PARTS KIT, BALL VAL

CONTACT INFORMATION|4|N743.23|WVT|N/A|ALANA.M.BOYER2.CIV@US.NAVY.MIL| ITEM UNIQUE IDENTIFICATION AND VALUATION (JAN 2023)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (DEC 2014)|1|See specification sections C and E| INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2||| INSPECTION AND ACCEPTANCE - SHORT VERSION|8||||||||| GENERAL INFORMATION-FOB-DESTINATION|1|B| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (JAN 2023)|16|Stand-Alone Receiving Report - Certifications Combo - Receiving Report & Invoice - Material|N/A|TBD|N00104|TBD|N39040 - Certifications, S4306A - Material |N50286|TBD|133.2|N/A|N/A|N39040 - Certifications |N/A|N /A|See DD FORM 1423|PORT_PTNH_WAWF_NOTIFICATION@NAVY.MIL ALANA.M.BOYER2.CIV@US.NAVY.MIL| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUNE 2003)|6|One year from date of delivery |One year from date of delivery ||||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM-BASIC (FEB 2024)|11|||||||||||| SMALL BUSINESS SUBCONTRACTING PLAN (DOD CONTRACTS)-BASIC (DEV 2026-O0037)(FEB 2026))|2||| WARRANTY OF DATA-BASIC (DEVIATION 2026-O0035) (FEB 2026)|2||| NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (DEV 2026-O0037)(FEB 2026)|1|| SECURITY PROHIBITIONS AND EXCLUSIONS (CLASS DEVIATION 2026-O0025)(FEB 2026)|7|||||||| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (OCT 2025)|13|||||||||||||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024))|5|||||| BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024)|1|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAR 2025)(DEVIATION 2025-O0003 AND2025-O0004))|13|332919|750|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||X| 1. DD1423 Data Item A001 (Inspection and Test Plan) may be waived if already on file at NAVSUP WSS Mechanicsburg. 2. Portsmouth NSY's DODAAC has changed from N00102 to N50286. Any reference to N00102 within this order should be updated to N50286. 3. The following proposed delivery schedule applies: Submission of Certification Data CDRLs will be on or before 20 days prior to scheduled delivery. PNSY review/acceptance of Certification CDRLs 6 working days after receipt of Certification DD 1423 CDRLs. Final delivery of material will be on or before 274 days after effective date of the resulting contract. 4. Any contract awarded as a result of this solicitation will be "DO" rated order; "DO" rated order certified for national defense use under the Defense Priorities and Allocations System (DPAS). 5. NAVSUP WSS Mechanicsburg will be considering past performance in the evaluation of offers. 6. If drawings are included in the solicitation, access needs to be requested on the individual solicitation page on Contracts Opportunities on the Government's beta.SAM website. After requesting access, send an email to the Primary POC listed on the solicitation. 7. This order is issued pursuant to Emergency Acquisition Flexibilities (EAF). 8. This is a Level 1 Repair. 9. Please submit: NOT TO EXCEED (NTE) pricing or FIRM FIXED PRICE (FFP). This includes the teardown, evaluation, inspection and full repair of the item to "like new" or "A" condition. See statement of work in solicitation. Please also provide an approximate cost of new item if available. 10. A beyond repair (BR)/ beyond economic repair (BER) price shall also beprovided in addition to the repair price at time submission of quote. 11. Do NOT include the cost for shipping material as the government implementedshipping system or ATAC will be shipping/delivering material. 12. This contract utilizes Commercial Asset Visibility (CAV). See clause NAVSUPWSSFA25 for further details. \ 1. SCOPE 1.1 The material covered in this contract/purchase order will be used in a crucial shipboard system. The use of incorrect or defective material would create a high probability of failure resulting in serious personnel injury, loss of life, loss of vital shipboard systems, or loss of the ship itself. Therefore, the material has been designated as SPECIAL EMPHASIS material (Level I, Scope of Certification, or Quality Assured) and special control procedures are invoked to ensure receipt of correct material. 2. APPLICABLE DOCUMENTS 2.1 Order of Precedence - In the event of a conflict between the text of this contract/purchase order and the references and/or drawings cited herein, the text of this contract/purchase order must take precedence. Nothing in this contract/purchase order, however, must supersede applicable laws and regulations unless a specific exemption has been obtained. 