SAMDaily.us | PRESOL | 48 | 48--VALVE ASSEMBLY,MANI

SAMDAILY.US - ISSUE OF OCTOBER 24, 2025 SAM #8733
SOLICITATION NOTICE

48 -- 48--VALVE ASSEMBLY,MANI

Notice Date: 10/22/2025 12:56:18 AM
Notice Type: Solicitation
NAICS: 332919 — Other Metal Valve and Pipe Fitting Manufacturing
Contracting Office: NAVSUP WEAPON SYSTEMS SUPPORT MECH MECHANICSBURG PA 17050-0788 USA
ZIP Code: 17050-0788
Solicitation Number: N0010425RFD37
Response Due: 11/10/2025 10:00:00 AM
Archive Date: 11/25/2025
Point of Contact: Electronic Mail: BENJAMIN.SPANGLER@NAVY.MIL
E-Mail Address: BENJAMIN.SPANGLER@NAVY.MIL
(BENJAMIN.SPANGLER@NAVY.MIL)
Description: CONTACT INFORMATION|4|N743.49|WVD|7176052147|benjamin.t.spangler.civ@us.navy.mil| ITEM UNIQUE IDENTIFICATION AND VALUATION (JAN 2023)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP REVIEW FEB 1991)(FEB 1999)|1|See specification sections C and E.| INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2||| DESIRED AND REQUIRED TIME OF DELIVERY (JUNE 1997)|29|0001AA|10|730|0001AB|10|730|||||||||||||||||||||||| 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 |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|| VALUE ENGINEERING (JUN 2020)|3|||| INTEGRITY OF UNIT PRICES (NOV 2021)|1|| EQUAL OPPORTUNITY FOR VETERANS (JUN 2020)|4||||| WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUNE 2003)|6|One year from date of delivery.|One year from date of delivery.||||| WARRANTY OF DATA--BASIC (MAR 2014)|2||| SMALL BUSINESS SUBCONTRACTING PLAN (JAN 2025)|4||||| EQUAL OPPORTUNITY FOR WORKERS WITH DISABILITIES (JUN 2020)|2||| TRANSPORTATION OF SUPPLIES BY SEA (OCT 2024)|2||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM-BASIC (FEB 2024)|11|||||||||||| PROGRESS PAYMENTS (NOV 2021)|4||||| REQUIREMENTS FOR CERTIFIED COST OR PRICING DATA AND DATA OTHER THAN CERTIFIED COST OR PRICING DATA-MODIFICATIONS (NOV 2021))|7|||||||| LIST OF AWARD ATTACHMENTS|5|||X|X|| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (OCT 2024)|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|| ROYALTY INFORMATION (APR 1984)|1|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAR 2025)(DEVIATION 2025-O0003 AND2025-O0004))|13|332919|750|||||||||||| COST ACCOUNTING STANDARDS NOTICES AND CERTIFICATION (DEVIATION 2018-O0015)(MAY 2018))|1|| REQUIREMENTS FOR SUBMISSION OF PROPOSALS VIA ELECTRONIC MEDIA (JAN 2018)|1|Electronic mail| TYPE OF CONTRACT (APR 1984)|1|Firm Fixed Price| ALTERATIONS IN SOLICITATION (APR 1984)|3|||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||X| REQUIREMENTS FOR CERTIFIED COST OR PRICING DATA AND DATA OTHER THAN CERTIFIEDCOST OR PRICING DATA (MAY 2024))|1|| This amendment is issued to update notes and clauses. Solicitation Note 5 updated to: If drawings are included in the solicitation, access needs to be requestedon the individual solicitation page on Contracts Opportunities on theGovernment's SAM.gov website. After requesting access, send an email to thePrimary POC 6. The complete RFP package must be signed and returned prior tothe closing date. Emailed or faxed proposals are acceptable. NECO quotes willNOT be accepted and will be determined non-responsive. \ 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 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 730 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. 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 6. The complete RFP package must be signed and returned prior to the closing date. Emailed or faxed proposals are acceptable. NECO quotes will NOT be accepted and will be determined non-responsive. \ 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 ""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 Documents, drawings, and publications supplied are listed under ""Drawing Number"". These items should be retained until an award is made. 2.2.4 The documents and drawings listed below under DRAWING NO. are not provided with this Contract/Purchase order. DRAWING NO CAGE REV DISTR CD ;281497-0003 99657 F B 236453 99657 G B 236454 99657 E B 234648 99657 R3 B 284027 99657 E B 236403-0001 99657 B B 284026-0002 99657 C B 234802 99657 C B ATP281497-0003 99657 C B; DRAWING DATA=EB-4147 |96169| B|SP |D|0001 | B|49998|9999999 DOCUMENT REF