<?xml version="1.0" encoding="windows-1252"?><SEC xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:noNamespaceSchemaLocation="http://si.ksc.nasa.gov/sidownloads/xml/specsintactSEC.xsd"><MTA NAME="SUBFORMAT" CONTENT="NEW"/><HDR><AST/><BRK/>
USACE / NAVFAC / AFCESA / NASA      UFGS-35 59 13.19 (April 2006)<BRK/>
                                    ------------------------------<BRK/>
Preparing Activity: <PRA>NAVFAC</PRA>          Replacing without change<BRK/>
                                    UFGS-02397 (May 2003)<BRK/>
<BRK/>
<HL4>UNIFIED FACILITIES GUIDE SPECIFICATIONS</HL4><BRK/>
<BRK/>
<HL4>References are in agreement with UMRL dated January 2009</HL4><BRK/>
<AST/><BRK/></HDR>
<BRK/>
<SCN>SECTION 35 59 13.19</SCN><BRK/>
<BRK/>
<STL>ARCH-TYPE RUBBER MARINE FENDERS</STL><BRK/>
<DTE>04/06</DTE><BRK/>
<NTE><BRK/>
<AST/><BRK/>
<NPR>NOTE:  This guide specification covers the requirements for <SCP>arch-type rubber 
marine fenders</SCP>.<BRK/>
<BRK/>
Edit this guide specification for project specific requirements by adding, deleting, 
or revising text.  For bracketed items, choose applicable items(s) or insert 
appropriate information.<BRK/>
<BRK/>
Remove information and requirements not required in respective project, whether 
or not brackets are present.<BRK/>
<BRK/>
Comments and suggestions on this guide specification are welcome and should 
be directed to the technical proponent of the specification.  A listing of <URL HREF="http://65.204.17.188/report/ufgs.html">technical 
proponents</URL>, including their organization designation and telephone number, is 
on the Internet.<BRK/>
<BRK/>
Recommended changes to a UFGS should be submitted as a  <URL HREF="http://65.204.17.188/projnet/cms/public.html">Criteria Change Request 
(CCR)</URL>.</NPR><BRK/>
<AST/><BRK/></NTE>
<NTE><BRK/>
<AST/><BRK/>
<NPR>NOTE:  On the project drawings, show location of fenders and size and spacing 
of fasteners.</NPR><BRK/>
<AST/><BRK/></NTE>
<BRK/>
<PRT><TTL>PART 1   GENERAL</TTL><BRK/>
<BRK/>
<SPT><TTL>1.1   REFERENCES</TTL><BRK/>
<NTE><BRK/>
<AST/><BRK/>
<NPR>NOTE:  This paragraph is used to list the publications cited in the text of 
the guide specification. The publications are referred to in the text by basic 
designation only and listed in this paragraph by organization, designation, 
date, and title.<BRK/>
 <BRK/>
Use the Reference Wizard's Check Reference feature when you add a RID outside 
of the Section's Reference Article to automatically place the reference in the 
Reference Article.  Also use the Reference Wizard's Check Reference feature 
to update the issue dates.<BRK/>
 <BRK/>
References not used in the text will automatically be deleted from this section 
of the project specification when you choose to reconcile references in the 
publish print process.</NPR><BRK/>
<AST/><BRK/></NTE>
<BRK/>
<TXT>The publications listed below form a part of this specification to the extent referenced.  The publications are 
referred to within the text by the basic designation only.</TXT><BRK/>
<BRK/>