2.2 Applicable Documents - The document(s) listed below form a part of this contract/purchase order including modifications or exclusions. 2.2.1 Documents, drawings, and publications supplied are listed under "Drawing Number". These items should be retained until an award is made. 2.2.2 "Document References" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. 2.2.3 Specification Revisions - The specification revisions listed under "Documents References" below are the preferred revision. Older and/or newer r evisions are acceptable when listed within Contract Support Library Reference Number CSD155 in ECDS (Electric Contractor Data Submission) at: ht tps://register.nslc.navy.mil/. This is to allow Contractors to use certain acceptable older specification revisions to purge their existing stock of material certified to those older revisions or to use newer specification revisions when material is certified to newly released revisions,without requiring the submittal of waiver/deviation requests for each specification revision on every contract. Revisions of specifications reflecting editorial and/or re-approval (e.g. E2009, R2014, etc.) are considered inconsequential, but are acceptable when their revisions are listedwithin CSD155 or elsewhere within this contract. DRAWING DATA=EB-2000 |96169| C|SP |D|0001 | C|00000|0000000 DRAWING DATA=5959311 |53711| C| |D|0001 | C|00000|0000000 DRAWING DATA=5959311C5 |53711| A|ER |D|0001 | A|00000|0000000 DRAWING DATA=7016077 |53711| B| |D|0001 | B|00000|0000000 DRAWING DATA=7016077B66 |53711| B|ER |D|0001 | B|00000|0000000 DOCUMENT REF DATA=FED-STD-H28 | | |B |190424|A| | | DOCUMENT REF DATA=FED-STD-H28 |0020| |B |941221|A| |01| DOCUMENT REF DATA=ANSI/ASQ Z1.4 | | | |080101|A| | | DOCUMENT REF DATA=ASTM-B367 | | | |220401|A| | | DOCUMENT REF DATA=ASTM-B381 | | | |130701|A| | | DOCUMENT REF DATA=MIL-STD-792 | | |F |230223|A| |01| DOCUMENT REF DATA=ISO_9001 | | | |081115|A| | | DOCUMENT REF DATA=ISO10012 | | | |030415|A| | | DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | | DOCUMENT REF DATA=MIL-I-45208 | | |A |810724|A|1 | | DOCUMENT REF DATA=MIL-STD-45662 | | |A |880801|A| | | DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | | DOCUMENT REF DATA=0900-LP-001-7000 | | | |810101|C| |01| DOCUMENT REF DATA=S9074-AQ-GIB-010/248 | | |1 |191112|A| | | DOCUMENT REF DATA=S9074-AR-GIB-010A/278 (CHG A) | | | |130214|A| | | 3. REQUIREMENTS 3.1 REFURBISHED MATERIAL STATEMENT OF WORK (REPAIR SOW) - 3.1.1 INSPECTION - Clean and determine if refurbishment is possible. At disassembly, the Contractor must record all identifying markings found on the parts of each assembly. The Contractor must maintain traceability of these markings to each unit throughout refurbishment. 3.1.2 IDENTIFYING MARKINGS - Part must have a MIC (Material Identification a and Control) code, heat/heat lot code, or unique Contractor traceability number/code that is visible on the part. See Material Traceability in paragraph 3 (Quality Assurance Provisions) of this contract for traceability requirements. The MIC code can consist of a 2, 3, or 4 letter material identifier, 4 or 5 digit Julian date, 3 digit lot serial number, and Certifying Activity Designator (CAD) which will be 1 or 2 letters; the 4 parts are normally separated by hyphens; examples: TIA-3089-30-QQ and ST-06262-506-A. 3.1.3 RE-USEABLE PARTS - - Any parts of the original assembly that are useable (replacement is not necessary), that are properly marked as identified above, and that have material certifications available may be utilized as initially supplied. Certifications are not required to be resubmitted by the contractor. - Any parts of the original assembly that are useable (replacement is not necessary), are properly marked as identified above, but material certifications are not available at the contractor's facility, a waiver must be submitted in accordance with Waiver/Deviation (Configuration Control) requirements specified elsewhere in the Contract. 3.1.4 NON-USEABLE PARTS - -Any parts of the original assembly that are not properly marked as identified above must be replaced and the required certifications must be submitted. - Any parts of the original assembly that are not usable (replacement is necessary) must be replaced and the required certifications must be submitted. 3.1.5 REFURBISHMENT - Upon completion of inspection, this item must be refurbished to be in accordance with ;NAVSEA Drawing 845-7016077 with ER7016077B66, consisting of one Ball Item 2; one Seat Item 114; and one seat Item 115, and liability ER5959311C5; , except as amplified or modified herein. This applies to all "Parts Requiring Certification" as identified elsewhere in this Contract/Purchase Order. 