DATA=ASTM-B21 | | | |200401|A| | | DOCUMENT REF DATA=FED-STD-H28 | | |B |190424|A| | | DOCUMENT REF DATA=FED-STD-H28 |0020| |B |941221|A| |01| DOCUMENT REF DATA=FF-S-86 | | |G |210127|A| | | DOCUMENT REF DATA=ANSI/ASQ Z1.4 | | | |080101|A| | | DOCUMENT REF DATA=ASTM-B150 | | | |190401|A| | | DOCUMENT REF DATA=ASTM-B171 | | | |040501|A| | | DOCUMENT REF DATA=ASTM-A493 | | | |090401|A| | | DOCUMENT REF DATA=ASTM-A574 | | | |211201|A| | | DOCUMENT REF DATA=ASTM-A581 | | | |950910|A| | | DOCUMENT REF DATA=ASTM-A582 | | | |211101|A| | | DOCUMENT REF DATA=ASTM-F606 | | | |191115|A| | | DOCUMENT REF DATA=ASTM-B633 | | | |151201|A| | | DOCUMENT REF DATA=QQ-B-639 | | |C |160219|A| | | DOCUMENT REF DATA=MIL-STD-792 | | |F |060519|A| | | DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | | DOCUMENT REF DATA=SAE AMS 5640 | | |V |160201|A| | | DOCUMENT REF DATA=SAE AMS 5659 | | |S |160801|A| | | DOCUMENT REF DATA=MIL-S-7720 | | |A |740726|A| 2| | 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=MIL-DTL-16232 | | |H |200915|A| | | DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | | DOCUMENT REF DATA=MIL-PRF-27617 | | |G |110815|A| | | DOCUMENT REF DATA=MIL-I-45208 | | |A |810724|A| 1| | DOCUMENT REF DATA=MIL-STD-45662 | | |A |880801|A| | | DOCUMENT REF DATA=SAE AMS-QQ-S-763 | | |D |150301|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 ;Complete manifold assembly to be in accordance with Marotta drawing 281497-0003, less items 104, 105, and 73, 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: ;MAROTTA DRAWING 281497-0003 (MANIFOLD ASSEMBLY); Part - ;NUT-RETAINER, Item 17; NUT, Item 23; BONNET, Item 24; and COVER, Item 33; Material - ;CRES 300 series per SAE AMS-QQ-S-763 or ASTM-A581 or ASTM-A582 or SAE AMS 5640; Part - ;BODY, Item 18; Material - ;SAE AMS-QQ-S-763, class 304; Part - ;FITTING, Item 38; Material - ;SAE AMS 5659, UNS S15500, Condition H-1025; Part - ;SCREW, Item 89 and SCREW, Item 99; Material - ;Alloy steel per MIL-DTL-1222, grade A574 or 4340, zinc plated; ;MAROTTA DRAWING 236453 (FILTER WITH DP INDICATOR ASSEMBLY); Part - ;PLUG, Item 2; Material - ;CRES 300 series per SAE AMS-QQ-S-763 or ASTM-A581 or ASTM-A582 or SAE AMS 5640; Part - ;SCREW, Item 3; Material - ;CRES 300 per ASTM A493 or MIL-S-7720 in accordance with FF-S-86; Part - ;BOWL, Item 6; Material - ;ASTM-A582, Type 303; or SAE AMS 5640, Type 1; or SAE AMS-QQ-S-763, Class 304 or 316; Part - ;Delta pressure indicator cover and Delta Dyne Plug (Indicator), item 1; Material - ;CRES 300 series per ASTM-A582 or SAE AMS-QQ-S-763 or SAE AMS-5640; ;MAROTTA DRAWING 236454 (BALL VALVE AND SPACER ASSY 2 1/2"" IPS); Part - ;SCREW, CAP, SOCKET HEAD, Items 91 and 92; Material - ;Alloy steel per MIL-DTL-1222, grade A574 or 4340, zinc plated; ;MAROTTA DRAWING 234648 (BALL VALVE ASSY); Part - ;STEM, Item 6; Material - ;ASTM B150, Temper TQ 50; Part - ;BONNET, Item 8; Material - ;SAE AMS-QQ-S-763, Class 304; Part - ;Ball (Q3), Item 4; Material - ;SAE AMS-QQ-S-763, Class 304, Condition A; Part - ;Seat (Q3), Item 23; Material - Torlon 4503, 4203, or 4203L (unfilled polyamide-imide) per Electric Boat Specification 4147. (Certificate of Compliance only is required) ;OR; Part - ;Seat (Q3), Item 23; Material - Ultem 1000 (unreinforced polyetherimide) (Properties Specified Below Only) ITEM PROPERTY ASTM TEST METHOD VALUE (A) Tensile Strength D638 15,000 PSI MIN (B) Rockwell Hardness D785 M112 +/-4 (C) Specific Gravity D792 1.27 +/-.02 (D) Water Absorption D570 .25% MAX (24 Hours) (E) IZOD Impact Strength D256 .5 FT-LBS/IN MIN AVE. Notched 1/8"" Note: Seats supplied under this contract must be manufactured from one type of material only. Mixed quantities of seats manufactured from Torlon and Ultem are unacceptable. ;MAROTTA DRAWING 284027, ASSEMBLY 284027-0001 (HANDVALVE ASSEMBLY); Part - ;RETAINER-SCREW, Item 13 and CAGE, Item 17; Material - ;CRES 300 Series per SAE AMS-QQ-S-763 or ASTM-A581 or ASTM-A582 or SAE AMS 5640; Part - ;STEM, Item 15; Material - ;SAE AMS-QQ-S-763, Class 316, Condition A; ;MAROTTA DRAWING 236403-0001 (PILOT & SHUTTLE VALVE MANIFOLD ASSY); Part - ;RETAINER, Item 11; HSG-ORIFICE, Item 21; SCREW, Item 22; and NUT, Item 23; Material - ;CRES 300 series per SAE AMS-QQ-S-763 