FRP - ATTACHMENT A - FRP MAT ASSEMBLY SPECS 29 JAN 21.pdf

ATTACHMENT A - FRP MAT ASSEMBLY SPECIFICATIONS

(29 January 2021)

This specification is approved for use by all Departments and Agencies of the Department of Defense within the distribution limitations noted at the bottom of the page.

A1. BACKGROUND.

A1.1. Scope. This specification describes the requirements for manufacturing the bolt- together fiber-reinforced polymer (FRP) panels made of layers of glass fiber and aramid fabric impregnated with polyester resin and connected using metal bushings. The FRP mats function as expedient foreign object debris (FOD) covers for crushed- stone or debris backfill crater repairs as part the airfield damage repair (ADR) program.

A1.2. Classification. The FRP panels shall be of the following types as specified (see A7.2.).

• Full-Size Panel

• Half-Size Panel

• Full-Size Anchor Panel

• Half-Size Anchor Panel

• Lower Joining Bushing

• Upper Joining Bushing

• Anchor Bushing

A1.2.1. Mat Assembly Definition. A typical FRP mat assembly capable of covering one 50-ft diameter repair (or multiple smaller repairs) is defined as having the components listed in Table 1. The lower joining bushings (A3.7.2.) shall be adhered (A3.3.2.5.) to the holes in the underlap edges of full-size panels and half-size panels prior to delivery.

A1.2.2. Mat Assembly Components. One (1) FRP mat assembly has four (4) FRP mat sets.

A1.2.3. Quantities of Components.

Table 1. Typical FRP Mat Set Component Quantities Component Quantity Full-size panel 7 Half-size panel 6

Full-size anchor panel 3 Half-size anchor panel 4 Lower joining bushing 1522 Upper joining bushing 175 Anchor bushing 125 1 If requested by Government, First Article testing will require one (1) half-size panel for destructive testing in addition to the quantities defined in the acquisition document.

2 Lower bushings shall be attached at each hole in the underlap region(s) of full-size and half-size panels.

Additional bushings should be accounted for in panels which will be required as part of the First Article testing protocol.

A2. APPLICABLE DOCUMENTS.

A2.1. General. The documents listed in this section are specified in sections A3, A4, and/or A6 of this standard. This section does not include documents cited in other sections of this standard or recommended for additional

A-1 information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specified requirements of documents cited in sections A3, A4, and/or A6 of this standard, whether or not they are listed.

A2.2. Documents, Publications, Standards, and Handbooks. The following specifications, standards, and handbooks form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those listed in the issue of the Department of Defense Index of Specifications and Standards (DoDISS) and supplement thereto, cited in the solicitation (see A7.2.).

A2.2.1 Department of Defense Specifications.

MIL-M-43248C Mats, Reinforcing, Glass Fiber

A2.2.2 Department of Defense Standards.

• MIL-STD-129R Military Marking for Shipment and Storage

• MIL-STD-1916 DoD Preferred Methods for Acceptance of Product

(Unless otherwise indicated, copies of the above specifications, standards, and handbooks are available from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094)

A2.2.3 ASTM International

• ASTM D123-13a Standard Terminology Relating to Textiles

• ASTM D696 Standard Test Method for Coefficient of Linear

ThermalExpansion of Plastics between -30°C and 30°C with a Vitreous Silica Dilatometer

• ASTM D790 Standard Test Methods for Flexural Properties of Unreinforced and Reinforced Plastics and Electrical Insulating Materials

• ASTM C881/M Standard Specification for Epoxy-Resin-BaseBonding Systems for Concrete

• ASTM D1929-96 Standard Test Method for Determining Ignition Temperature of Plastics

• ASTM D2565 Standard Practice for Xenon-Arc Exposure of Plastics Intended for Outdoor Applications

• ASTM D2583 Standard Test Method for Indentation Hardness of Rigid Plastics by Means of a Barcol Impressor

• ASTM D3039/M Standard Test Methods for Tensile Properties for Polymer Matrix Composite Materials

• ASTM D3953-15 Standard Specification for Strapping, Flat Steel and Seals

• ASTM D4389 Standard Specification for Finished Glass Fabrics Woven from Rovings

(Application for copies should be addressed to ASTM International, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959 or obtained at www.astm.org .)

A2.2.4 SAE Aerospace Material Specifications.

SAE-AMS-QQ-P-416 Plating, Cadmium (Electrodeposited) (Application for copies should be addressed to the SAE World Headquarters, 400 Commonwealth Drive, Warrendale, PA 15096-0001 or obtained at www.sae.org .)

A2.2.5 Field Manuals.

FM 55-9 APPENDIX D 463L Cargo System

A-2 http://www.astm.org/ http://www.sae.org/

A2.2.6 Technical Manuals.

TO 35D33-2-2-2 463L Air Cargo Pallets HCU-6/E

A2.3. Order of Precedence. In the event of a conflict between the text of this document and the references cited herein (except for related associated specifications or specification sheets), the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.

A3. FRP MAT PANEL COMPONENTS REQUIREMENTS.

A3.1. First Article. When specified (see A7.2.), a sample shall be subjected to first article inspection in accordance with A4.2.1.

A3.2. Mat Description. Four (4) types of FRP panels, full-size, half-size, full-anchor, and half- anchor are described in this specification. Three (3) types of bushings, upper joining, lower joining, and anchor, required to assemble the panels to form a FOD cover, are also described. Installation tools and anchoring systems required for FRP installation will be detailed separately.

A3.3. Materials. Materials shall be as specified herein and in applicable specifications and standards, and other reference documents. Materials not specified shall be selected by the contractor and shall be subject to all provisions of this specification. Materials shall be free of defects which adversely affect performance of serviceability of the finished product. Certification that the herein specified materials meet the requirements of this specification shall be made available to the government at any time upon request.

A3.3.1. FRP Material. The FRP mat panels shall be fabricated from fiberglass, polyester resin, and high strength aramid fabric using a closed molding process (i.e., Resin Transfer Molding (RTM) or Vacuum Resin Transfer Molding (VRTM)). The FRP mat panels shall be fabricated as shown in the Drawings 142003 – 142011 on pages A-17 thru A-26. Full-size and half-size panel edges shall be reinforced with one ply of high-strength aramid fabric with a minimum width of 14-in; anchor panels shall be reinforced with one continuous 24-in wide layer of high-strength aramid fabric. All FRP mat panels shall include UV inhibitors to minimize degradation during outdoor use.

A3.3.1.1. Polyester Resin. The FRP panels shall be fabricated using a polyester resin. The resin shall be polyester, thermosetting, RTM laminating type. A catalyst should be used to achieve appropriate gel times. The resin and catalyst composition shall be designated by a code number. The code number may include a trade name, if desired.