3.1.6 ADDITIONAL SOW REQUIREMENTS - ;Balls which are not usable must be dispositioned and new balls are not to be manufactured under this contract.; 3.2 ;For seats, Items 114 and 115, dimension 1.562 inch nominal must be manufactured to 1.582 +/- 0.005 inch. The stack height requirement of ER7016077B66 does not apply.; 3.3 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: Part - ;Ball - Item 2; Material - Centrifugally cast 6AL-4V, ASTM-B367, Grade C-5, with mechanical properties as listed in Supplimentary Requirements S6 and S8. ;or ASTM-B381, Grade F-5 with the following modified mechanical properties: Ultimate Tensile Strength - 125,000 psi Minimum (Longitudinal direction) Elongation in 4D - 10% Minimum Yield Strength - 115,000 psi Minimum Reduction of Area Minimum 20%; Part - ;Seats (Q3) - Item 114 and Item 115; Material - MC903 (Type 6 cast nylon produced with polyepsilon caprolactam by the direct polymerization process) as manufactured by the Polymer Corporation or equal in accordance with Electric Boat Division Specification 2000. (Properties Specified Below Only) Item Property Test Method Value (A) Melting Point ASTM E794 or ASTM D3418 221 deg C +/- 9 (B) Relative Viscosity ASTM D789 (Notes 1 and 4) 2000 Minimum (C) Specific Gravity ASTM D792 1.15-1.17 at 23 deg C (D) Dimensional Change Notes 2 & 4 0.2% Maximum (E) Tensile Impact ASTM D1822 Type S 80 ft-lbs/in�2 Specimen (Notes 5 & 6) Minimum (Note 3) (F) Tensile Yield Stress ASTM D638 (Note 6) 9000 psi Min. (Note 3) (G) Compressive Strength^ ASTM D695 (Note 6) 9000 psi Min. (Note 3) ^(at 1 percent Offset) (H) Water Absorption 24 hour ASTM D570 1.3 percent Maximum Saturation ASTM D570 7.0 percent Maximum (I) Rockwell "M" Hardness ASTM D785 75 Minimum Note 1: The test specimen must be finely ground particulates. After immersion the material must be checked daily for dissolution and must dissolve no longer than one hundred twenty (120) hours from the start of immersion. Within twenty-four (24) hours of the test specimen determined to be fully dissolved, it must be tested for viscosity. Note 2: Dimensional stability testing must be performed in accordance with the dimensional stability method per ASTM D5989 or equivalent. The percent change in each dimension, outside diameter, inside diameter and thickness must not be greater than the value specified. Note 3: These values are minimum averages. Separate specimens results may vary by 25%. Note 4: Any change to an already established heat or annealing cycle to achieve both relative viscosity and/or dimensional stability must be presented to the procuring activity for approval along with justification for the change. Note 5: Tensile-impact test specimens are to be type S in accordance with ASTM D1822, or round cylindrical specimens in accordance with MIL-DTL-32286, Paragraph 3.8 Note 6: Prior to test, the specimens must be dried in accordance with Federal Specification L-P- 410A, Paragraph 4.4.5. 3.4 Testing Certification - Certifications are required for the following tests on the items listed below. Additional testing on other piece parts (if any) per applicable drawings and specifications is still required, but certifications are only required as listed below. Test - Non-Destructive Tests Item - ;Weld Repair and/or Production Weld (as applicable); Performance - Per applicable fabrication specification Acceptance - Per applicable fabrication specification 3.5 ;Ball outside diameter may be reworked to a minimum of 21.495 inches to refurbish the ball surface to meet drawing requirements and represents a relaxation below the drawing dimension. All other dimensions including Sphericity and concentricity apply. Balls which require reworking beyond the limitation specified herein are to be dispositioned as noted elsewhere in the contract. Defects in the Ball Stem Slot are acceptable if backlash between Ball and Stem does not exceed 5 degrees and defects must not exceed 0.050 inches in depth or cover more than 40 percent of the surface.; 3.6 Ball Spherical Surface Waviness - Unless otherwise specified on drawing, all sealing area surfaces must have a spherical surface waviness which does not exceed 0.0005 inches of height per inch of spherical surface. Roughness and waviness ratings must apply in a direction which yields the maximum rating, normally perpendicular to the lay. 3.7 ;Ball surface waviness must be verified prior to telflon coating.; 3.8 Chemours Company (formerly DuPont) Teflon Coating 850G-204 and 852G-201. Use of Chemours Company (formerly DuPont) Teflon Coating 851N-204 and 852N-201 is acceptable until exhausted - Teflon coating of ball(s) must be in accordance with general note ;2.C; of drawing ;803-5959311; . 