48--VALVE,BALL

Description

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|x||x|||||| STOP-WORK ORDER (AUG 1989)|1|| GENERAL INFORMATION-FOB-DESTINATION|1|b| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (JAN 2023)|16|Stand-Alone Receiving Report - Certifications Combo - Receiving Report & Invoice - Material ||TBD|N00104|TBD|TBD|N50286|TBD|||N/A|||||| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| MANDATORY USE OF WORKFLOW PRO (WFP) MOD ASSIST MODULE|1|| VALUE ENGINEERING (JUN 2020)|3|||| INTEGRITY OF UNIT PRICES (NOV 2021)|1|| EQUAL OPPORTUNITY FOR VETERANS (DEV 2026-O0040)(FEB 2026)|4||||| WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUNE 2003)|6|one year from date of delivery|one year from date of delivery||||| EQUAL OPPORTUNITY FOR WORKERS WITH DISABILITIES (DEV 2026-O0040)(FEB 2026)|4||||| TRANSPORTATION OF SUPPLIES BY SEA (OCT 2024)|2||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM-BASIC (FEB 2024)|11|||||||||||| NOTICE OF CYBERSECURITY MATURITY MODEL CERTIFICATION LEVEL REQUIREMENTS (NOV 2025))|1|| WARRANTY OF DATA-BASIC (DEVIATION 2026-O0035) (FEB 2026)|2||| PROGRESS PAYMENTS (DEVIATION 2026-O0022)(FEB 2026)|4||||| NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (DEV 2026-O0037)(FEB 2026)|1|| SECURITY PROHIBITIONS AND EXCLUSIONS (CLASS DEVIATION 2026-O0025)(FEB 2026)|7|||||||| LIST OF AWARD ATTACHMENTS|5|||||| 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|||||||||||||| ROYALTY INFORMATION (APR 1984)|1|| COST ACCOUNTING STANDARDS NOTICES AND CERTIFICATION (DEV 2026-O0006)(FEB 2026)|1|| INSTRUCTIONS TO OFFERORS -- COMPETITIVE ACQUISITION (DEV 2026-O0048)(MAR 2026)|2||| TYPE OF CONTRACT (DEV 2026-O0045)(MAR 2026)|1|FFP| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||x| ONLY ONE OFFER (DEVIATION 2026-O0048)(MAR 2026)|1|| This amendment is being issued to remove WSSTERMMZ01. 1.This is a procurement for the Level One Program. 2.DD1423 Data Item A001 (Inspection and Test Plan) may be waived if already on file at NAVSUP WSS Mechanicsburg. 3.Drawings can be accessed thru: sam.gov. 4.All contractual documents (i.e. contracts, purchase orders, task orders, delivery orders, and modifications) related to the instant procurement are considered to be "issued" by the Government when copies are either deposited in the mail, transmitted by facsimile, or sent by other electronic commerce methods such as email. The Government's acceptance of the contractor's proposal constitutes bilateral agreement to "issue" contractual documents as detailed herein. 5.Partial and early delivery of requirement is authorized and desired and is at no additional cost to either the vendor or the Government. 6.NAVSUP WSS will be considering past performance in the evaluation of offers. See Clause 252.204-7024. 7.This award will be issued bilaterally, requiring the contractor's written acceptance prior to execution. 8.This is a rated order certified for national defense use and the Contractor will follow all requirements of the Defense Priorities and Allocations System Regulation (15 CFR 700), see clause 52.211-14. 9.NECO bids will not be accepted, offers must include original RFP and email it to michael.e.thoman2.civ@us.navy.mil 10. Offerors must have a valid U.S. security clearance of confidential orhigher in order to respond to this RFP (N0010426RZB51), because the RFPincludes anannex classified at the confidential level which will be releasedonly to offerors possessing the appropriate clearance. All classified materialmust be handled in accordance with the National Industrial Security ProgramOperating Manual(NISPOM) (32 CFR Part 117).11.The following proposed