Any changes in the resin components or manufacturing process shall necessitate use of a different code number. The cured resin shall not be corrosive to metals. When used in conjunction with the fiberglass reinforcement specified in (A3.3.1.2.) and tested as per Section A4.5., the resin shall produce a laminate with the required physical properties listed in Table 3. Furthermore, the resin and catalyst combination in conjunction with the fiberglass reinforcement (A3.3.1.2.) shall produce a laminate which retains a minimum of 90 percent of the required flexural strength and tensile strength (Table 3) after being exposed to artificial ultra violet (UV) light for 720 hours, as per ASTM 2565 Table 1, Cycle Number 2 and tested as outlined in Section A4.5. of this specification.

A3.3.1.2. Fiberglass Reinforcement. The fiberglass reinforcement shall produce a laminate with the required physical properties listed in Table 3.

A3.3.1.2.1. Fiberglass Type. The fiberglass reinforcement used for the mat panels shall be a fiberglass fabric mat reinforcement composite Type V, consisting of a multi-axial woven, stitched, or knitted roving that may be stitched or bonded to a Type III, Class I, Grade A chopped strand backing per MIL-M-43248C. Definitions of the textile terms used herein are described in ASTM D123. All fiberglass used in the roving, continuous strand, and chopped fiber mat portions of the reinforcement shall be E-type (MIL-M-43248C). The glass shall be white in color.

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A3.3.1.2.2. Roving. The roving material shall be constructed by weaving, stitching, or knitting individual rovings in multi-axial (2 or more) directions.

A3.3.1.2.3. Chopped Strand Mat. The chopped strand mat shall consist of randomly oriented strands. The strands shall be treated with a silane sizing compatible with the polyester resin in accordance with ASTM D4389 and shall be bonded together with a compatible bonding agent. Additional thin chopped strand layers may be added as required to promote a proper bond between reinforcement layers.

A3.3.1.3. High-strength Aramid Fabric Reinforcement. The high-strength aramid fabric shall be constructed as required so that the tensile strength of resin impregnated strands shall be ≥ 500,000 psi (example: Kevlar® 49 or equivalent). The high-strength aramid fabric reinforcement shall be, 15 ± 2 ounces per square yard, and be compatible with polyester resin (A3.3.1.1.). The high-strength aramid fabric shall be approved by the Government prior to use.

A3.3.1.4. Continuous Strand Mat. The continuous strand mat shall be a continuous filament mat consisting of randomly oriented strands in multiple layers held together with a polyester binder and with a silane coupling agent.

Continuous strand mat shall be compatible with the polyester resin (A3.3.1.1.).

A3.3.1.5. Color of Panels. All surfaces of the FRP panels shall be colored representative of an “Army” green using pigmented resin. The selected pigment shall be compatible with the polyester resin (A3.3.1.1.). Excessive flaking, peeling, or scaling of panel coloring shall be grounds for rejection of the product.

A3.3.1.6. Non-skid Coating. The top wearing surface of each panel shall be coated, except for the underlap edges, with a non-skid coating. The coating shall be composed of crystalline silica and the polyester resin (A3.3.1.1.). The crystalline silica shall be RUST-OLEUM 200504 or equivalent and shall be compatible with the polyester resin (A3.3.1.1.). The dosage rate shall be approximately 1-lb crystalline silica per gallon of polyester resin (A3.3.1.1.).

The non-skid coating shall be applied to the wearing surface of each panel within 24 hrs of removal of the panel from the mold. Panel surfaces shall be clean, dry, and free of dust or other contaminates prior to application of the non-skid coating. Non-uniform application or excessive flaking, peeling, or scaling of the non-skid coating shall be grounds for rejection of the product.

A3.3.2. Bushing Material.

A3.3.2.1. Lower Joining Bushing. Lower joining bushings shall be made from 303 Stainless Steel.

A3.3.2.2. Upper joining bushing. The upper joining bushing shall be made from 1045 Steel and plated per SAE- AMS-QQ-P-416 Rev F, TYP II, Class 2, Gold. The upper joining bushing bolt shall be SAE Grade 5, 5/8-11 Thread. The upper joining bushing bolt shall be plated per AMS QQ-P-416 Rev F, TYP II, Class 2, Gold Hydrogen Embrittlement release baked at 370 degrees F for 23 hours within 4 hours of plating before assembly. The upper joining bushing bolt shall be adhered to the upper joining bushing via a threadlocking material (A3.3.2.7.).

A3.3.2.3. Anchor Bushing. Anchor bushings shall be made from 1045 Steel and plated per SAE-AMS-QQ-P-416 Rev F, TYP II, Class 2, Gold.

A3.3.2.4. Anchor Bushing Lining. If required (see Section A7.2.) anchor bushings shall be lined on the bottom surface and around the shoulder with an exothermic, rapid curing, elastomeric polyurethane lining system. Lining shall be brand Rhino TuffGrip or equivalent. The lining shall not migrate into the 0.828-in diameter hole in the underside of the anchor bushing so as not to prevent passage of an anchor bolt through said hole.

A3.3.2.5. Adhesive. The adhesive used to bond lower bushings to panel underlap edges shall be in accordance with ASTM C881, Type I, Grade 3, Class B.

A3.3.2.6. Rivet. The rivet used to fasten lower bushings to panel underlap edges shall be stainless steel structural blind rivets such as Huck MGL100-U8-8 or equivalent. If a rivet other than the Huck MGL100-U8-8 is selected, it shall be approved by the Government prior to use in lower joining bushings.

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A3.3.2.7. Threadlocking Material. The threadlocking material shall be LOCTITE 263 Red Threadlocker or equivalent and shall be applied at the manufacturer recommended application rate to ensure adhesion of the upper joining bushing bolt to the upper joining bushing (A3.3.2.2.). If the threadlocking material is other than LOCTITE 263, the material shall be approved by the Government prior to use.

A3.4. Panel Dimensions and Weights. All panels of the same classification shall be identical to the extent necessary to ensure interchangeability of component parts, assemblies, accessories, and spare parts.

A3.4.1. Full-size Panels. Full-size panels shall be finished to dimensions shown in Drawing 142003, on page A-17.