<REF><ORG>ASME INTERNATIONAL (ASME)</ORG><BRK/><BRK/><RID>ASME B18.22.1</RID><RTL>(1965; R 2008) Plain Washers</RTL><BRK/><BRK/><RID>ASME B18.22M</RID><RTL>(1981; R 2005) Metric Plain Washers</RTL><BRK/><BRK/></REF><REF><ORG>ASTM INTERNATIONAL (ASTM)</ORG><BRK/><BRK/><RID>ASTM A 479/A 479M</RID><RTL>(2008) Standard Specification for Stainless Steel Bars and Shapes for Use in Boilers and Other Pressure Vessels</RTL><BRK/><BRK/><RID>ASTM D 1171</RID><RTL>(1999; R 2007) Rubber Deterioration - Surface Ozone Cracking Outdoors or Chamber (Triangular Specimens)</RTL><BRK/><BRK/><RID>ASTM D 2000</RID><RTL>(2008) Standard Classification System for Rubber Products in Automotive Applications</RTL><BRK/><BRK/><RID>ASTM D 395</RID><RTL>(2003; R 2008) Standard Test Methods for Rubber Property - Compression Set</RTL><BRK/><BRK/><RID>ASTM D 412</RID><RTL>(2006ae1e2) Standard Test Methods for Vulcanized Rubber and Thermoplastic Elastomers - Tension</RTL><BRK/><BRK/><RID>ASTM D 471</RID><RTL>(2006; R 2008) Standard Test Method for Rubber Property - Effect of Liquids</RTL><BRK/><BRK/><RID>ASTM D 573</RID><RTL>(2004) Standard Test Method for Rubber - Deterioration in an Air Oven</RTL><BRK/><BRK/><RID>ASTM D 575</RID><RTL>(1991; R 2007) Rubber Properties in Compression</RTL><BRK/><BRK/><RID>ASTM D 624</RID><RTL>(2000; R 2007) Tear Strength of Conventional Vulcanized Rubber and Thermoplastic Elastomers</RTL><BRK/><BRK/><RID>ASTM D 746</RID><RTL>(2007) Standard Test Method for Brittleness Temperature of Plastics and Elastomers by Impact</RTL><BRK/><BRK/><RID>ASTM F 593</RID><RTL>(2002; R 2008) Stainless Steel Bolts, Hex Cap Screws, and Studs</RTL><BRK/><BRK/><RID>ASTM F 594</RID><RTL>(2008) Standard Specification for Stainless Steel Nuts</RTL><BRK/><BRK/></REF><REF><ORG>U.S. DEPARTMENT OF DEFENSE (DOD)</ORG><BRK/><BRK/><RID>MIL-PRF-907</RID><RTL>(Rev F) Antiseize Thread Compound, High Temperature</RTL><BRK/><BRK/></REF></SPT><SPT><TTL>1.2   SUBMITTALS</TTL><BRK/>
<NTE><BRK/>
<AST/><BRK/>
<NPR>NOTE:  Review submittal description (SD) definitions in Section 01 33 00 SUBMITTAL 
PROCEDURES and edit the following list to reflect only the submittals required 
for the project.  Submittals should be kept to the minimum required for adequate 
quality control.<BRK/>
<BRK/>
A “G” following a submittal item indicates that the submittal requires Government 
approval.  Some submittals are already marked with a “G”.  Only delete an existing 
“G” if the submittal item is not complex and can be reviewed through the Contractor’s 
Quality Control system.  Only add a “G” if the submittal is sufficiently important 
or complex in context of the project.<BRK/>
<BRK/>
For submittals requiring Government approval on Army projects, a code of up 
to three characters within the submittal tags may be used following the "G" 
designation to indicate the approving authority.  Codes for Army projects using 
the Resident Management System (RMS) are:  "AE" for Architect-Engineer; "DO" 
for District Office (Engineering Division or other organization in the District 
Office); "AO" for Area Office; "RO" for Resident Office; and "PO" for Project 