deliveryschedule applies: 11.The following proposed delivery schedule applies: Submission of all certification data CDRLS 20 days prior to delivery. PNSY review/acceptance of certification CDRLS 18 working days after receipt. Final delivery of material (800 days) 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 Identification of Classified Documents - This contract/purchase order requires the Contractor to have authorized access to classified documents in accordance with the attached Contract Security Classification Specification (DD Form 254). The classified documents and security level are: ;4384676 - CONFIDENTIAL; 2.3 Applicable Documents - The document(s) listed below form a part of this contract/purchase order including modifications or exclusions. 2.3.1 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. 2.3.2 Documents, drawings, and publications supplied are listed under "Drawing Number". These items should be retained until an award is made. 2.3.3 "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| | | | DRAWING DATA=EB-2937 |96169| B|SP |D| | | | DRAWING DATA=H553-7801B11 |53711| A|ER |D| | | | DRAWING DATA=H553-7801B111 |53711| A|ER |D| | | | DRAWING DATA=H553-7801B124 |53711| A|ER |D| | | | DRAWING DATA=H553-7801B134 |53711| A|ER |D| | | | DRAWING DATA=H553-7801B147 |53711| A|ER |D| | | | DRAWING DATA=H553-7801B182 |53711| A|ER |D| | | | DRAWING DATA=H553-7801B20 |53711| A|ER |D| | | | DRAWING DATA=H553-7801B21 |53711| A|ER |D| | | | DRAWING DATA=H553-7801B226 |53711| A|ER |D| | | | DRAWING DATA=H553-7801B256 |53711| A|ER |D| | | | DRAWING DATA=H553-7801B274 |53711| B|ER |D| | | | DRAWING DATA=H553-7801B3 |53711| A|ER |D| | | | DRAWING DATA=H553-7801B318 |53711| A|ER |D| | | | DRAWING DATA=H553-7801B329 |53711| A|ER |D| | | | DRAWING DATA=H553-7801B340 |53711| B|ER |D| | | | DRAWING DATA=H553-7801B38 |53711| B|ER |D| | | | DRAWING DATA=H553-7801B408 |53711| A|ER |D| | | | DRAWING DATA=H553-7801B454 |53711| A|ER |D| | | | DRAWING DATA=H553-7801B54 |53711| A|ER |D| | | | DRAWING DATA=H553-7801B545 |53711| A|ER |D| | | | DRAWING DATA=H553-7801B60 |53711| B|ER |D| | | | DRAWING DATA=H553-7801B64 |53711| A|ER |D| | | | DRAWING DATA=H553-7801B66 |53711| A|ER |D| | | | DRAWING DATA=H553-7801B67 |53711| A|ER |D| | | | DRAWING DATA=4384676 |53711| C| |D| | | | DRAWING DATA=4677382 |53711| C| |D| | | | DRAWING DATA=5959311 |53711| C| |D| | | | DRAWING DATA=5959311C5 |53711| A|ER |D| | | | DRAWING DATA=6985328 |53711| B| |D| | | | DRAWING DATA=7016077 |53711| B|DW |D| | | | DRAWING DATA=7016077B105 |53711| A|ER |D| | | | DRAWING DATA=7016077B108 |53711| A|ER |D| | | | DRAWING DATA=7016077B113 |53711| A|ER |D| | | | DRAWING DATA=7016077B115 |53711| A|ER |D| | | | DRAWING DATA=7016077B119 |53711| A|ER |D| | | | DRAWING DATA=7016077B129 |53711| A|ER |D| | | | DRAWING DATA=7016077B132 |53711| A|ER |D| | | | DRAWING DATA=7016077B137 |53711| A|ER |D| | | | DRAWING DATA=7016077B150 |53711| A|ER |D| | | | DRAWING DATA=7016077B152 |53711| A|ER |D| | | | DRAWING DATA=7016077B156 |53711| A|ER |D| | | | DRAWING DATA=7016077B160 |53711| B|ER |D| | | | DRAWING DATA=7016077B162 |53711| A|ER |D| | | | DRAWING DATA=7016077B163 |53711| A|ER |D| | | | DRAWING DATA=7016077B165 |53711| A|ER |D| | | | DRAWING DATA=7016077B173 |53711| A|ER |D| | | | DRAWING DATA=7016077B174 |53711| A|ER |D| | | | DRAWING DATA=7016077B177 |53711| A|ER |D| | | | DRAWING DATA=7016077B194 |53711| A|ER |D| | | | DRAWING DATA=7016077B198 |53711| A|ER |D| | | | DRAWING DATA=7016077B2 |53711| A|ER |D| | | | DRAWING DATA=7016077B205 |53711| B|ER |D| | | | DRAWING DATA=7016077B22 |53711| A|ER |D| | | | DRAWING DATA=7016077B30 |53711| A|ER |D| | | | DRAWING DATA=7016077B39 |53711| C|ER |D| | | | DRAWING DATA=7016077B41 |53711| A|ER |D| | | | DRAWING DATA=7016077B57 |53711| B|ER |D| | | | DRAWING DATA=7016077B66 |53711| B|ER |D| | | | DRAWING DATA=7016077B73 |53711| A|ER |D| | | | DRAWING DATA=7016077B76 |53711| A|ER |D| | | | DRAWING DATA=7016077B81 |53711| A|ER |D| | | | DRAWING DATA=7016077B83 |53711| A|ER |D| | | | DRAWING DATA=7016077B9 |53711| A|ER |D| | | | DRAWING DATA=7016077B93 |53711| A|ER |D| | | | DRAWING DATA=7016077B98 |53711| A|ER |D| | | | DRAWING DATA=7016077B99 |53711| A|ER |D| | | | DRAWING DATA=7069126 |53711| A|DW |D| | | | DRAWING DATA=7069126A10 |53711| A|ER |D| | | | DRAWING DATA=7069126A12 |53711| A|ER |D| | | | DRAWING DATA=7069126A3 |53711| A|ER |D| | | | DRAWING DATA=7069126A4 |53711| A|ER |D| | | | DRAWING DATA=7069126A6 |53711| A|ER |D| | | | DRAWING DATA=7069126A8 |53711| A|ER |D| | | | DRAWING DATA=7069127 |53711| A|DW |D| | | | DRAWING DATA=7069127A10 |53711| B|ER |D| | | | DRAWING DATA=7069127A5 |53711| A|ER |D| | | | DRAWING DATA=7069127A7 |53711| A|ER |D| | | | DRAWING DATA=7069127A9 |53711| A|ER |D| | | | 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=QQ-N-281 | | |D |851023|A|2 | | DOCUMENT REF DATA=QQ-N-286 | | |G |001207|A| | | DOCUMENT REF DATA=ASTM-B381 | | | |130701|A| | | DOCUMENT REF DATA=ASTM-B564 | | | |220401|A| | | DOCUMENT REF DATA=ASTM-D638 | | | |100315|A| | | DOCUMENT REF DATA=ASTM-D792 | | | |200701|A| | | DOCUMENT REF DATA=MIL-STD-792 | | |F |230223|A| |01| DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | | DOCUMENT REF DATA=ASTM-E1417 | | | |160615|A| | | DOCUMENT REF DATA=ASTM-E1444 | | | |160601|A| | | DOCUMENT REF DATA=MIL-STD-2035 | | |A |950515|A| | | DOCUMENT REF DATA=MIL-STD-2132 | | |D |080310|F| |01| DOCUMENT REF DATA=SAE AMS 2631 | | |G |220701|A| | | DOCUMENT REF DATA=EB/GD SPEC 2937 | | |B |900906|A| | | DOCUMENT REF DATA=ASTM-D4066 | | | |130701|A| | | DOCUMENT REF DATA=SAE AMS 6931 | | |D |171201|A| | | DOCUMENT REF DATA=ISO_9001 | | | |081115|A| | | DOCUMENT REF DATA=ISO10012 | | | |030415|A| | | DOCUMENT REF DATA=MIL-DTL-15024 | | |G |180303|A| | | DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | | DOCUMENT REF DATA=QPL 25027 | | |17 |000207|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=AIA/NAS NASM 25027 | | |1 |121221|A| | | 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=T9074-AD-GIB-010/1688 | | |1 |120713|A| | | DOCUMENT REF DATA=S9074-AR-GIB-010A/278 (CHG A) | | | |130214|A| | | DOCUMENT REF DATA=T9074-BD-GIB-010/0300 | | |2 |121218|A| | | 3. REQUIREMENTS 3.1 ;The 12 inch Hull and Backup Ball Valve must be in accordance with Naval Sea Systems Command Drawing 6985328 Assembly "C" and all invoked DRNs and liabilities included with this contract/purchase order, except as amplified or modified herein.; 3.2 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: Part - ;Body, Part Number 90-1C, with details on drawing 7016077 (Item 90-1); Material - ;T9074-BD-GIB-010/0300, Appendix E, Grade HY-100; Part - ;Safe End, Part Number 90-4C, with details on drawing 7016077 (Item-90-4); Material - ;EB SPEC 2937 or ASTM-B564, alloy UNS N06625 (In accordance with Supplementary Note S2.A. on Drawing 7016077); Part - ;Upper Bushing, Part Number 90-6C, with details on drawing 7016077 (Item 90-6); Material - ;ASTM-B564, Alloy UNS N10276 (In accordance with Supplementary Note S2.A. on Drawing 7016077); Part - ;Ball, Item 123C, with details on drawing 7016077 (Item 120); Material - ;Forged 6AL-4V to SAE-AMS-6931 (In accordance with Supplementary Note S2.B. on Drawing 7016077) 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) - Part