or ASTM-A581 or ASTM-A582 or SAE AMS 5640; Part - ;BODY, Item 30; Material - ;ASTM B21, UNS C46400, Temper H04 or H02 with the following minimum properties: Tensile Strength 58,000 PSI Yield Strength 30,000 PSI Elongation per ASTM B21 for the starting material size and temper; Part - ;SCREW, Items 67 and 68; Material - ;Alloy steel per MIL-DTL-1222, grade A574 or 4340, zinc plated; ;MAROTTA DRAWING 284027, ASSEMBLY 284027-0002 (HAND VALVE ASSY); Part - ;RETAINER-SCREW, Item 13 and CAGE, Item 17; Material - ;CRES 300 Series per SAE AMS-QQ-S-763 or ASTM-A581 or ASTM-A582 or SAE AMS 5640; Part - ;STEM, Item 15; Material - ;SAE AMS-QQ-S-763, Class 316, Condition A; ;MAROTTA DRAWING 284026-0002 (PILOT VALVE ASSY); Part - ;STEM, Item 19; Material - ;CRES Series 300 per SAE AMS-QQ-S-763 or ASTM-A581 or ASTM-A582 or SAE AMS 5640; Part - ;NUT, Item 29 and SLEEVE-RETAINING, Item 31; Material - ;ASTM-B21, alloy C46400, Temper H02; or ASTM-B171, alloy C46400; or QQ-B-639, alloy 464; Part - ;BODY, Item 28; Material - ;SAE AMS-QQ-S-763, class 316; ;MAROTTA DRAWING 234802 (ADAPTER AND SCREEN ASSY); Part - ;ADAPTER-BLOCK, Item 13; Material - ;ASTM-B21, alloy C46400, Temper H02; 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 - Intergranular Corrosion Test (Only for SAE-AMS-QQ-S-763, Classes 304-condition A, 304L, 316-condition A, 316L, 317-condition A, 321 and 347 material. Test must be performed prior to fabrication/machining) Item - ;Items 17, 18, 23, 24, and 33 of drawing 281497-0003; Items 1 (Delta pressure indicator cover and Delta Dyne Plug Indicator), 2, and 6 of drawing 236453; Items 4 and 8 of drawing 234648; Items 13, 15, and 17 of drawing 284027; Items 11, 21, 22, and 23 of drawing 236403-0001; Items 13, 15, and 17 of drawing 284027; Items 19 and 28 of drawing 284026-0002; Performance - SAE-AMS-QQ-S-763 Acceptance - SAE-AMS-QQ-S-763 Test - ;Liquid Penetrant Inspection or Magnetic Particle Inspection (Wet Method) (Either inspection is acceptable); Item - ;Items 91 and 92 of drawing 236454; Items 67 and 68 of drawing 236403-0001; items 89 and 99 of drawing 281497-0003; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Test - ;Liquid Penetrant Inspection; Item - ;Item 3 of drawing 236453; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Test - ;Acceptance Tests; Item - ;Each Manifold Assembly; Performance - ;ATP281497-0003; Acceptance - ;ATP281497-0003; Test - Non-Destructive Tests Item - ;Weld Repair and/or Production Weld (as applicable); Performance - Per applicable fabrication specification Acceptance - Per applicable fabrication specification 3.4 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/ 3.5 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. 3.6 FF-S-86 mechanical property and metallographic testing sample sizes must use ASQ Z1.4 Inspection Level S-1 with AQL = 1.0.NOTE: The sample size values must conform to FF-S-86E and earlier revisions. 3.7 Wedge Tensile Test Specimens (Headed fasteners) - A wedge tensile test must be conducted on a Full Size Fastener for each production lot and reported aspart of the Mechanical Properties. The required specimens for the Wedge Tensile Test must be separate fasteners from those required for the Yield Test. 3.7.1 Testing for Socket Head Cap Screws must be in accordance MIL-DTL-1222, paragraphs 4.5.2.3 and 4.5.2.3.1. 3.7.2 Testing for all other Headed Fasteners with a nominal diameter greater than 1/4-inch must be in accordance with ASTM-F606 for grades 5, 8, B7, and B16.For all other grades, the following wedge angles must be used. a. Except as specified in item c below, fasteners with a nominal diameter of 1/4-inch through 1-inch (inclusive) must be tested with a ten degree wedge. b. Except as specified in item c below, fasteners with a nominal diameter over 1-inch must be tested with a six degree wedge. c. Fasteners that are of grades 8, B7, B16, 410, 416, 416Se, 431, and 630 and are threaded within one diameter to the underside of the head must be tested as follows: Sizes 1/4 inch through 3/4 inch (inclusive) Use a six degree wedgeSizes over 3/4 inch Use a four degree wedge d. Fasteners which have passed testing with wedge angles greater than those specified should be considered acceptable. 