Office.  Codes following the "G" typically are not used for Navy,  Air Force, 
and NASA projects.<BRK/>
<BRK/>
Choose the first bracketed item for Navy, Air Force and NASA projects, or choose 
the second bracketed item for Army projects.</NPR><BRK/>
<AST/><BRK/></NTE>
<BRK/>
<TXT>Government approval is required for submittals with a "G" designation; submittals not having a "G" designation 
are [for Contractor Quality Control approval.][for information only.  When used, a designation following the 
"G" designation identifies the office that will review the submittal for the Government.]  The following shall 
be submitted in accordance with Section <SRF>01 33 00</SRF> SUBMITTAL PROCEDURES:</TXT><BRK/>
<BRK/>
<LST><SUB>SD-03 Product Data</SUB></LST><BRK/>
<BRK/>
<ITM><SUB>Fender</SUB></ITM><BRK/>
<BRK/>
<ITM><SUB>Hardware</SUB></ITM><BRK/>
<BRK/>
<LST><SUB>SD-05 Design Data</SUB></LST><BRK/>
<BRK/>
<ITM>Reaction--energy--percent compression <SUB>curve</SUB></ITM><BRK/>
<BRK/>
<ITM><SUB>Dimension</SUB></ITM><BRK/>
<BRK/>
<ITM><SUB>Fender</SUB> material specifications</ITM><BRK/>
<BRK/>
<ITM><SUB>Design</SUB> calculations</ITM><BRK/>
<BRK/>
<LST><SUB>SD-06 Test Reports</SUB></LST><BRK/>
<BRK/>
<ITM><SUB>Minimum Tensile Strength</SUB></ITM><BRK/>
<BRK/>
<ITM><SUB>Shore Hardness (Durometer)</SUB></ITM><BRK/>
<BRK/>
<ITM><SUB>Modulus at 400 Percent Elongation</SUB></ITM><BRK/>
<BRK/>
<ITM><SUB>Maximum Compression Set</SUB></ITM><BRK/>
<BRK/>
<ITM><SUB>Tear Resistance</SUB></ITM><BRK/>
<BRK/>
<ITM><SUB>Minimum Elongation</SUB></ITM><BRK/>
<BRK/>
<ITM><SUB>Ozone Resistance</SUB></ITM><BRK/>
<BRK/>
<ITM><SUB>Low Temperature Impact Resistance</SUB></ITM><BRK/>
<BRK/>
<ITM><SUB>Water Absorption</SUB></ITM><BRK/>
<BRK/>
<ITM><SUB>Heat Resistance</SUB></ITM><BRK/>
<BRK/>
<ITM><SUB>Compression Deflection Resistance</SUB></ITM><BRK/>
<BRK/>
<ITM><SUB>Fender Compression Test</SUB></ITM><BRK/>
<BRK/>
<ITM><SUB>Angular Fender Compression Test</SUB></ITM><BRK/>
<BRK/>
<ITM>  Tests shall have been performed on the specified fender within 5 years of submittal of the 
reports for approval.  Test reports shall be accompanied by notarized certificates from the 
manufacturer certifying that the tested material is of the same type, quality, manufacture and 
make as that proposed to be supplied.</ITM><BRK/>
<BRK/>
<LST><SUB>SD-08 Manufacturer's Instructions</SUB></LST><BRK/>
<BRK/>
<ITM><SUB>Installation</SUB> Instructions</ITM><BRK/>
<BRK/></SPT>
<SPT><TTL>1.3   DELIVERY HANDLING AND STORAGE</TTL><BRK/>
<BRK/>
<TXT>Fenders shall be undamaged when delivered and shall be handled and stored so as to prevent damage, such as bending 
or abrading end fittings, cutting of rubber, or damage to coating of hardware.  Protect fenders from exposure 
to damaging liquids, oils, greases and extended exposure to sunlight.</TXT><BRK/>
<BRK/></SPT>
</PRT><PRT><TTL>PART 2   PRODUCTS</TTL><BRK/>
<BRK/>
<SPT><TTL>2.1   CONFIGURATION</TTL><BRK/>
<NTE><BRK/>
<AST/><BRK/>
<NPR>NOTE:  Coordinate angle with angular compression test requirements.</NPR><BRK/>