Panel edges shall be recessed to 0.25-in thickness on top edge (overlap) and 0.25-in thickness on the bottom edge (underlap). Two adjacent edges of a panel shall have the recess at the panel bottom; the other two edges shall be recessed at the panel top. The thickness of the panels at any underlap or overlap edge shall be 0.25 ± 0.05-in. The thickness of the panels in the center shall be 0.40 +.125/-.000-in. The 2.25-in diameter hole pattern along the underlap edges and the 2.50-in diameter hole pattern along the overlap edges is shown in Drawing 142003, on page A-17. The lower bushings shall be attached to the underlap edges at each hole using adhesive (A3.3.2.5) and two rivets (A3.3.2.6.). All holes in underlap edges of full-size panels shall contain lower bushings.

A3.4.2. Half-size Panels. Half-size panels shall be finished to dimensions shown in Drawing 142004, on page A-18.

Panel edges shall be recessed to 0.25-in thickness on top edge (overlap) and 0.25-in thickness on the bottom edge (underlap). Two adjacent edges of a panel shall have the recess at the panel bottom; the other two edges shall be recessed at the panel top. The thickness of the panels at any underlap or overlap edge shall be 0.25 ± 0.05-in. The thickness of the panels in the center shall be 0.40 +.125/-.000-in. The 2.25-in diameter hole pattern along the underlap edges and the 2.50-in diameter hole pattern along the overlap edges is shown in Drawing 142004, on page A-18. The lower bushings shall be attached to the underlap edges at each hole using adhesive (A3.3.2.5.) and two rivets (A3.3.2.6.). All holes in underlap edges of half-size panels shall contain lower bushings.

A3.4.3. Anchor Panels. Anchor panels are used to allow a full-size panel’s or half-size panel’s final underlap edge containing lower bushings to be transitioned to an open- holed edge for anchoring of the mat without removal of the lower bushings. These panels shall be anchored to the pavement surface using the anchor bushings and appropriate anchor system.

A3.4.3.1. Full-size Anchor Panels. Full-size anchor panels shall be finished to the dimensions shown in Drawing 142005, on page A-19. The thickness of the panel at the overlap edge shall be 0.25 ± 0.05-in. The thickness of the remaining panel shall be shall be 0.40 +.125/-.000-in. The 2.50-in diameter hole pattern along the panel edges is shown Drawing 142005, on page A-19.

A3.4.3.2. Half-size Anchor Panel. Half-size anchor panels shall be finished to the dimensions shown in Drawing 142005, on page A-19. The thickness of the panel at the overlap edge shall be 0.25 ± 0.05-in. The thickness of the remaining panel shall be 0.40 +.125/-.000-in. The 2.50-in diameter hole pattern along the panel edges is shown in Drawing 142005A, on page A-20.

A3.4.4. Weight. Approximate weight of the panels shall be as given in Table 2.

Table 2. Approximate Panel Weights Description Weight, lbs Full-size panel 400 Half-size panel 200 Full-size anchor panel 150 Half-size anchor panel 75

A3.5. Fiberglass and Aramid Fabric Reinforcement Laminate Schedule.

A3.5.1. Full-size and Half-size Panels. Each full-size and half-size panel shall contain 70-in wide plies of fiberglass reinforcement (A3.3.1.2.1.) that shall run continuous for the full length of each panel. Discontinuities or overlaps in the reinforcement section are not allowed. Each full-size and half-size panel may contain continuous strand mat

A-5 across the full 70-in width of the panel. There shall be no more than one discontinuity in continuous strand layers (i.e. 20-in of material spliced with 50-in of material to create the full 70-in wide section of continuous strand mat).

The outside edges of the panel’s four sides shall be reinforced with one 14-in wide minimum ply of high-strength aramid fabric (A3.3.1.3.). The selected laminate schedule shall be approved by the Government prior to use. An example reinforcement laminate schedule is shown in Drawings 142006 thru 142008 on pages A-21 thru A-23.

A3.5.2. Full-size and Half-size Anchor Panels. Each full-size and half-size anchor panel shall be constructed from 24-in-wide and 16-in wide plies of fiberglass reinforcement (A3.3.1.2.1.) that shall run continuous for the full length of each anchor panel. Each full-size and half-size anchor panel may contain continuous strand mat (A3.3.1.4.) across the full width of the panel. Each anchor panel shall be reinforced with one 24-in-wide ply of high-strength aramid fabric (A3.3.1.3.). Discontinuities or overlaps in the reinforcement, continuous strand mat, or aramid fabric sections are not allowed. The selected laminate schedule shall be approved by the Government prior to use. An example reinforcement laminate schedule is shown in Drawings 142006 thru 142008 on pages A-21 thru A-23.

A3.6. Polyester Resin. The panels shall be fabricated using a polyester resin (A3.3.1.1.) applied at a ratio of fiberglass reinforcement to resin of approximately 60:40 by weight. The exact rate of application shall be adjusted as required to obtain the specified properties and dimensions of the mat. The polyester resin shall thoroughly wet all reinforcement.

A3.7. Holes and Bushings.

A3.7.1. Holes. Holes shall be cut on the panel overlap, underlap, and anchor panel edges in accordance with the patterns shown in Drawings 142003 thru 142005A on pages A-17 thru A-20. The holes on the underlap edges of the panels shall be 2.25 ± 0.05-in in diameter. The holes on the overlap and anchor panel edges shall be 2.50 ± 0.0-in in diameter.

A3.7.2. Lower Joining bushings. A detailed drawing of the lower joining bushing is shown in Drawing 142010, on page A-25.The lower bushings shall be attached to the underlap edges of the full-size and half-size panels at each hole using adhesive (A3.3.2.5.) and two rivets (A3.3.2.6.). The rivet shall have no sharp edges. The bottom of the rivet receiving holes in the lower joining bushing shall be counter bored in accordance with Drawing 142010, on page A-25. The lower bushings shall be threaded to receive the 0.625-in bolt from the upper joining bushing.

A3.7.3. Upper Joining bushing. A detailed drawing of the upper joining bushings is shown in Drawing 142010, on page A-25. Upper joining bushings will be connected to lower joining bushings to join panels together to form a cover. The head of the upper joining bushing bolt shall sit flush with the 2.40-in top shoulder of the upper joining bushing.

A3.7.4. Anchor Bushings. A detailed drawing of the anchor bushings is shown in Drawing 142011, on page A-26.

The anchor bushing is designed to facilitate anchoring the system to a pavement surface through the holes on panel overlap edges and anchor panel edges.

A3.8. FRP Mat Panel Mechanical Properties. The cured resin shall produce a laminate having the mechanical properties shown in Table III when tested as specified in Section A4.5.