Numbers 114 and 115, with details on drawing 7016077 (Items 114 and 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. Part - ;Access Cover, Part Number 4C, with details on drawing 7016077 (Item 4); Material - ;EB SPEC 2937 or ASTM-B564, alloy UNS N06625 (In accordance with Supplementary Note S2.A. on Drawing 7016077); Part - ;Stems, Part Number 5C, with details on drawing 7016077 (Item 5); and Part Number 107C, with details on drawing 7016077 (Item 107); Material - ;SAE AMS 6931, composition TI-6AL-4V, (In accordance with Supplementary Note S2.B. on Drawing 7016077); Part - ;Stud, Continuous Thread, Part Number 8C, modified to drawing note 7027 and with details on drawing 7016077 (Item 8); Material - ;QQ-N-286; PART - ;Nut, Self Locking, Part Number 9, with details on drawing 7016077 (Item 9); MATERIAL - QQ-N-281, class A annealed (hot finished or cold drawn) or class B cold drawn. All material must be from the same class. SELF-LOCKING ELEMENT- ASTM-D4066, Group 01, Class 1, Grade 1 Part - ;Disc, Part Number 14C, with details on drawing 7016077 (Item 14); Material - ;EB SPEC 2937 or ASTM-B564, alloy UNS N06625 (In accordance with Supplementary Note S2.A. on Drawing 7016077); 3.3 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 - ;Ultrasonic Inspection for Soundness (Prior to any machining); Item - ;Body, Part Number 90-1C (100% of each Body); Performance - ;T9074-BD-GIB-010/0300 Appendix E; Acceptance - ;T9074-BD-GIB-010/0300 Appendix E; Test - ;Magnetic Particle Inspection (After final machining); Item - ;Body, Part Number 90-1C; Performance - ;T9074-AD-GIB-010/1688; Acceptance - ;T9074-AD-GIB-010/1688; Test - ;Ultrasonic Inspection on Starting Material; Item - ;Ball, Part Number 123C; Performance - ;SAE-AMS-2631 Class B; Acceptance - ;SAE-AMS-2631 Class B; Test - ;Ultrasonic Inspection (before final machining); Item - ;Stems, Part Numbers 5C and 107C; Performance - ;SAE AMS-6931 and SAE AMS-2631; Acceptance - ;SAE AMS-2631; Test - ;Dye Penetrant Inspection (after final machining); Item - ;Stems, Part Numbers 5C and 107C; Performance - T9074-AS-GIB-010/271 Acceptance - MIL-STD-2035 Test - ;Ultrasonic Inspection (prior to machining); Item - ;Access Cover, Part Number 4C; Disc, Part Number 14C; Safe End, Part Number 90-4C; Upper Bushing, Part Number 90-6C; Performance - ;Supplementary note S2.A.(5).(A) of drawing 7016077; Acceptance - ;Supplementary note S2.A.(5).(A) of drawing 7016077; Test - ;Dye Penetrant Inspection (after final machining); Item - ;Access Cover, Part Number 4C; Disc, Part Number 14C; Safe End, Part Number 90-4C; Upper Bushing, Part Number 90-6C; Performance - ;T9074-AS-GIB-010/271 and Supplementary note S4.D of drawing 7016077; Acceptance - ;Supplementary note S2.A.(5).(B) of drawing 7016077; Test - ;Liquid Penetrant Inspection; Item - ;Stud, Continuous Thread, Part Number 8C; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Test - ;Dye Penetrant Inspection for Non-Magnetic Grades; Item - ;Nut, Part Number 9; Performance - T9074-AS-GIB-010/271 or ASTM-E1417/ASTM-E1444 (Method C solvent removal techniques must not be used on thread) Acceptance - ;NASM25027; Attribute - Annealing and Age Hardening Item - ;Stud, Continuous Thread, Part Number 8C; Performance - QQ-N-286 Test - ;Alloy Identity Test; Item - ;Access Cover, Part Number 4C; Disc, Part Number 14C; Safe End, Part Number 90-4C; Performance - ;Paragraph 4.6 of Electric Boat Specification 2937; Acceptance - ;Paragraph 4.6 of Electric Boat Specification 2937; Test - Ultrasonic Inspection on Starting Material Item - ;All Items requiring certification made from QQ-N-286 with a diameter or