<AST/><BRK/></NTE>
<BRK/>
<TXT><SUB>Fender</SUB> shall be extruded and shall be continuous in the length indicated.  The fenders shall have a truncated 
"A" cross section shape and be attached to the structure at the base, the widest <SUB>dimension</SUB>, of the arch.  The 
connecting hardware shall be fully exposed.  No encased hardware or molded fenders shall be allowed.  The fender 
and hardware shall be designed and factory tested to the loads per linear<MET> meter</MET><ENG> foot</ENG> of fender specified in paragraph 
entitled "PERFORMANCE," for angles of approach of<MET> 0 and 0.26 rad</MET><ENG> 0 and 15 degrees</ENG>.  Fender anchor bolts and method 
of anchorage shall be of the size and spacing required by the manufacturer's <SUB>design</SUB> and testing; however, the 
size and spacing of anchor bolts indicated on the drawings shall be construed to be the minimum required, unless 
exceeded by the requirements of the fender manufacturer's design.</TXT><BRK/>
<BRK/></SPT>
<SPT><TTL>2.2   ELASTOMER</TTL><BRK/>
<BRK/>
<TXT>The elastomer shall be the ethylene propylene dimonomer (EPDM), as specified in <RID>ASTM D 2000</RID>, with the following 
properties:</TXT><BRK/>
<NTE><BRK/>
<AST/><BRK/>
<NPR>NOTE:  Coordinate values with calculated design requirements.</NPR><BRK/>
<AST/><BRK/></NTE>
<BRK/>
<MET><TBL><THD><BRK/>
<HL4><HL1>ELASTOMER PROPERTY REQUIREMENTS</HL1></HL4><BRK/></THD>
<BRK/>
         <SUB>Minimum Tensile Strength</SUB>                [14 MPa] [_____]<BRK/>
         (<RID>ASTM D 412</RID>)<BRK/>
<BRK/>
         <SUB>Shore Hardness (Durometer)</SUB>              [70 <HL1>+</HL1> 5] [_____]<BRK/>
         (<RID>ASTM D 412</RID>)<BRK/>
<BRK/>
         <SUB>Modulus at 400 Percent Elongation</SUB>       [6.2 MPa]  [_____]<BRK/>
         (<RID>ASTM D 412</RID>)<BRK/>
<BRK/>
         <SUB>Maximum Compression Set</SUB>                 [25] [_____] Percent<BRK/>
         (<RID>ASTM D 395</RID> Method B,<BRK/>
         Maximum Percent 22 Hr. at 70 Degrees C<BRK/>
<BRK/>
         <SUB>Tear Resistance</SUB>                         [300] [_____] lb/in.<BRK/>
         (<RID>ASTM D 624</RID>; DIE B Min. 150 lb/in)<BRK/>
<BRK/>
         <SUB>Minimum Elongation</SUB>                      [500] [_____] Percent<BRK/>
         (<RID>ASTM D 412</RID>)<BRK/>
<BRK/>
         <SUB>Ozone Resistance</SUB>                        [80] [_____] H <HL1>+</HL1><BRK/>
         (<RID>ASTM D 1171</RID> Exposure Method B;<BRK/>
         70h Bent Loop at 38 Degrees C; 50pphm)<BRK/>
<BRK/>
         <SUB>Low Temperature Impact Resistance</SUB>       [0] [_____] Degrees C<BRK/>
         (<RID>ASTM D 746</RID> Procedure B;<BRK/>
         Non-Brittle at -55 Degrees C)<BRK/>
<BRK/>
         <SUB>Water Absorption</SUB>                        [10.0] [_____] Percent<BRK/>
         (<RID>ASTM D 471</RID> Method B;<BRK/>
         70h at 100 Degrees C.;<BRK/>
         Volume Change <HL1>+</HL1>5 Percent<BRK/>
<BRK/>
         <SUB>Heat Resistance</SUB>                         Shall exceed<BRK/>
         (<RID>ASTM D 573</RID>; 70h at 100 Degrees C        requirements<BRK/>