3.8.1 Naval Ordnance Systems Command OD 10362 First Revision dated 15 Aug 1961 is provided by Contract Support Library Reference Number CSD018 in ECDS at https://register.nslc.navy.mil/ 3.9 A visual inspection shall be performed on the finished seat with acceptance criteria on critical surfaces per CSD167 in the ECDS (Electronic Contractor Data Submission) system at: https://register.nslc.navy.mil/. 3.10 Thread Inspection Requirements - All threads on threaded parts must be inspected using appropriate inspection methods, inspection systems, and inspection gages/instruments in accordance with FED-STD-H28 series. Substitution of thecommercial equivalent inspection in accordance with ASME B1 series is acceptable. 3.10.1 System 21 of FED-STD-H28/20 must be used as a minimum inspection requirement for threads when the design drawing or design specification does not specify an inspection requirement. 3.10.2 For Navy and Shipyard drawings, system 21 of FED-STD-H28/20 may be substituted for System 22 without further Navy approval when the design drawing invokes System 22 and does not cite governing specifications that specifically require system 22. System 22 of FED-STD-H28/20 must be used when the drawing references other governing specifications that specifically require System 22, such as certain thread types of MIL-DTL-1222. 3.10.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.11 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.12 Welding or Brazing - When welding, brazing, and allied processes are required, as invoked by Section C paragraph 3 requirements, they must be in accordance with S9074-AR-GIB-010A/278, 0900-LP-001-7000 for brazing of piping and pressure vessel applications, or S9074-AQ-GIB-010/248 for brazing of other applications. For all production and repair welding and brazing personnel and procedures must be qualified under S9074-AQ-GIB-010/248 or 0900-LP-001-7000, as applicable. Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing. 3.13 Configuration Control - The Contractor must maintain the total equipment baseline configuration. For items of proprietary design, Contractor drawings showing the latest assembly configuration must be provided to the Government in electronic (C4) format. Definitions are provided elsewhere in the Contract/Purchase Order. 3.13.1 Waivers/Deviations - All waivers and deviations, regardless of significance or classification require review and approval by the Contracting Officer. Waivers and Deviations must be designated as Critical, Major, or Minor. The Contractor must provide a copy of this request to the QAR. Requests must include the information listed below. a. A complete description of the contract requirement affected and the nature of the waiver/deviation (non-conformance), including a classification of Critical, Major, or Minor. b. Number of units (and serial/lot numbers) to be delivered in this configuration. c. Any impacts to logistics support elements (such as software, manuals, spares, tools, and similar) being utilized by Government personnel or impacts to the operational use of the product. d. Information about remedial action being taken to prevent reoccurrence of the non-conformance. 3.13.2 All requests for Waivers/Deviations on NAVSUP-WSS Contracts must be submitted to the NAVSUP WSS Contracting Specialist via eMail. 3.13.3 ECPs - The Government will maintain configuration control and change authority for all modifications or changes affecting form, fit, function, or interface parameters of the Equipment and its sub-assemblies. The Contractor must submit an Engineering Change Proposal (ECP) for any Class I or II changes that impact the Equipment covered by this contract. ECPs must be prepared in Contractor format, and must include the following information: a. The change priority, change classification (Class I or Class II), and change justification. b. A complete description of the change to be made and the need for that change. c. A complete listing of other Configuration Items impacted by the proposed change and a description of the impact on those CIs. d. Proposed changes to documents controlled by the Government. e. Proposed serial/lot number effectivities of units to be produced in, or retrofitted to, the proposed configuration. f. Recommendations about the way a retrofit should be accomplished. g. Impacts to any logistics support elements (such as software, …