BALL KIT, CERAMIC

CONTACT INFORMATION|4|N743.49|WVT|771-229-0573|benjamin.t.spangler.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 BENJAMIN.T.SPANGLER.CIV@US.NAVY.MIL| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| MANDATORY USE OF WORKFLOW PRO (WFP) MOD ASSIST MODULE|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)(JUL 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|||||||| 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|| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (DEVIATION 2026-O0043)(FEB 2026))|13|||||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||X| 1. DD1423 Data Items with title of "INSPECTION AND TEST PLAN" SUB TITLE "INSPECTION SYSTEM PROCEDURES" may be waived if already on file at NAVSUP WSS Mechanicsburg. 2. Portsmouth NSY's DODAAC has changed from N00102 to N50286. Any reference toN00102 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 137 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 in accordance with DFARS 252.204-7024. 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 SAM.gov 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 implemented shipping system or ATAC will be shipping/deliveringmaterial. 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 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. 2.2.2 Documents, drawings, and publications supplied are listed under "Drawing Number". These items should be retained until an award is made. 2.2.3 "Document References" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. DRAWING DATA=EB-2000 |96169| C|SP |D|0001 | C|49998|0484385 DRAWING DATA=4384676 |53711| C| |D|0001 | C|00026|0000000 DRAWING DATA=7016077 |53711| B| |D|0001 | B|49998|0175546 DRAWING DATA=7016077 |53711| B| |D|0002 | B|49998|0144180 DRAWING DATA=7016077 |53711| B| |D|0003 | B|49998|0157797 DRAWING DATA=7016077 |53711| B| |D|0004 | B|49998|0219730 DRAWING DATA=7016077 |53711| B| |D|0005 | B|49998|0175065 DRAWING DATA=7016077 |53711| B| |D|0005.1 | B|49998|0433181 DRAWING DATA=7016077 |53711| B| |D|0006 | B|49998|0137035 DRAWING DATA=7016077 |53711| B| |D|0007 | B|49998|0114084 DRAWING DATA=7016077 |53711| B| |D|0008 | B|49998|0149567 DRAWING DATA=7016077 |53711| B| |D|0009 | B|49998|0121920 DRAWING DATA=7016077 |53711| B| |D|0010 | B|49998|0169937 DRAWING DATA=7016077 |53711| B| |D|0011 | B|49998|0102221 DRAWING DATA=7016077 |53711| B| |D|0012 | B|49998|0076363 DRAWING DATA=7016077 |53711| B| |D|0013 | B|49998|0130062 DRAWING DATA=7016077 |53711| B| |D|0013.1 | B|49998|0055906 DRAWING DATA=7016077 |53711| B| |D|0014 | B|49998|0110930 DRAWING DATA=7016077 |53711| B| |D|0015 | B|49998|0157569 DRAWING DATA=7016077 |53711| B| |D|0016 | B|49998|0096892 DRAWING DATA=7016077 |53711| B| |D|0017 | B|49998|0105348 DRAWING DATA=7016077 |53711| B| |D|0018 | B|49998|0079948 DRAWING DATA=7016077 |53711| B| |D|0019 | B|49998|0106131 DRAWING DATA=7016077 |53711| B| |D|0020 | B|49998|0071311 DRAWING DATA=7016077 |53711| B| |D|0021 | B|49998|0091132 DRAWING DATA=7016077 |53711| B| |D|0022 | B|49998|0070819 DRAWING DATA=7016077 |53711| B| |D|0023 | B|49998|0110036 DRAWING DATA=7016077 |53711| B| |D|0024 | B|49998|0103251 DRAWING DATA=7016077 |53711| B| |D|0025 | B|49998|0124278 DRAWING DATA=7016077 |53711| B| |D|0026 | B|49998|0100543 DRAWING DATA=7016077 |53711| B| |D|0027 | B|49998|0139517 DRAWING DATA=7016077 |53711| B| |D|0028 | B|49998|0133775 DRAWING