3.7.3 For fasteners having a length less than the minimum specified in Table 1 of ASTM-F606, one ""test specimen fastener"" must be manufactured from each lot of fasteners and tested to represent that lot. The length of these test specimen fasteners must meet the minimum specified in table 1 of ASTM-F606 but must not exceed it by more than 1/4 inch. Test specimen fasteners must be the same type, style, and diameter as the production lot and must be manufactured from the same starting material, using the same manufacturing techniques as the production lot, and must be heat treated (if required) along with the production lot. 3.8 Thread Forming - The following provides the official interpretation of paragraph 4.5.2.7 of MIL-DTL-1222. 3.8.1 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. 3.8.2 Thread rolling is a cold working process and is not considered to be a machining or grinding operation. Therefore, fasteners which have rolled threads do not satisfy the provisions of MIL-DTL-1222J paragraph 4.5.2.7.b and are not eligible for the ""Alternate Mechanical Testing"" provision. 3.8.3 Thread rolling alone is not a sufficient cold working process to qualify a fastener to be in the cold worked (CW) condition. This condition is only applicable to some 300 series stainless steel studs, screws and nuts. These CW condition fasteners must be manufactured from cold worked bar stock or be cold headed in order to qualify. The threads may subsequently be rolled, machined or ground. Testing of the finished fasteners and/or reporting of the starting bar stock material properties is subject to the same provisions found in MIL-DTL-1222J paragraph 4.5.2.7 and discussed above. 3.9 Hydrogen Embrittlement Relief - Plated/coated fasteners and fasteners per paragraph 3.7 of MIL-DTL-1222 require hydrogen embrittlement relief heat treatment in accordance with ;ASTM-B633 for Zinc plated fasteners which exceed HRC 31 and/or 1000 MPA or MIL-DTL-16232 for phosphate coated fasteners which exceed HRC 39.; . Certification is required. 3.10 Seat Stack Height Measurement - To ensure that each seat is within tolerance, check each seat singularly by measuring the seat height over the ball. This measurement is calculated by adding one-half ball diameter to the half stack height dimension on the drawing. Limits are determined by the ball diameter tolerance and the half stack height tolerance. Check dimensions by measuring from the seat back face to top of ball. Manufacturers of seats that do not have a ball of the required size available will be required to manufacture a dummy ball or segment of a ball with sufficient spherical surface to check the above dimension. 3.11 ;Ball, Item 4 on Drawing 234648, is to be Teflon coated and not hard chrome plated.; 3.12 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 ;5; of drawing ;234648; . 3.12.1 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/ 3.12.2 CSD099 provides guidance for acceptance/rejection of teflon-coated valve balls after valve assembly production testing. 3.13 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. 3.14 ;Surface waviness must be verified before Teflon coating.; 3.15 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 887355443; ) 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. 3.16 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. 3.17 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.18 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. 3.18.1 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. 3.18.2 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. 3.18.