minimum distance between parallel surfaces of 4 inches or greater of the starting material, or when required by a drawing or specification invoked elsewhere in this contract; Performance - T9074-AS-GIB-010/271 or MIL-STD-2132, and QQ-N-286 Acceptance - QQ-N-286 Test - Quality Conformance Tests Item - Self-Locking Nuts Performance - ;NASM25027; Acceptance - ;NASM25027; Attribute - Certificate of Completion Item - Self-Locking Nut Nonmetallic Insert Performance - ;ASTM-D4066, Group 01, Class 1, Grade 1; Attribute - Certificate of Compliance Item - Self-Locking Nuts Performance - This Certificate must state that self-locking nuts were manufactured by an approved source. Approved sources are those listed on QPL-25027 for the appropriate fastener. This QPL may also be considered as approved sources for Heavy Hex self-locking nuts. Test - Pressure Tests Item - Each Assembly Performance - ;Supplementary Note S5 of Drawing 7016077; Acceptance - ;Supplementary Note S5 of Drawing 7016077; Test - Non-Destructive Tests Item - ;Weld Repair (as applicable); Performance - Per applicable fabrication specification Acceptance - Per applicable fabrication specification Test - Quality Conformance/Compliance Inspection Item - ;HY-100 starting material; Performance - ;T9074-BD-GIB-010/0300; Acceptance - ;T9074-BD-GIB-010/0300; Attribute - ;Eddy Current Test; Item - ;Cladding Thickness for joints: J0207, J0210, J0218, and J0219; Performance - ;Supplementary Note S3.E.(5).(A) of drawing 7016077; Test - ;Visual and Magnetic Particle Inspection (Root and Final Layer); Item - ;Joints: J0201, J0202, J0203, J0204, J0205 and J0206; Performance - ;T9074-AD-GIB-010/1688; Acceptance - ;T9074-AD-GIB-010/1688; Test - ;Visual and Dye Penetrant Inspection (Final Layer After Machining) (Cladding); Item - ;Joints: J0207, J0208, J0209; Performance - ;T9074-AD-GIB-010/1688; Acceptance - ;MIL-STD-2035, Class 2; Test - ;Visual and Dye Penetrant Inspection (Final Layer After Machining) (Cladding); Item - ;Joint: J0210; Performance - ;T9074-AD-GIB-010/1688; Acceptance - ;MIL-STD-2035, Class 2; Test - ;Dye Penetrant Inspection (Root); Item - ;Joints: J0211 and J0216; Performance - ;T9074-AD-GIB-010/1688; Acceptance - ;T9074-AD-GIB-010/1688; Test - ;Visual and Dye Penetrant Inspection (Final Layer); Item - ;Joints: J0211 and J0216; Performance - ;T9074-AD-GIB-010/1688; Acceptance - ;T9074-AD-GIB-010/1688; Test - ;Visual and Dye Penetrant Inspection (Root and Final Layer) (Cladding); Item - ;Joints: J0212, J0213; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;MIL-STD-2035, Class 2; Test - ;Visual and Dye Penetrant Inspection (Root and Final Layer) (Cladding); Item - ;Joints: J0214 and J0215; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;MIL-STD-2035, Class 1; Test - ;Visual and Dye Penetrant Inspection (Root); Item - ;Joint: J0217; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;MIL-STD-2035, Class 1; Test - ;Visual and Dye Penetrant Inspection of Inner diameter and Outer Diameter (After Machining); Item - ;Joint: J0217; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;MIL-STD-2035, Class 1; Test - ;Visual and Dye Penetrant Inspection (Final Layer After Machining) (Cladding); Item - ;Joints: J0218 and J0219; Performance - ;T9074-AD-GIB-010/1688; Acceptance - ;T9074-AD-GIB-010/1688; Test - ;Visual and Dye Penetrant Inspection (Final Layer After Machining) (Cladding); Item - ;Joints: J0220 and J0221; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;MIL-STD-2035, Class 1; Test - ;Dye Penetrant Inspection of Inner diameter and Outer Diameter (After Machining); Item - ;Joint: J0222; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;MIL-STD-2035, Class 2; 3.4 The pressure tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure tolerances are not provided by drawings, specifications or specified elsewhere in this contract, the following must be used: For pressure tests below 100 PSIG, the pressure tolerance must be +1 PSIG / -0 PSIG. For pressure tests at or above 100 PSIG up to and including 2500 PSIG, the pressure tolerance must be +2% / -0 PSIG rounded off to the nearest multiple of the smallest graduation on an analog test pressure gauge, not to exceed 50 PSIG. For pressure tests above 2500 PSIG, the pressure tolerance must be +2% / -0 PSIG, rounded off to the nearest multiple of the smallest graduation on an analog test pressure gauge, not to exceed 200 PSIG. The pressure test time tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure test time tolerances are not provided by drawings, specifications or specified elsewhere in this contract, the following must be used: For a test duration up to and including 1 hour, the tolerance must be +5 minutes / - 0 minutes. For a test duration of more than 1 hour up to and including 24 hours, the tolerance must be +30 minutes / - 0 minutes. For a test duration of more than 24 hours, the tolerance must be +60 minutes / - 0 minutes. 3.5 Radiography is required on ;Joint J0217 and must be identified to the weld joint; . 3.6 ;NAVSEA letter 08M/90-08645 dated 10 May 1990 is not necessary for the subject contract.; 3.7 Confidential Hydrostatic Test Pressures - When test pressures are confidential, certification must reference ;4384676 Revision C; and the item number to which the item was tested in lieu of the actual pressures. Any drawing requirement to mark the working pressure on the item does not apply and is strictly prohibited. 3.8 ;The seat thickness must be 1.582 +/- 0.005 inches for Seats, Part Numbers 114 and 115 on drawing 6985328. The stack height requirement of ER7016077B66 does not apply.; 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 ;Applicable portion of Stem, Part Number 107C, must be Teflon coated in accordance with note 2.C. of General Notes Drawing 5959311.; 3.11 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. 3.12 ;Surface waviness must be verified prior to Teflon coating.; 3.13 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 ;5959311; . 3.13.1 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/ 3.13.2 CSD099 provides guidance for acceptance/rejection of teflon-coated valve balls after valve assembly production testing. 3.14 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number ;CSD099; in ECDS at https://register.nslc.navy.mil/ 3.15 First Article Approval (Contractor Testing) - First Article Test (FAT) and approval is required. 3.16 Forging Sketches and FAT for Forgings - Forging Sketches and First Article Testing for forgings are required for ;Safe End, Part Number 90-4C, Upper Bushing, Part Number 90-6C, Access Cover, Part Number 4C and Disc, Part Number 14C; per ;Supplementary Notes S2.A.(2) and S2.A.(3) of Drawing 7016077; . 3.17 Component Identification Description (CID) - When applicable drawing(s) and/or specification(s) specify that a nameplate or identification plate is required, the CID number ( ;CID 88A100240X; ) must be added. When no plate is specified, an identification plate in accordance with MIL-DTL-15024, Type "C" on brass or Type "H" on aluminum must be securely attached to each assembly showing the above CID number. No assembly must be shipped without the CID number attached. 3.18 K-MONEL Fasteners - Material must be heat treated per QQ-N-286. 