 11 % e4 Fame! 8: EW-4-2 e 4 , + , . . + . + + + + + + + . . . . . . . . . . . . + . . + + + + + + + + + + . +, e + + + + + , , . . . + + + + e e + , 4 . . . , + + . . + e ; * *
- e e i n e + + , , , + + , + + + + , e e e +, . e 4 dc DEF2 W ':Dh. Snctes! ': Lateral Deflection unthes) ,
' ,w e .a, oau;e b ., m, era e san .sas;e 1 tax e V ..
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~e w e L:ad 20 0.000 0.000 a. Coo 0.000 ; 0.000 : 0.020 0.005 ; 0.013 -} 5 h r. ef:E- 4 D 21 20 I 0. W.i 0. 000 0.0/> 0.000 1 0.000 . 0.020 0.005 0.013 i
; -- ; i iep L:6: 40 J. M 0.011 . . X4 0.001 . u.00o ; 0.090 0.050 1 0.070 !
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4 c a ;:a: 110 0.000 0. 0C 0.005 0. W 0. 00', ; 0.0~5 ).220 0. 029 i h , a*:gr ie n i! :t.0 ' O. OX 0. DCC s.(Ni 0. 004 , 0.003 0.025 'O.020 0.02B Iet:n Lea: :60 ; 0.04s ^ 04
. 0.000 0.0C5 0.0:4 l 0.250 0.150 O.215 -
5 h at L:a: 16; ; r , gh t 043 0,001 c.005 ; d.025 i 0.250 0.100 ; 0.215 t 4 c 4 Lte: 160 .X1 0.004 0.00s 0. 0% , 0. 0'.4 0.040 0.030 O.035 t i 5 *m af e Feisa; 1:0 ; .01 0.0:4 0.00o 0.00A : 0.004 0.040 0.030 ; 0.035 h ;;* _:a: :33 . 0.06; 0. 06: U. M 0.015 0.0~7 ; 0.320 0.270 . 0.295 5 m ai es:' :50 < 0. Det 0.0t2 0.Ti 0.015 : 0.038 : 0.220 0.250 t 0.300 l 4 m e L:e: 18) : 0.000 0.006 DSA 0.008 : 0.0:e . 0. 0'/) 0.040 ; 0.045 5 m a+te- Fe m al 180 1 0.fC 0.00: 0.005 0.002. 0. 416 : 0.050 0.040 ! 0.C45 i
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t I wa,#. Campressim Lcad Data Sheet .l Prcest 'ests } ATI f 7008 t Test Eate: 11/7 27 Farel s: %-4-2 ; . .. . e , + + + . . , + + , , + + , . . . . . . .. + +, , , + + + + + + . + + e + + + + + + + + + + + + + e * , . + + e , * * * * + + e e , + , e ++ ; ++ + + e e e e + + + + ,
- e e + + + e s e e + + , e e e e . .
=;=- : : !
t is;;,L:a: MO 0.C 57 '
,. :6 0.0:e 0.0'8 i C.00 : 0.520 0.450 : 0.485, ;
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; : : l
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- an '3as;e ! Ba;;e 2 Ea.;;e 3 Gau;e 4 : Avera;e : Bau;e 5 Bauge 6 Avera;e ,
h;;r L:at 2 0.006 0.0c6 0.301 0.001 1 0.004 -l 0.070 0.070 : 0.070 i
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j Be;n t:tt 40 : 0.011 0.012 0.001 0.002 0.007 1 0.105 0.110 O.10E l 5 *a. a+ L:a: 40 0.011 0.012 0.001 0.002 : 0.007 l 0.105 0.100 : 0.103 i
- st.e Lee: 40 0.006 o. 5'A 0.000 0.000 : 0.000 1 0.040 0.0:5 . 0.02 l
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I
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! *: it . t: 151 0.099 0.100 0.042 0.000 1 0.06B i 0.730 0.590 . (.660 4 .: e 1:23 150 0.301 0.(04 0.014 0. E 0.005 1 0.120 0.100 : 0.110 f 5 " r efit- ;e sal :2:
O.001 0.0?4 0.013 0. 002 : 0.005 : 0.290 0.260 : 0.27* l I C'Eh *. kr: tate s :erced et* 271 1:s. a;;1:e: 1: tre top :f the pa e1. ( iest a:raratus ) . t t
- 2. Et:r.isne de'le:t:c, at 200 Ea* ;
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+++=4++++...+++++++++++++++.+++++++++4*++..,*++++++++.++e+.e+e.+e++++++++++e... +++++++++++++++++++++++++++++e LC4 DETDWi!]N un:tes) Lateral Defle: tion un:*.es) bse 3a_;e : 3au;e 2 Sa.4e 3 Ba.2;e 4 1.e< age : Sau0e 5 Sauge s ' Average ir., n _:a: '
_: *d. 0. M C.X: 0.001 O.Xu O.010 0.015 k 0.01; 5 r;r at L a 20 : 0 X1 0.0/J: 0.001 0.001 . 0.001 ; 0.010 0.015 0.0 ; Fem L:ad 20 ' O.000 0.00 0.000 0.000 0.000 0.000 0.305 t 0.X: 5 " n a*ter Fee:(al 20 ' O.NC 0.001 0.000 0.000 . 0.000 1 0.005 0.005 O.005
- -- ; i 1 Fe;;*.L:#: 40 : 0.X: 0.001 0.001 0.001 : 0.00: ; 0.015 0.020 : 0.0:E I 5 *19 4t ;:sf O' O.00: 0.X1 0.001 0.001 1 0.0)! i 0.015 0.020 : 0.315 r e":a _:a: O C .XO o.001 0.000 0.000 0. DN O.000 0.005 O.X0 5
- a a'ts- :e r .al O, 0.000 0.00: 0.000 0.0@ 0. M ; 0.000 0.005 : 3. X; l -:- . -]
Bs;;7 L a: O' J.T2 0.302 0.002 0.001 . 0.002 O.020 0.025 . 0.02: c, . y ^C ' ^
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! : at L:a: :20 0. 'C 0. ZC 0. 00; 0.0% 0. X2 0.040 0.055 ; 0 ?'