         Ch Tensile, Elong. -25 Percent,<BRK/>
         Hardness +10<BRK/>
<BRK/>
         <SUB>Compression Deflection Resistance</SUB>       Shall exceed<BRK/>
         (<RID>ASTM D 575</RID> Method B;                   requirements<BRK/>
         3 S Dwell at 23 Degrees C<BRK/></TBL>
</MET><ENG><TBL><THD><BRK/>
<HL4><HL1>ELASTOMER PROPERTY REQUIREMENTS</HL1></HL4><BRK/></THD>
<BRK/>
         <SUB>Minimum Tensile Strength</SUB>                [2000 psi] [_____]<BRK/>
         (<RID>ASTM D 412</RID>)<BRK/>
<BRK/>
         <SUB>Shore Hardness (Durometer)</SUB>              [70 <HL1>+</HL1> 5] [_____]<BRK/>
         (<RID>ASTM D 412</RID>)<BRK/>
<BRK/>
         <SUB>Modulus at 400 Percent Elongation</SUB>       [900 psi] [_____]<BRK/>
         (<RID>ASTM D 412</RID>)<BRK/>
<BRK/>
         <SUB>Maximum Compression Set</SUB>                 [25] [_____] Percent<BRK/>
         (<RID>ASTM D 395</RID> Method B,<BRK/>
         Maximum Percent 22 Hr. at 158 Degrees F<BRK/>
<BRK/>
         <SUB>Tear Resistance</SUB>                         [300] [_____] lb/in.<BRK/>
         (<RID>ASTM D 624</RID>; DIE B Min. 150 lb/in)<BRK/>
<BRK/>
         <SUB>Minimum Elongation</SUB>                      [500] [_____] Percent<BRK/>
         (<RID>ASTM D 412</RID>)<BRK/>
<BRK/>
         <SUB>Ozone Resistance</SUB>                        [80] [_____] H <HL1>+</HL1><BRK/>
         (<RID>ASTM D 1171</RID> Exposure Method B;<BRK/>
         70h Bent Loop at 100 Degrees F; 50pphm)<BRK/>
<BRK/>
         <SUB>Low Temperature Impact Resistance</SUB>       [-40] [_____] Degrees F<BRK/>
         (<RID>ASTM D 746</RID> Procedure B;<BRK/>
         Non-Brittle at -67 Degrees F)<BRK/>
<BRK/>
         <SUB>Water Absorption</SUB>                        [10.0] [_____] Percent<BRK/>
         (<RID>ASTM D 471</RID> Method B;<BRK/>
         70h at 212 Degrees F.;<BRK/>
         Volume Change <HL1>+</HL1>5 Percent<BRK/>
<BRK/>
         <SUB>Heat Resistance</SUB>                         Shall exceed<BRK/>
         (<RID>ASTM D 573</RID>; 70h at 212 Degrees F        requirements<BRK/>
         Ch Tensile, Elong. -25 Percent,<BRK/>
         Hardness +10<BRK/>
<BRK/>
         <SUB>Compression Deflection Resistance</SUB>       Shall exceed<BRK/>
         (<RID>ASTM D 575</RID> Method B;                   requirements<BRK/>
         3 S Dwell at 73 Degrees F<BRK/></TBL>
</ENG><BRK/></SPT>
<SPT><TTL>2.3   <SUB>HARDWARE</SUB></TTL><BRK/>
<BRK/>
<SPT><TTL>2.3.1   Plates and Angles</TTL><BRK/>
<BRK/>
<TXT><RID>ASTM A 479/A 479M</RID>, Type 316L stainless steel for plates, angles, and miscellaneous hardware required to attach 
the fenders to the structure.</TXT><BRK/>
<BRK/></SPT>
<SPT><TTL>2.3.2   Nuts, Bolts, and Washers</TTL><BRK/>
<BRK/>
<TXT><RID>ASTM F 593</RID> or <RID>ASTM F 594</RID>, Group 2 (316 alloy) stainless steel for nuts and bolts. <MET> <RID>ASME B18.22M</RID></MET><ENG> <RID>ASME B18.22.1</RID></ENG>
 for washers, except fabricate washers of 316 alloy stainless steel.</TXT><BRK/>
<BRK/></SPT>
<SPT><TTL>2.3.3   Antiseize Compound</TTL><BRK/>