Table 3. Required Properties of FRP Panels Property Requirement Test Method Reference Tensile Strength, x-axis (Min) 32,000 psi ASTM D3039/M Tensile Strength, y-axis (Min) 45,000 psi ASTM D3039/M Flexural Strength, x-axis (Min) 42,000 psi ASTM D790 Flexural Strength, y-axis (Min) 65,000 psi ASTM D790 Thermal Expansion (Max) 1.8 x 10-5 in/in/°C ASTM D696 Ignition Temperature, Flash (Min) 450° F ASTM D1929 Hardness, Top (Min) 45 ASTM D2583 Hardness, Bottom (Min) 45 ASTM D2583

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Note: All testing is to be performed on those areas of panels which do not contain the high-strength aramid fabric reinforcement unless reasonable cause for testing other sections is cited (A4.2.1.). The x-direction is defined as the direction transverse to the intended direction of trafficking. The y-direction is defined as the direction parallel to the intended direction of trafficking which is perpendicular to the direction of anchor panel placement as seen in Drawing 142009, on page A-24.

A3.9. Workmanship. Workmanship for the FRP panels and bushings shall be of the quality prevailing among manufacturers normally producing similar items to those specified. Quality Control shall be of the quality prevailing among manufacturers normally producing similar items to those specified, and the panels shall be free from the following defects:

• Incorrect thickness

• Incorrect hole placement or size

• Delamination

• Dry spots

• Voids

• Blisters

• Crazing

• Cracks or tears

A4. FRP MAT PANEL COMPONENTS VERIFICATION.

A.4.1. Classification of Inspections of FRP Mat Panel Components. The inspection requirements specified herein are classified as follows:

• First article inspection.

• Conformance inspection.

A4.2. First Article Inspection. . If requested, a first article submission consisting of one typical FRP mat assembly (A1.2.1.) should be delivered to the Government (see A7.2.) for inspection and testing. The first article inspection shall be performed on a minimum of one of each type of panel (A1.2.) ordered. This inspection shall include examination specified in Section A4.4. and testing specified in Section A4.2.1. The first article may be either a first production item or a standard production item from the supplier’s current inventory provided the item meets the requirements of the specification and is representative of the design, construction, and manufacturing techniques applicable to the remaining items to be furnished under the contract. The Government reserves the right to determine at its discretion whether a current inventory item shall be accepted as a First Article submission. The panels produced under the contract shall be inspected by the manufacturer at their plant under the direction and in the presence of Government representatives. The purpose of this inspection shall be to determine panel conformity with the contract. Acceptance of the First Article inspection shall not constitute a waiver by the Government of its rights under the provisions contract document or relieve the manufacturer from any requirements defined in this specification. Failure to meet inspection criteria shall constitute cause for rejection.

A4.2.1. First Article Testing. If requested by the Government (see A7.2.), First Article testing shall be performed in conjunction with the First Article inspection specified in A4.2. First Article testing shall be performed on a randomly selected half-size panel submitted with the First Article submission. This randomly selected half-size panel shall be destructively tested and will remain property of the Government. First Article testing shall consist of the testing specified in A4.5.1. through A4.5.7. and shall be conducted by an independent or Government laboratory.

Failure to meet test or inspection criteria shall constitute cause for rejection. First Article approval shall not constitute a waiver by the Government of its rights under the provisions of the contract document or relieve the manufacturer of any requirements defined in this specification. Should the Government have reason to suspect that full-size panels, full-size anchor panels, half-size anchor panels, and/or the other half-size panels are not representative of construction of the half-size panel randomly selected for first article testing, the Government reserves the right to destructively test any panel included in the first article submission and reject the product on a case-by-case basis (areas of panels including aramid fabric reinforcement should exhibit approximately a minimum

A-7 of 80% of the required properties given in Table 3. If additional panels are destructively tested, they will remain property of the Government.

A4.3. Conformance Inspection. The conformance inspection shall include the specified examination of A4.4. and any selected tests of A4.5. and shall be performed on panels selected at the Government’s discretion at a rate of no more than two percent of production volume for destructive testing. The manufacturer is required to notify the Government should raw materials change at any time during production. Following this notification the Government may, at its discretion, perform additional conformance inspections as described herein. Failure to comply with the mechanical properties listed in Table III shall be cause for rejection of all panels manufactured using the same methods as the tested panel(s).

A4.4. Workmanship Examination. A minimum of one of each panel type (A1.2.) shall be examined for compliance with the requirements specified in Section A3 of this specification. Any redesign or modification of manufacturer’s standard product to comply with specified requirements, or any necessary redesign or modification following failure to meet specified requirements shall receive particular attention for adequacy and suitability. This element of inspection shall encompass all visual examinations and dimensional measurements. Noncompliance with any specified requirements or presence of one or more of the following defects preventing or lessening maximum efficiency shall constitute cause for rejection.

• Thickness. Verify by measuring each full, half, and anchor panel edge in at least two (2) places (minimum eight measurements per piece).

• Hole size and placement. Verify specification compliance by measuring at least five (5) holes on each full, half, and anchor panel.

• Delamination. Not tolerable in the FRP panels. Verify by visual examination when removing the panel from the mold.

• Dry spots. None are tolerable in excess of 0.5-in in diameter. More than 10 occurrences in any 1-square ft area are not tolerable. Verify by visual examination when removing the panel from the mold.

• Blisters and voids. None are tolerable in excess of 0.5-in in diameter. More than 10 occurrences in any single panel are not tolerable. Verify by visual examination when removing the panel from the mold.

• Non-skid coating. Verify that the nonskid coating is the correct particle size and has been applied uniformly across the appropriate panel areas. Non- uniform coating or inappropriate particle size shall not be tolerable.

• Cracks or tears. None are tolerable that penetrate into the fiberglass reinforcement of the panels. Verify by visual examination and measurement when removing the panel from the mold.

A4.5. Testing. Failure to comply with the mechanical properties listed in Table III shall be cause for rejection of all panels manufactured using the same methods as the tested panel(s). All tests shall be performed on specimens without the high-strength aramid fabric (A3.3.1.3.) with the exception of panels that are suspected of not being uniform across the production lot (A4.2.1.).

A4.5.1. Tensile Strength. Tensile strength testing shall be performed in accordance with ASTM D3039/M except as specified herein. Ten tensile tests will be performed on specimens randomly selected from a portion(s) of an FRP panel(s). Five (5) specimens shall be oriented parallel to the x-axis, and five (5) shall be oriented parallel to the y-axis. Test specimens shall measure 10-in long (along reference axis) by 1-in wide by the thickness of the panel (0.4-in nominal). The rate of crosshead movement shall be 0.1-in per minute. Failure of the tested average of either the x-direction or y-direction test specimens to meet the requirement specified in Table 3 shall be cause for rejection of the product.