3.18.1 Fasteners that have been hot or cold headed or roll threaded must be solution annealed followed by age hardening subsequent to all heading and thread rolling operations. The mechanical properties on certifications must be actual properties of the annealed and age hardened material and must meet the requirements of QQ-N-286. 3.18.2 QQ-N-286 fasteners that have been headed and/or roll threaded must not beage hardened unless the material has been solution annealed subsequent to the heading and threading operations. Threads formed after the final age hardening heat treatment must be cut or ground only. 3.19 K-MONEL Fasteners - K-MONEL externally threaded fasteners must have mechanical properties determined in accordance with MIL-DTL-1222. Test results must include Tensile, Yield, Elongation and Hardness as required by MIL-DTL-1222. (The Hardness tests must be performed on a full size fastener.) 3.19.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222. 3.19.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order. 3.20 Slow Strain Rate Tensile Test Laboratories - The Slow Strain Rate Tensile Test of QQ-N-286 must be performed by one of the following laboratories: Huntington Alloys, a Special Metals Company Attn: Bill Bolenr 3200 Riverside Drive Huntington, WV 257059 Phone: (304) 526-5889 FAX: (304) 526-5973 Metallurgical Consultants, Inc. Attn: W. M. Buehler 4820 Caroline PO Box 88046 Houston, TX 77288-0046 Phone: (713) 526-6351 FAX: (713) 526-2964 Naval Surface Warfare Center, Carderock Division Attn: Eric Focht Code 614 9500 Macarthur Blvd West Bethesda, MD 20817-5700 Phone: (301) 227-5032 FAX: (301) 227-5576 Teledyne Allvac Attn: Dr. W. D. Cao 2020 Ashcraft Ave. Monroe, NC 28110 Phone: (704) 289-4511 FAX: (704) 289-4269 Westmoreland Mechanical Testing and Research Inc. Attn: Andrew Wisniewski P.O. Box 388 Youngstown, PA 15696-0388 Mannesmann Rohrenwerke Mannesmann Forschungsinstitut (MFI) Attn: Dr. Weiss Postfach 251160 47251 Duisburg Germany Phone: 011-49-0203-9993194 FAX: 011-49-0203-9994415 ThyssenKrupp VDM USA, Inc. Attn: D. C. Agarwal 11210 Steeplecrest Drive, Suite 120 Houston, TX 77065-4939 Phone: (281) 955-6683 3.21 Thread Forming - The following provides the official interpretation of paragraph 4.5.2.7 of MIL-DTL-1222. 3.21.1 In order to qualify for "Alternate Mechanical Testing" found in MIL-DTL-1222J paragraph 4.5.2.7 and utilize the mechanical properties for the starting bar stock in lieu of performing yield strength or proof stress testing on finished fasteners, all of the subsequent provisions found in MIL-DTL-1222J paragraphs 4.5.2.7 a through e must be met. If any single provision is not met, all required mechanical testing must be performed on the finished full sized fasteners. These provisions are explained as follows: a. Proper product lot control and traceability must be in place. b. No heat treatment (including hot heading and hot forming), cold forming, drawing, rolling and thread rolling may be performed on the starting bar, fastener blanks or finished fasteners after the completion of the mechanical testing on the starting bar. c. and d. The proper size starting bar must be selected to ensure mechanical properties of finished fasteners are represented by the mechanical properties of the starting bar. e. The mandatory testing, axial tensile (studs) and wedge tensile (screws and bolts) must be performed on full sized fasteners. Note that there is a typographical error in paragraph 4.5.2.7 and that the axial load test is a mandatory test that must be performed on studs as required in paragraph 4.5.2.7.e. 3.21.2 Thread rolling is a cold working process and is not considered to be a machining ...