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.19 ;Lubricate O-rings and threads with grease per MIL-PRF-27617 Type III.; 3.20 O-ring grooves and mating sealing surfaces must be inspected per the contractually invoked drawings or specifications. When the drawings or specifications do not provide specific defect criteria or state that no defects are allowed, the General Acceptance Criteria (GAC) standard must be used for inspecting O-ring grooves and mating sealing surfaces only. Repairs to sealing surfaces and O-ring grooves with unacceptable defects may be accomplished within the limits of the size and tolerances provided in the applicable drawing. Repairs thatwould exceed these limits require approval (including final dimensions). The data that is red lined (crossed out) is excluded from the GAC for this contract and is not to be used for acceptance or rejection criteria. The GAC document is identified as Contract Support Library Reference Number CSD008 at https://register.nslc.navy.mil/ 3.21 NAVSEA 0948-LP-045-7010 - Any applicable requirements of NAVSHIPS 4410.17,NAVSEA 0948-LP-045-7010, or 0948-045-7010 which the contractor must meet are included in this contract/purchase order. The above documents are for GovernmentUse Only. Further application of the above documents is prohibited.prohibited. 3.21.1 Marking of material with a Material Designator per the Drawing is also prohibited, with the exception of Fasteners. Fasteners must be marked with a Material Symbol/Designator as specified elsewhere in this contract. 3.22 Certificate of Compliance - (SPECIAL EMPHASIS MATERIAL) The Contractor must prepare and submit a certificate of compliance certifying that the items/components furnished under this contract comply with the requirements of the procurement document, including any/all invoked specifications and drawings. 3.23 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. 3.23.1 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. 3.23.2 All requests for Waivers/Deviations on NAVSUP-WSS Contracts must be submitted to the NAVSUP WSS Contracting Specialist via eMail. 3.23.3 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, manuals, spares, tools, and similar) being utilized by Government personnel in support of the product. h. Impacts to the operational use of the product. i. Complete estimated life-cycle cost impact of the proposed change. j. Milestones relating to the processing and implementation of the engineering change. 3.24 Mercury Free - Mercury and mercury containing compounds must not be intentionally added or come in direct contact with hardware or supplies furnished under this contract. Mercury contamination of the material will be cause for rejection. ^ QUALITY ASSURANCE REQUIREMENTS ^ 3.25 See CDRL DI-MISC-80678 (Test Certification) - A statement of tests performed, listing the pieces tested must be furnished along with a copy of the test results. Certification must include the contractor's name, address and date, quantity inspected, identified to the contract/purchase order and item number, and the Contractor's or authorized personnel's signature. Test certifications must reference the standard/specification, including the revision, to which the testing was performed and the acceptance criteria used. Test procedure numbers may also be referenced on test reports. Test reports on weldments must be identified to weld joint and layer. 3.26 Welding Requirements - When production or repair welding is required, the applicable welding procedure(s) and qualification data must be submitted for review and approval. In addition, the CONSUMED WELD METAL C of C as defined below must be submitted as part of the certification OQE package submitted by the Contractor. Note: These requirements do not apply to tack/spot welds when the conditions of Section 4.2.1.1 of S9074-AR-GIB-010A/278 are met. 3.26.1 Approval of the Contractor's qualification data must be obtained prior to performing any welding (production or repair). 3.26.2 If the Contractors qualification data has previously been approved by the Navy for other contracts, a copy of the original approval letter may be submitted along with the procedures and qualification data report to expedite the approval process. The approval letter must reference the applicable welding procedure and qualification data report identification/number. Prior approval does not guarantee acceptance for this or any future contracts. As far as practical, all procedures for the contract must be submitted at the same time. Welding procedures and qualification data must be submitted in a commercially available electronic format such as Adobe Acrobat PDF. The contractor must state the applicability of each weld procedure and qualification data submitt...
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