A4.5.2 Flexural Strength. Flexural strength testing shall be performed in accordance with ASTM 790, Procedure A, except as specified herein. Ten flexural tests will be performed on specimens randomly selected from a portion(s) of an FRP panel(s). Five (5) specimens shall be oriented parallel to the x-axis, and five (5) shall be oriented parallel to the y-axis. Test specimens shall measure 10-in long (along reference axis) by 1-in wide by the thickness of the mat (0.4- in nominal). The rate of crosshead movement shall be 0.43-in per minute. The support span shall be 8.0-in. The loading nose shall have a radius of 1.0-in, and the radius of the supports shall be 0.5-in. Failure of the tested average

A-8 of either the x-direction or y- direction test specimens to meet the requirement specified in Table 3 shall be cause for rejection of the product.

A4.5.3. Thermal Expansion. Thermal expansion testing shall be performed in accordance with ASTM D696 except as specified herein. A minimum of two specimens, one tested in the x-direction and one tested in the y-direction, shall be tested at temperature extremes of -30°C to +30°C. Failure of the tested average to meet the requirements specified in Table III shall be cause for rejection of the product.

A4.5.4. Ignition Temperature. Ignition temperature testing shall be performed in accordance with ASTM D1929 except as specified herein. Only the flash ignition temperature of the FRP material is required to be determined. A minimum of two determinations shall be made. Failure of any specimen to meet the requirements specified in Table III shall be cause for rejection of the product.

A4.5.5. Hardness. The indentation hardness of each selected specimen shall be tested according to ASTM D2583 except as specified herein. The hardness shall be measured at a minimum of ten points on the top surface of the selected panel and ten points on the bottom surface of said panel. The measurements shall be taken at 73.4°F ± 3.6°F after being conditioned at that temperature with 50 ± 10 percent relative humidity for a minimum of 5 hours. Failure of the tested averages to meet the requirements specified in Table III shall be cause for rejection of the product.

A4.5.6. Dimensional Accuracy. An overall check of the dimensional accuracy shall be made by joining the panels in a random order to form a cover, as shown in Drawing 142009, on page A-24. The joining shall be completed using the upper joining bushings supplied by the manufacturer and the lower joining bushings which shall be fixed to the underlap regions of full- and half-size panels. Binding, misalignment, or the inability to join the panels in this manner to form a cover shall be cause for rejection of the product.

A4.5.7. Interchangeability Test. When panels pass the test of A.4.5.6., disassemble the cover and reassemble the panels in a different sequence. Binding, misalignment, or the inability to join the panels in this manner to form a cover shall be cause for rejection of the product.

A5. ADDITIONAL REQUIRED FRP MAT PANEL ASSEMBLY ITEMS.

A5.1. Metal Pallet w/16 D-Rings. A detailed drawing of the FRP mat panel, metal pallet w/16 d-rings is shown on page A-31. There are two (2) metal pallets w/16 d-rings are required per FRP Mat Panel Assembly.

A5.2. 463L Pallets HCU-6/E. Four (4) 463L pallets HCU-6/E (NSN 1670-00-820-4896) are part of the full FPR mat assembly. These 463L pallets are used to ship the FRP Mat Panel Assembly with using USAF cargo aircraft.

A5.3. Couplers, Square Pallet, 463L. Four (4) couplers, square pallet, 463L (NSN 1670-01-061-0990) are part of the full FRP mat assembly. Two (2) couplers are used to couple two (2) 463L pallets to make a pallet train.

A5.4. Geotextile Fabric Roll. One (1) roll of geotextile fabric material roll (15-ft wide x 300-ft long) is part of the full FRP mat assembly. Geotextile fabric roll shall be US Fabrics or equivalent (see A5.4.1 and A5.4.2) See Figure A5.4.

A5.4.1. Geotextile Fabric Roll Material.

• Nonwoven needle-punched geotextile made of 100% polypropylene staple filaments

• Resists ultraviolet and biological deterioration, rotting, naturally encountered basics and acids.

• Polypropylene is stable within a pH range of 2 to 135-1/2-in (140 mm) paddle diameter

A5.4.2. Geotextile Fabric Roll.

• Weight: ASTM D-5264; 6-oz/y2

• Tensile Strength: ASTM D-4632; 160-lbs

• Elongations @ Break: ASTM D-4632; 50%

• Mullen Burst: ASTM D-3786; 305-psi

• Puncture Strength: ASM D-4833; 90-lbs

A-9

• CBR Puncture: ASTM D-6241; 410-lbs

• Trapezoidal Tear: ASTM D-4533; 60-lbs

• Apparent Opening Size: ASTM D-4751; 70 US Sieve

• Permittivity: ASTM D-4491; 1.50 Sec-1

• Water Flow Rate: ASTM D-4491; 110-g/min/sf

• UV Resistance @ 500 Hours: ASTM D4355; 70%

Figure A5.4.

A5.5. Tarp, UV Resistant. Two (2) tarps, UV resistant are part of the full FRP mat assembly. Tarps, UV resistant shall be Tarps Now part #FS-P12MIL-FR or equivalent (see A5.5.1.)

A5.5.1. Tarp, UV resistant, properties.

• 100% Water Proof

• Meets fire resistant codes: NFPA 701 & CPAI-84

• Heavy duty poly tarp

• 12 mil thick

• Acid & rot resistant

• Brass grommets approximately every 24-in

A5.6. Snap Hook Ratchet Strap, Heavy Duty, Black, 2-in. 12 snap hook ratchet straps, heavy duty, black 2-in are part of the full FRP mat assembly. Snap hook ratchet straps, heavy duty, black 2-in shall be Ratchet Straps USA, part # US-2HDRFS or equivalent (see A5.6.1.). See Figure A5.6.

A5.6.1. Snap hook ratchet straps, heavy duty, black 2-in properties.

• Component length: 30-ft nominal

• Component width: 2-in nominal webbing

• Material: Polyamide nylon webbing and steel connector snap

• Special features: 30-ft long and web strength of 12,000-lbs

• Tightening device: Ratchet w/integral hooks and operating strength of 11,000-lbs for the ratchet and

10,000-lbs for the hooks.

A-10

Figure A5.6.

A5.7. Dunnage, 4-in x 4-in x 78-in, Heat Treated. 12 pieces of dunnage, 4-in x 4-in x 78-in HEAT TREATED are part of the full FRP mat assembly. Dunnage, 4-in x 4-in x 78-in HEAT TREATED shall be AMS Network, LLC, part # HTL4x4x80 or equivalent (see A5.7.1.).

A5.7.1. Dunnage, 4-in x 4-in x 78-in, Heat Treated.