DATA=7016077 |53711| B| |D|0029 | B|49998|0092742 DRAWING DATA=7016077 |53711| B| |D|0030 | B|49998|0077445 DRAWING DATA=7016077 |53711| B| |D|0031 | B|49998|0094077 DRAWING DATA=7016077 |53711| B| |D|0032 | B|49998|0067914 DRAWING DATA=7016077 |53711| B| |D|0033 | B|49998|0094440 DRAWING DATA=7016077 |53711| B| |D|0034 | B|49998|0088128 DRAWING DATA=7016077 |53711| B| |D|0035 | B|49998|0078641 DRAWING DATA=7016077 |53711| B| |D|0036 | B|49998|0075186 DRAWING DATA=7016077 |53711| B| |D|0037 | B|49998|0071460 DRAWING DATA=7016077 |53711| B| |D|0038 | B|49998|0068639 DRAWING DATA=7016077 |53711| B| |D|0039 | B|49998|0078106 DRAWING DATA=7016077 |53711| B| |D|0040 | B|49998|0069474 DRAWING DATA=7016077 |53711| B| |D|0041 | B|49998|0077366 DRAWING DATA=7016077 |53711| B| |D|0042 | B|49998|0082080 DRAWING DATA=7016077 |53711| B| |D|0043 | B|49998|0098311 DRAWING DATA=7016077 |53711| B| |D|0044 | B|49998|0063930 DRAWING DATA=7016077 |53711| B| |D|0045 | B|49998|0139043 DRAWING DATA=7016077 |53711| B| |D|0046 | B|49998|0195681 DRAWING DATA=7016077 |53711| B| |D|0047 | B|49998|0112401 DRAWING DATA=7016077 |53711| B| |D|0048 | B|49998|0188714 DRAWING DATA=7016077 |53711| B| |D|0049 | B|49998|0091075 DRAWING DATA=7016077 |53711| B| |D|0050 | B|49998|0108246 DRAWING DATA=7016077 |53711| B| |D|0051 | B|49998|0085364 DRAWING DATA=7016077 |53711| B| |D|0052 | B|49998|0093309 DRAWING DATA=7016077 |53711| B| |D|0053 | B|49998|0101459 DRAWING DATA=7016077 |53711| B| |D|0054 | B|49998|0081213 DRAWING DATA=7016077 |53711| B| |D|0055 | B|49998|0087062 DRAWING DATA=7016077 |53711| B| |D|0056 | B|49998|0082649 DRAWING DATA=7016077 |53711| B| |D|0057 | B|49998|0077652 DRAWING DATA=7016077 |53711| B| |D|0058 | B|49998|0067483 DRAWING DATA=7016077 |53711| B| |D|0059 | B|49998|0085396 DRAWING DATA=7016077 |53711| B| |D|0060 | B|49998|0068904 DRAWING DATA=7016077 |53711|B9|1N |D|0001 |B9|49998|0040107 DRAWING DATA=7016077B147 |53711| A|ER |D|0001 | A|49998|0078803 DRAWING DATA=7016077B147 |53711| A|ER |D|0001.1 | A|49998|0071521 DRAWING DATA=7016077B147 |53711| A|ER |D|0001.2 | A|49998|0076275 DRAWING DATA=7016077B147 |53711| A|ER |D|0001.3 | A|49998|0085170 DRAWING DATA=7016077B147 |53711| A|ER |D|0001.4 | A|49998|0082066 DRAWING DATA=7016077B147 |53711| A|ER |D|0001.5 | A|49998|0026339 DRAWING DATA=7016077B147 |53711| A|ER |D|0001.6 | A|49998|0026274 DRAWING DATA=7016077B147 |53711| A|ER |D|0002 | A|49998|0230472 DRAWING DATA=7016077B165 |53711| A|ER |D|0001 | A|49998|3807537 DRAWING DATA=7016077B66 |53711| B|ER |D|0001 | B|00026|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 |060519|A| | | 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=T9074-AS-GIB-010/271 | | |1 |140911|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 ;Naval Ship Systems Command Drawing 845-7016077, ER7016077B66, ER7016077B147, and ER7016077B165 consisting of one Ball, Item 116 and one each mating Seats, Items 114 and 115; , 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 116; 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, Items 114 and 115 (Q3); Material - MC903 (Type 6 cast nylon produced with polyepsilon caprolactam by the direct polumerization process) as manufactured by the Polymer Corporation or equal in accordance with Electric Boat Division Specification 2000. (Properties Specified Below Only) ITEM PROPERTY ASTM TEST METHOD VALUE (A) Melting Point D789 221 deg C +/- 9 (430 deg F +/- 16) (B) Relative Viscosity D789 1500-6500 (RV is a unitless value, the RV test specimens must dissolve within a 120 hour period) (C) Specific Gravity D792 1.15 - 1.17 @ 23 deg C (73F) (D) Dimensional Change Note 1 .2% MAX (E) Tensile Impact D1822 80 FT-LB/SQ IN Type S Specimen Minimum Note 3 Note 2 (F) Tensile Yield Stress D638 9,000 PSI MIN Note 2 Note 3 (G) Compressive Strength D695 9,000 PIS MIN 1% Offset Note 2 Note 3 (H) Water Absorption D570 24 HR 1.3% MAX Saturation 7% MAX NOTES: 1. The test method to determine dimensional stability must be performed as follows: The test specimens must be measured at 23 deg C +/- 3 (73 deg F +/- 5) and placed in a mineral oil^ bath maintained 184 deg C +/- 3 (363 deg F +/- 5). The specimens must remain in the bath for six (6) hours at temperature and allowed to slow cool in the bath at a rate not to exceed 23 deg C +/- 3 (41 deg F +/- 5) per hour. When the bath reaches 23 deg C +/- 3 (73 def F +/- 5), the test specimens must be removed and measured. The percent change in each dimension, outside diameter, inside diameter and thickness must not be greater than the value specified. ^Mineral oil meets the specifications as listed below: Description..........................Passes U.S.P. Test (USP XX, P.1143) Solubility...........................Passes U.S.P. Test (USP XX, P.1143) Neutrality...........................Passes U.S.P. Test (USP XX, P.532) Readily Corbonizable Substances......Passes U.S.P. Test (USP XX, P.532) Limit of Polynuclear Compounds.......Passes U.S.P. Test (USP XX, P.532) Solid Parafin........................Passes U.S.P. Test (USP XX, P.532) Specific Gravity @ 25 deg C (77F)....0.8600 to 0.8900 Viscosity @ 37.8 deg C (100 F).......73.6 to 84.4 Centistokes (340-390 SUS) Flash Point Cleveland Open Cup.......420 deg F (216 C) (Typical) Refractive Index @ 20 deg C (68F)....1.480 (Typical) 2. Prior to test specimens must be conditioned as follows: The specimens must be subjected to a temperature of 71 deg C +/- 3 (160 deg F +/- 5) under a vacuum to a maximum of one millimeter absolute pressure until a change of less than .2% between two weighings sixteen (16) hours apart is achieved. 3. These values are minimum averages. Separate specimen values may not vary more than 25% under the specified minimum. 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 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 Alumina-Titania/PTFE coating of Ball(s) must be in accordance with A & A Company Specification Navy016 Rev L. Each Ball manufactured/repaired under this Order must be tagged with a durable non-metallic tag with thefollowing statement: "Ball coated with Alumina-Titania/PTFE coating per A & ACompany, South Plainfield New Jersey, proprietary procedure NAVY016 Rev L. This coating was approved by NAVSEA and these Balls are an approved replacement for the Ball, piece ;2; , of Naval Ship Systems Command Drawing ;845-7016077; ." 3.6 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/. 3.7 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. 3.8 ;Surface waviness must be verified after Grinding/Finishing of Alumina-Titania coating and before PTFE application. Surface finish of the Alumina-Titania coating, prior to PTFE application must be 32 Microinches.; 3.9 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 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 specifica