in:.e ;:n :D 0,M: 0.T: 0.001 0.001 s.00: , 0.010 0.010 cm . . 13 ' C^:
. 0.X: 3.0c: 0. %1 .%1 0.010 5.0:0 .0!0 5 "_._a':e- :e m a:
is;:- ;;a: :O ?. :C 3. %' O.X4 0.001 .-. XC : 0.050 0.0'5 l 0.0o: I l *:r at L a: "E 0. 3C 0. 003 0.004 0.001 0.XC ! 0.050 0.075 : 0.06 l :n:ve L:a:: 10 .N: 0.600 0.001 0.00 a001 i 0.01* 0.030 ! 0. r2 5 *: a *e< fema! d 10 0.4:1 0.0% 0.001 OM01 C. M : 0.015 0.025 - 0.020 M 6 'Q 0.002 r h;;t Las 0. 003 0.0(4 0.00 1 0. 0$* 0.090 O.0'B
! m at ;:a: 15) ' O. 0'1 0.:C 0.0(4 0.0M D.002 .; 0.065 0.00 ; 0.079 k m e 1:2 :' i* 0.00 0. %0 0. G' 1 0.0: 0.001 0.025 0.050 0.03E
! *:n af:2- 'e m a: h0' O.CC 0.0% 0.001 0.001 . 0. E l 0.025 0.050 t 0.0'e i
5em L:a: 130 , 0.002 0.00; 0.0u5 0.00: ; 0.003 - 0.0B0 0.125 : ?.103 5 *:n at Lea: 190 0.002 0.tc L.005 0.X 1 0.MG : 0.0v0 0.120 , 0.10( 4:M L:a: 230 0.001 0.0M 0.001 0.002 0. 74 O.00 0.075 ; 0.055 5 7:n after hec'.a1 120 0.5.C: 0.000 0.001 0.002 : 0.001 : 0.0':5 0.075 l 0.05* t t 5
,w., _ _ _ _ . _ . _ __ _ , --_.r._- - - - - - , ~ . . , . - ~ . . ~ - - , . - - - - -,_,._-n_,-
l PRoMAT INC. ~l g ..m y yW, ah -- b11 age Centri Drr.-e
"**d'"' "^'* '
0 . . Q15) 775-M5 _.m. .. ,. . : u x teteCop,ec a,5, m.*1 January 2, 1990 " NG255 3975 Page 1 of 3 ; l r SR89-020-3 ASTM E-72 LOAD TESTING OF 2 HR. SOLID WALL ASSEMBLY l 1.0 Purpose The purpose of this testing is to determine if Promat-H , boards assembled in a solid wall assembly will provide ! load carrying capabilities in accordance with ASTM E72-80 ;
" Standard Methods of Conducting Strength Tests of Panels for Building Construction." 1 2.0 Scope !
This procedure establishes the systems to be tested, preparation of the sample and method of testing. i 3.0 References i i 3.1 ASTM Standard E72-80 4.0 Definitions j f 4.1 None 5.0 Responsibility 5.1 The technical services department shall be responsible ! for determining the test objectives, preparation of the test- i specimen, coordinating test performance with the testing > organization and verifying that the testing organization is : knowledgeable and capable of performing and documenting the ! test results. , 5.2 The third party testing organization shall be responsible for the test methods used to satisfy the test l objectives, performance of quality assurance, performance of l appropriate tests, documentation of the results and the l issuance of an appropriate report. , 6.0 Testing
]
6.1 Data to be acquired
- a. Duration, . magnitude and direction of incremental load applied to the wall assembly a
. ~ . - -
PROM AT INC. g.- ,; , , , M Valage Center Dme Reading PA1%07 88i# i . -y e . T _ W5i 775-7775 Toie cop,en ms,7771341 January 2, 1990 NKL255-W5 Page 2 of 3 l
- b. Deformation of the panel assembly during application ;
of the load. , i
- c. Deformation (or set) of the panel assembly after removal of the load. ;
i
- d. Ultimate load and cause of failure at panel assembly destruction. ;
6.2 Materials *
- a. 1" (25mm) Promat-H calcium silicate boards as manufactured by Promat Inc. ;
- b. 3/4" (20mm) Promat-H calcium silicate boards as manufactured by Promat Inc.