• Material: Heat Treated Wood

• Size: 4-in x 4-in x 78-in

• Material Spec: ISPM 15

A5.8. Tarp Tie Downs, 6-in. 24 tarp tie downs, 6-in are part of the full FRP mat assembly. Tarp tie downs, 6-in shall be Tarps Now part # TA-BB6-100-BLK or equivalent (see A5.8.1.). See Figure A1.5.8.

A5.8.1. Tarp Tie Downs, 6-in.

• Material: Premium elastic cord & durable nylon black ball

• Stretches out to 8.5-in

• Color: Black

Figure A5.8.

A5.9. Tarp Tie Downs, 11-in. 20 tarp tie downs, 11-in are part of the full FRP mat assembly. Tarp tie downs, 11-in shall be Tarps Now part # TA-BB11-100-BLK or equivalent (see A5.9.1.). See Figure A5.9.

A5.9.1. Tarp Tie Downs, 11-in.

A-11

• Material: Premium elastic cord & durable nylon black ball

• Stretches out to 15.5-in

• Color: Black

Figure A5.9.

A5.10. IDIQ Unit of Issue per Item for FRP Mat Panel Assembly. Table 4, shows what the unit of issue for each item in the FRP mat panel assembly listing, when NOT procured as a full assembly.

Table 4. IDIQ Quantities per Item for FRP Mat Panel Assembly Item Unit of Issue

FRP Mat Panel, Full Size, Half Size, Full Anchor, and Half Anchor

1 Mat Set (7 Full Mat Panels, 6 Half Panels, 3 Full Anchor Panels, 4 Half Anchor Panels, and 1 FRP Mat Panel Metal Pallet) with 1 FRP Mat Panel Metal Pallet, 16-D Rings

FRP Mat Panel Metal Pallet, 16-D- Rings

1 each

463L Pallet HCU-6/E 1 each Coupler, 463L Pallet 1 set of two (2) Geo-Fabric 15-ft x 300-ft roll 1 roll Tarp, UV Resistant 1 each Snap Hook Ratchet Strap, Heavy Duty, Black, 2-in

1 set of four (4)

Dunnage, 4-in x4-in x 78-in, Heat Treated

1 each

Tarp Tie Downs, 6-in 1 set of twelve (12) Tarp Tie Downs, 11-in 1 set of ten (10)

A6. FRP MAT PANEL ASSEMBLY PACKAGING.

A6.1 Packaging. For acquisition purposes, the packaging requirements shall be as specified in the contract or order (see A7.2.). When actual packaging of material is to be performed by DoD personnel, these personnel need to contact the responsible packaging activity to ascertain requisite packaging requirements. Packaging requirements are maintained by the Inventory Control Point’s packaging activity within the Military Department or Defense Agency, or within the Military Department’s System Command. Packaging data retrieval is available from the managing Military Department’s or Defense Agency’s automated packaging files, CD-ROM products, or by contacting the responsible packaging activity.

A6.2. FRP Mat Panel Packaging Requirements. The following list of packaging requirements are used to package each FRP mat set for shipping.

A-12

A6.2.1. Plastic Sheeting, Black, 10mil. ~1,400-ft of plastic sheeting, black, 10mil is required to wrap each of the four (4) FRP mat panel sets. Plastic sheeting, black 10mil shall be Husky part # CF1020B or equivalent (see A6.2.1.1.).

A6.2.1.1. Plastic Sheeting, Black 10mil.

• Material: Polyethylene plastic

• Thickness: 10 Mil

A6.2.2. Metal Strapping (Banding) 5/8-in x .023-in. ~560-ft of metal strapping (banding) 5/8-in x .023-in is required to secure each of the four (4) FRP mat panel sets. Metal strapping 5/8-in x .023-in shall be Uline part #S-1082 or equivalent (see A6.2.2.1.).

A6.2.2.1. Metal Strapping 5/8-in x .023-in.

• Material: Low carbon cold-rolled steel (not stainless or galvanized or zinc coated)

• Finish: Painted and waxed

• Width: 5/8-in

• Thickness: .023-in

• Breaking Strength: 1,725-lbs

A6.2.3. Metal Strapping (Banding) Seals (Clips), 5/8-in. 48 metal strapping (banding) seals (clips), 5/8-in are required secure the metal strapping around each of the four (4) the FRP mat panel sets. Metal strapping (banding) seals (clips), 5/8-in shall be Uline part #S-832 or equivalent (see A6.2.3.1.).

A6.2.3.1. Metal Strapping (Banding) Seals (Clips), 5/8-in.

• Material: Rust resistant zinc coating (not stainless steel)

• Type: Open

• Fits Strapping Width: 5/8-in

• Seal Length: 1.094-in

• Compatibility:

o High Tensile: H-530 o Standard: H-25 o Industrial: H-352 o Deluxe: H-663

• Standards: Meets ASTM D3953, Finish B-Grade 2, Class R-Regular Duty, Style I-Open

A6.2.4. Edge Protectors, 2-1/2-in x 1-3/4-in. 112 Edge Protectors, 2-1/2-in x 1-3/4-in are required during the securing of the metal strapping around each of the four (4) the FRP mat panel sets, to protect the edges of the FRP mat panel from the metal strapping. Edge protectors, 2/-1/2-in x 1-3/4-in shall be Uline part #S-3474 or equivalent (see A6.2.4.1.) see Figure A6.2.4.

A6.2.4.1. Edge Protectors, 2-1/2-in x 1-3/4-in.

• Material: Polyethylene Hival Thermoplastic Resin

• Size: 2-1/2-in x 1-3/4-in

• Thickness: 0.07-in

• Color: Black

A-13

Figure A6.2.4.

A6.2.5. Edge Protectors, 5-1/4-in x 2-in. 16 edge protectors, 5-1/4-in x 2-in are required during the securing of the each of the four (4) the FRP mat panel sets on to the metal pallet w/16 D-Rings using the snap hook ratchet straps, heavy duty, black 2-in. Metal strapping (banding) seals (clips), 5/8-in shall be Uline part #S-3843 or equivalent (see A6.2.5.1.) see Figure A6.2.5.

A6.2.5.1. Edge Protectors, 5-1/4-in x 2-in.

• Material: Polyethylene Hival Thermoplastic Resin

• Size: 5-1/4-in x 2-in

• Thickness: 0.07-in

• Color: Black

Figure A6.2.5.

A6.3. Full FRP Drawing Package. The vendor shall furnish to the gov’t a full FRP mat panel assembly drawing package. This drawing package shall include a complete inventory listing with National Stock Numbers (NSNs)/manufacturer’s part numbers (if not a NSN has been created for item), packaging drawings with item details (as seen in drawings on pages A-27 thru A-35), be gov’t owned, and have the AFCEC logo on each page. If there are any approved (gov’t) changes to any item in this FRP mat panel assembly, the vendor shall provide updated revisions of the drawing package within 90 days of each approved change.