<BRK/>
<TXT><RID>MIL-PRF-907</RID>.</TXT><BRK/>
<BRK/></SPT>
</SPT><SPT><TTL>2.4   PERFORMANCE</TTL><BRK/>
<NTE><BRK/>
<AST/><BRK/>
<NPR>NOTE:  Coordinate values with calculated design requirements.</NPR><BRK/>
<AST/><BRK/></NTE>
<BRK/>
<TXT>When vertically compressed by a plate extending the full length and width of a<MET> 0.30 m</MET><ENG> one foot</ENG> section of the 
fender, the fender shll ab sorb <MET>[8950] [_____] joules</MET><ENG> [6,600] [_____] foot pounds</ENG> of energy <HL1>+</HL1>10 percent when 
[48] [_____] percent compressed (i.e., to a dimension of [52] [_____] percent of its original height) with a 
corresponding load of not more than<MET> [85,402] [_____] N</MET><ENG> [19,200] [_____] pounds</ENG> <HL1>+</HL1>10 percent.</TXT><BRK/>
<BRK/>
<SPT><TTL>2.4.1   <SUB>FENDER COMPRESSION TEST</SUB></TTL><BRK/>
<NTE><BRK/>
<AST/><BRK/>
<NPR>NOTE:  Coordinate values with calculated design requirements.</NPR><BRK/>
<AST/><BRK/></NTE>
<BRK/>
<TXT>Compress fender along its longitudinal axis between two parallel flat plate surfaces to a compressed dimension 
of [48] [_____] percent of its original height.  Record load and the corresponding deflection at<MET> 6 mm</MET><ENG> 1/4 inch</ENG>
 increments and plot as a graph of load versus deflection.  The Load-Deflection <SUB>curve</SUB> shall then be integrated 
to generate an Energy-Deflection curve for the fender.  After compression of the fender to [48] [_____] percent 
of its original height, the fender shall be rebound to 98 percent of its original height within [ten] [_____] 
minutes after the load is removed.</TXT><BRK/>
<BRK/></SPT>
<SPT><TTL>2.4.2   <SUB>ANGULAR FENDER COMPRESSION TEST</SUB></TTL><BRK/>
<NTE><BRK/>
<AST/><BRK/>
<NPR>NOTE:  Coordinate values with calculated design requirements.</NPR><BRK/>
<AST/><BRK/></NTE>
<BRK/>
<TXT>Compress fender along its longitudinal axis between two flat plate surfaces, at an angle of<MET> [0.26] [_____] rad</MET><ENG>
 [15] [_____] degrees</ENG> to each other, to a compressed dimension of [48] [_____] percent of its original height.  
Record load and the corresponding deflection at<MET> 6 mm</MET><ENG> 1/4 inch</ENG> increments and plot as a graph of load versus deflection.  
The Load-Deflection curve shall then be integrated to generate an Energy-Deflection curve for the fender.  After 
compression of the fender to [48] [_____] percent of its original height, the fender shall rebound to 98 percent 
of its original height within [10] [_____] minutes after the load is removed.</TXT><BRK/>
<BRK/></SPT>
</SPT></PRT><PRT><TTL>PART 3   EXECUTION</TTL><BRK/>
<BRK/>
<SPT><TTL>3.1   <SUB>INSTALLATION</SUB></TTL><BRK/>
<BRK/>
<TXT>Install fenders with the fender longitudinal axis vertical.  Install the fenders in the position and at the spacing 
indicated on the drawings.</TXT><BRK/>
<BRK/>
<SPT><TTL>3.1.1   Antiseize Compound</TTL><BRK/>
<BRK/>
<TXT>Coat threads of bolts prior to applying washers and nuts.  Recoat bolt thread projection beyond nut after tightening.</TXT><BRK/>
<BRK/></SPT>
</SPT></PRT>    <END/><BRK/></SEC>