- c. 8 x 1 5/8" self-drilling phillips bugle head Hi-Lo screw fastener,
- d. 7/16" x 1 1/2" x 16 Ga staples as manufactured by Senco Fastening Systems, part N17. j
- e. 7/16" x 2" x 16 Ga. staples as manufactured by Senco Fastening Systems, part N21. ;
1 1 /2" x 22 Ga galvanized steel angle.
- f. I /2" x1 6.3 Testing :
- a. The wall assembly shall be constructed in accordance ,
with Promat drawings AAD-104 thru luD-107, AAD-186 and AAD-189 (attached to this document). [
- b. The 1 1 /2" x1 1 /2" angles shall be attached to the perimeter of the masonry frame supplied by the testing .i organization utilizing the supplied fasteners. I
- c. The first layer of Promat-H (20 mm) shall be applied to the angles utilizing a 8 xboarg/8" 1 self- ,
drilling phillips bugle head Hi-Lo screw fastener spaced 12" on center (see drawing AAD-104, 186 & 189 ). i e
- d. The second layer of Promat-H (25 rm) board shall be ,
applied to the first layer with a vertical joint : staggered 24". The boards shall be fastened to the i first layer utilizing 7/16" x1 1 /2" x 16 Ga. staples ' on 12" horizontal spacing and 6" vertical spacing (see ; drawing AAD-105, 186 & 189). , i
'I aga53gygg PROM AT INC. j g r- . 7 Vil!,ge Center Drne g
S Readmg, P A 1%07 m. E f - ins > 775-ms
.un ,. = Tete cop.er: ,nsi m-w1 January 2, 1990 me :ss-ws Page 3 of 3 i
- e. The third layer of Promat-H (20 mm) board shall be applied to the second layer with the vertical joints staggered 24". The ds shall be fastened to the second layer utilizing boay/16" x 2" x 16 Ga. staples on i 12" horizontal spacing and 6" vertical spacing (see [
drawing AAD-106, 186 & 189). ,
- f. Testing shall be conducted in accordance with ASTM E72-80 including Compressive Load, Tensile Load, f Transverse Load - Specimen Vertical, Impact Load and Racking Load (per ASTM E564-84). ;
6.4 Final Report
?
^
- a. The testing organization shall prepare a report outlining test performance and results thereof as soon !
as possible. j r I 9 l t I f i
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-- 8x 15/8'self drillitig screwfasterior
. . . . . . . N '
g!h!!!ggigou) e jlib . g- 20 mm Promat-H
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20mm Promat H PROMAT, ING VILLAGE CENTER DRIVE READING, PA 19607 4' - v 4* - e __ . 2-" PROJECT: SR88 - 032
._______...___o_.__. to .
DRAWN:11/28/88 BY:DAVIDHAINES
"^*'"""
1st LAYER OF PROMAT-H SOLIDWALL
^^ ~'"*
2 Hr. ASSEMBLY
1 / - 7/16' x 1 1/2* x 1 G Ga. staples, typical all boards
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--- RSDING, PA 19607 2' - 0* 4' - 0* l 4' . o-
--+ PROJECT: SR88-032 to O DRAWN:11/29/88 BY: DAVID HAINES 2 nd LAYER OF PROMAT-H SOLIDWALL l'" "
330~ios 2 nd LAYER - 2 Hr.
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JOINT STAGGER LOCATIONS PROMAT, INC VILLAGE CENTER DRIVE NOTE: All boards will bo nomina! 4* x 10' - Field cut to test framo READING, PA 19607 PROJECT: SR88-032 DRAWN:11/29/88 . BY: DAVID HAINES. -
""^*'""*
SOLID WALL- 2 HR
^^ ' ' # ~
JOINT LOCATIONS t
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; STAPLES
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PROJECT: SR89-020 9' s- .i ' s' ? _ s c. s ., DRAWN: 10-5-89 BY:DAVIDIIAINES
"^*'"""
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,. , . -. ,. , ASTM- L772
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SOLID WALL
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! ?'*- Transverse load test apparatus i and set-up
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PilOTO 13 Transverse load test apparatus { r. ..
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- PIIOTO 20 Test wall breaks in half at ultimate 2
load during transverse load test i r. a l r a s ) I l i i
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