A6.4. FRP Panel Set Packaging Requirements. Stacked mat set(s) shall be wrapped in one (1) layer of polyethylene sheeting, 10 mils. Prior to banding, the exterior of the packaged assembly shall be sealed to help prevent moisture

A-14 intrusion. The stacked, wrapped, and sealed assemblies shall be banded along the entire approximate 18 ft length of the stacked assembly by flat steel metallic bands conforming to ASTM D3953, Type 1, Regular Duty High-Strength strapping, size 5/8-in by 0.023-in thick. The spacing of the banding shall be no greater than 3-ft. The banding shall use regular duty, organic finished, snap-on seal of 5/8-in width, as per ASTM D3953. A plastic edge protector of 2- 1/2-in width and 1-3/4-in leg length shall be used to protect the FRP panels from the steel banding at each point of corner contact with the stacked panels (four protectors per band). The plastic edge protector shall be PAC Strapping Products CP-122 or equivalent.

A6.4.1. FRP Panel Set Stacking Sequence. Each FRP panel set will be stacked in the following sequence from the bottom of the stack upwards:

• One (1) full-size panel

• One (1) full-size panel

• Two (2) half-size panels

• One (1) full-size panel

• One (1) full-size panel

• Two (2) half-size panels

• One (1) full-size panel

• One (1) full-size panel

• Three (3) full-size Anchor panels

• Four (4) half-size Anchor panels

• Two (2) half-size panels

• One (1) full-size panel

A6.4.1.1. FRP Mat Panel, (pallet #1) Metal Pallet w/16 D-rings Packing Requirements. Two (2) FRP mat panel sets; each packaged according to A6.4.1. One (1) FRP mat panel set can be placed on the metal pallet and the second FRP mat panel shall be set on six (6) 4-in by 4-in wooden dunnage, that is placed between the two (2) FRP mat panel sets. These two (2) FRP mat panel sets will be covered by a UV-resistant trap and secured with 2-in wide x 27-ft long snap hook ratchet straps. On the underlap side of the pallet, the vendor shall paint “1 of 5” and “Fork Entry This Side” on the UV-resistant trap (see shown in Figure A6.6.). Reference drawings on pages A-27 thru A- 35.

A6.4.1.2. FRP Mat Panel, (pallet #2) Metal Pallet w/16 D-rings Packing Requirements. Two (2) FRP mat panel sets; each packaged according to A6.4.1. One (1) FRP mat panel set can be placed on the metal pallet and the second FRP mat panel shall be set on six (6) 4-in by 4-in wooden dunnage, that is placed between the two (2) FRP mat panel sets. These two (2) FRP mat panel sets will be covered by a UV-resistant trap and secured with 2-in wide x 27-ft long snap hook ratchet straps. On the underlap side of the pallet, the vendor shall paint “2 of 5” and “Fork Entry This Side” on the UV-resistant trap (see example as shown in Figure A6.6.). Reference drawings on pages A- 27 thru A-35.

Figure A6.6.

A-15

A6.4.1.3. 463L Pallets. Four (4) 463L Pallets HCU-6/E (NSN 1670-00-820-4896) are part of the full FPR mat assembly. These four (4) 463L pallets will be placed on top of the two (2) wrapped and secured FRP mat panel sets on “pallet #2” metal pallet w/16 d-rings. The four (4) 463L pallets will be placed in stacks of two and two, with two

(2) couplers coupling each set of two (2) 463L pallets (A5.2.), per the drawing on page A-34.

A6.4.1.4. Couplers, Square Pallet, 463L. Four (4) Couplers, square pallet, 463L (NSN 1670-01-061-0990) are part of the full FRP mat assembly. Two (2) couplers (A5.3.) are used to couple two (2) 463L pallets to make a pallet train.

A6.4.1.5. Geotextile Fabric Roll. One (1) roll of geotextile fabric material roll (15-ft wide x 300-ft long); wrapped in a weather proof packaging (A5.4.), is placed on top of the 463L coupled pallets on the top metal pallet.

A6.4.1.6. FRP mat panel assembly shipping configuration. Secured “pallet #2” shall be placed on a secured “pallet #1”. Then the 463L pallets (coupled together (A5.2. and A5.3.) and the geotextile fabric roll (A5.4.) is center on top of the 463L pallets. Then all items are secured with 2-in wide x 27-ft long snap hook ratchet straps, as shown in drawing on page A-35.

A7. NOTES.

A7.1. Intended Use. This specification covers FRP panels and bushings for use as an expedient cover for backfilled bomb craters within airfield pavements.

A7.2. Acquisition Requirements. Acquisition documents should specify the following:

• Title, number, and date of this specification

• Type and number of panels required

• If reference documents are other than those specified

• When first article testing is required for inspection and approval

• If bushings are to be made from different material than what is specified

• If panels are to be fabricated differently than what is specified

• If a non-skid coating other than what is specified is to be required

• If an anchor bushing lining material is required

• If size of the cover to be assembled to check the overall dimensional accuracy of the panels is different than what it specified

• Requirements for marking of the panels

• Level of packing required

A-16

A-17

A-18

A-19

A-20

A-21

A-22

A-23

A-24

A-25

A-26

DESCRIPTION REV DATE APPROVED

INITIAL RELEASE -- 5/11/12018 JBB

UPDATED A 4/26/2019 JBB

UPDATED B 2/11/2020 JBB

PART NO ITEM NO QTY DESCRIPTION MATERIAL SPEC NSN UNIT WEIGHT (LBS) TOTAL WEIGHT (LBS)

FRP-4K-PT 0001 1 FIBER-REINFORCED POLYMER (FRP) PANEL ASSEMBLY MIL-DTL-XXXX N/A 23175

AMSPALLET1 0001-A 1 PALLET #1 CONSISTING OF 2 MAT SETS STATEMENT OF WORK N/A 10873

AMSPALLET2 0001-B 1 PALLET #2 CONSISTING OF 2 MAT SETS PLUS 1 ROLL GEOTEXTILE STATEMENT OF WORK N/A 12300

N/A 0001-C 1 INVENTORY LIST N/A N/A 1

PREPARED: J.B.B. DATE: 02/11/2020

CHECKED: N/A DATE:02/11/2020

ENGINEER: J.B.B. DATE: 02/11/2020

APPROVED: J.B.B. DATE:02/11/2020

SCALE: NONE

A

B

C

4 3

A

C

SHEET

B

TITLE:

DRAWING NO:

6833284-01

REV:

B

FIBER-REINFORCED POLYMER

(FRP) KIT

PANEL ASSEMBLY

NOTES

AMS NETWORK, LLC

CONSISTS OF ITEM 0001-A THROUGH

0001-C

AMS INDUSTRIES. LLC

AMS INDUSTRIES. LLC

AMS INDUSTRIES. LLC

4 3 2

TABLE 1

CAGE CODE:

65S22THIRD ANGLE PROJECTION

FIBER-REINFORCED POLYMER (FRP) PANEL ASSEMBLY

DETAILED SPECIFICATION

FIBER-REINFORCED POLYMER (FRP) MAT FOR AIRFIELD DAMAGE RECOVERY (ADR)

SCOPE:

THIS DRAWING PACKAGE DETAILS THE PACKAGING AND COMPONENTS FOR THE UNITED STATES AIR FORCE FIBER- REINFORCED POLYMER (FRP) PANEL SETS. THIS ASSEMBLY IS A COMPONENT OF THE FRP-UTC THAT PROVIDES FOD COVER

CAPABILITY.

CLASSIFICATION:

FRP PANELS SHALL BE THE FOLLOWING TYPES:

(a) FULL PANEL 208 X 78 INCHES

(b) HALF PANEL 108 X 78 INCHES

(c) FULL ANCHOR PANEL 200 X 24 INCHES

(d) HALF ANCHOR PANEL 100 X 24 INCHES

PANEL ASSEMBLY DEFINITION:

REQUIRED PANELS SUFFICIENT TO PROVIDE FOD COVER CAPABILITY FOR 1 EACH 50 FT DIAMETER CRATER;

OR MULTIPLE SMALLER CRATERS (3 EACH 30 FT; OR 6 EACH 20 FT; OR 20 EACH 10 FT; OR MIXTURE)

QUANTITIES OF COMPONENTS:

COMPLETE PANEL ASSEMBLY CONSISTS OF:

4 MAT SETS, 1 ROLL GEO-TEXTILE, 4 EACH 463L PALLETS, AND 4 COUPLERS

A-27

INITIAL RELEASE -- 5/11/2018 JBB

UPDATED A 4/26/2019 JBB

UPDATED B 2/11/2020 JBB

PALLET # 1

2 FRP MAT SETS

PALLET #2

2 FRP MAT SETS

1 ROLL GEO-TEXTILE

4 EACH 463L PALLETS

4 EACH 463 L PALLET COUPLERS

FRP PANEL ASSEMBLY (PALLET #1 AND PALLET #2 )

4 FRP MAT SETS

1 ROLL GEO-TEXTILE

4 EACH 463L PALLETS

4 EACH 463 L PALLET COUPLERS

PREPARED: J.B.B. DATE: 02/11/2020

CHECKED: N/A DATE:02/11/2020

ENGINEER: J.B.B. DATE: 02/11/2020

APPROVED: J.B.B. DATE:02/11/2020

SCALE: NONE

5 4 3 2 1

A A

TITLE:

FIBER-REINFORCED POLYMER

(FRP) KIT

PANEL KIT

THIRD ANGLE PROJECTION

CAGE CODE:

65S22

DRAWING NO:

6833284-01

REV:

A

SHEET

C

B B

C

4 3 2 1

A-28

INITIAL RELEASE -- 5/11/2018 JBB

UPDATED A 4/26/2019 JBB

UPDATED B 2/11/2020 JBB

PART NO ITEM NO QTY U/I DESCRIPTION MATERIAL MATERIAL SPEC NSN

UNIT WEIGHT

(LBS)

TOTAL WEIGHT

(LBS) NOTES

FRP-FP-LJB 0001-01 14 EA FULL MAT PANEL W/LOWER BUSHINGS VARIOUS MIL-DTL-XXXX-142003 N/A 400.00 5600.00 AMS NETWORK, LLC FRP-HP-LJB 0001-02 12 EA HALF PANEL W/LOWER BUSHINGS VARIOUS MIL-DTL-XXXX-142004 N/A 200.00 2400.00 AMS NETWORK, LLC FRP-FAP 0001-03 6 EA FULL ANCHOR PANEL VARIOUS MIL-DTL-XXXX-142005 N/A 150.00 900.00 AMS NETWORK, LLC FRP-HAP 0001-04 8 EA HALF ANCHOR PANEL VARIOUS MIL-DTL-XXXX-142005A N/A 75.00 600.00 AMS NETWORK, LLC CF1020B 0001-05 700 SF BLACK 10 MIL PLASTIC SHEETING POLYETHYLENE COMML N/A 0.03 17.50 HUSKY S-1082 0001-06 280 FT STEEL BANDING .0.23 X 5/8-in POLYESTER COMML N/A 0.01 1.40 ULINE S-832 0001-07 28 EA STEEL SEALS 5/8 X 1-31/32-in GALVANIZED COMML N/A 0.01 0.28 ULINE FS-P12MIL-PR 0001-11 1 EA UV RESISTANT TARPS SILVER 10 X 20-ft POLYETHYLENE COMML N/A 15.00 15.00 TARPS NOW TA-BB6-100-BLK 0001-12 12 EA TARP TIE DOWNS-6-in HIGH GRADE RUBBER COMML N/A 1.00 12.00 TARPS NOW TA-BB11-100-BLK 0001-12A 10 EA TARP TIE DOWNS-11-in HIGH GRADE RUBBER COMML N/A 1.00 10.00 TARPS NOW S-3474 0001-19 56 EA EDGE PROTECTORS 2-1/2 X 1-3/4-in PLASTIC COMML N/A 0.10 5.60 ULINE S-3843 0001-20 8 EA EDGE PROTECTORS-5 X 2-in PLASTIC COMML N/A 0.20 1.60 ULINE US-2HDRFS 0001-13 4 EA 2-in SNAP HOOK RATCHET STRAPS 27 FT.BLACK POLYESTER COMML N/A 6.00 24.00 RATCHET STRAPS USA 16DRMPA 0001-22 1 EA 16 D-RING METAL PALLET ASSEMBLY SA36 STEEL PLATE COMML N/A 938.00 938.00 AMS NETWORK, LLC HTL4X4X80 0001-08 12 EA DUNNAGE 4 X 4 X 78-in HEAT TREATED LUMBER HT WOOD ISPM 15 N/A 29.00 348.00 AMS NETWORK, LLC

10873

PALLET #2

PART NO ITEM NO QTY U/I DESCRIPTION MATERIAL MATERIAL SPEC NSN

UNIT WEIGHT

(LBS)

TOTA…