Firing Valve with Muffler for Naval Weapon Systems

|4|N743.30|N/A|717-605-2379|[email protected]| 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||| INSPECTION AND ACCEPTANCE - SHORT VERSION|8|X||X|||||| STOP-WORK ORDER (AUG 1989)|1|| 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 |[email protected]| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| INTEGRITY OF UNIT PRICES (NOV 2021)|1|| 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||| EQUAL OPPORTUNITY FOR WORKERS WITH DISABILITIES (JUN 2020)|2||| LIST OF AWARD

ATTACHMENTS|5|||||| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (OCT 2025)|13|||||||||||||| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAR 2025)(DEVIATION 2025-O0003 AND2025-O0004))|13|332919|750|||||||||||| TYPE OF CONTRACT (APR 1984)|1|Firm Fixed Price| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||x| DD1423 Data Item A001 may be waived if already on file atNAVSUP WSS Mechanicsburg. Any contract awarded as a result of this solicitation will beDO rated order certified fornational defense use under the Defense Priorities andAllocations System (DPAS). \ 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 The documents and drawings listed below under DRAWING NO. are not provided with this Contract/Purchase order. DRAWING NO CAGE REV DISTR CD ;280912-1005 99657 D B 233985-0002 99657 C B 236001-1005 99657 E B 236461-0002 99657 E B 233029 99657 L B 281015-0001 99657 G B 235445-0003 99657 A B 284031-1005 99657 D B 236463-1005 99657 D B 283538 99657 J B ATP280912-1005 99657 C B; 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. 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=ANSI/ASQ Z1.4 | | | |080101|A| | | DOCUMENT REF DATA=ASTM-B150 | | | |190401|A| | | DOCUMENT REF DATA=ASTM-A240 | | | |240501|A| | | DOCUMENT REF DATA=ASTM-A262 | | | |150901|A| | | DOCUMENT REF DATA=QQ-N-281 | | |D |851023|A|2 | | DOCUMENT REF DATA=ASTM-A574 | | | |211201|A| | | DOCUMENT REF DATA=ASTM-A581 | | |B |950910|A| | | DOCUMENT REF DATA=ASTM-A582 | | | |211101|A| | | DOCUMENT REF DATA=ASTM-F593 | | |A |131201|A| | | DOCUMENT REF DATA=ASTM-F606 | | | |191115|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=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=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) | | | |130215|A| | | 3.

REQUIREMENTS 3.1 ;Firing valve assembly to be in accordance with Marotta drawing 280912-1005 , 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 280912-1005; Part - ;Body, item 13 and Cover, item 14; Material - ;SAE-AMS-5659, CRES 15-5 PH, H1025; Part - ;Fitting, item 15; Material - ;ASTM-B150, alloy UNS C63000, temper TQ50; Part - ;Socket Head Cap Screw, item 86; Material - ;MIL-DTL-1222, Grade 630. Chemicals per ASTM-F593 and mechanicals per MIL-DTL-1222, Table II; Part - ;Socket head cap screw, item 87; Material - ;MIL-DTL-1222, grade A574, Marotta drawing 233985-0002 for differential pressure indicator; Part - ;Body; Material - ;CRES 300 SER PER QQ-S-763, ASTM-A581, ASTM-A582, AMS 5640 OR MONEL PER QQ-N-281, Marotta drawing 236001-1005 for dome system assembly; Part - ;Retainer screw, item 25 and body, item 36; Material - ;SAE-AMS-5659, CRES 15-5PH, H1025; Part - ;Housing, item 28; Material - ;ASTM-B21 UNS C46400 Temper H02; Part - ;Plug and Bleeder, item 81; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS-5640 or ASTM-A581 or ASTM-A582; Part - ;Socket Head Cap Screw, Item 100; Material - ;MIL-DTL-1222, grade A574, Marotta drawing 281015-0001 for a Valve relief assembly; Part - ;Retainer, item 17 and Body, item 18; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS-5640 or ASTM-A581 or ASTM-A582, Marotta drawing 235445-0003 for a Compensator assembly; Part - ;Housing, item 12 and Cover, item 13; Material - ;QQ-N-281; Part - ;Socket Head Cap Screw, item 60; Material - ;MIL-DTL-1222, Grade 630. Chemicals per ASTM-F593 and mechanicals per MIL-DTL-1222, Table II, Marotta drawing 283538, part number 283538-1344 for a Hand valve assembly; Part - ;Retainer Screw, item 13; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS-5640 or ASTM-A581 or ASTM-A582; Part - ;Stem, item 15; Material - ;SAE-AMS-QQ-S-763, class 316, condition A, Marotta drawing 284031-1005 for a Pilot Valve assembly; Part - ;Body, Item 116; Material - ;SAE-AMS-5659, CRES 15-5PH, H1025; Part - ;Valve Nut, item 121; Material - ;ASTM-B150 C63200 TQ50 or TQ55, Marotta drawing 233029, part number 233029-0001 for a screw assembly; Part - ;Screw, Item 12; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS-5640 or ASTM-A581 or ASTM-A582, Marotta drawing 236463-1005 Interlock Assembly; Part - ;Adapter, Item 102; Material - ;SAE-AMS-5659, CRES 15-5PH, H1025; Part - ;Adapter, item 106; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS-5640 or ASTM-A240 or ASTM-A581 or ASTM-A582; Part - ;Body, item 104; Material - ;ASTM-B150, alloy C63020, temper TQ30, Marotta drawing 236461-0002, for a Regulator Assembly; Part - ;Guide, Item 15 and body, item 26; Material - ;SAE-AMS-5659, CRES 15-5 PH, H1025; Part - ;Cover, item 28, and Plug and Bleeder, item 85; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS-5640 or ASTM A581 or ASTM A582; Part - ;Socket Head Cap Screw, Item 82; Material - ;MIL-DTL-1222, grade A574 or grade 4340; 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 - Non-Destructive Tests Item - ;Weld Repair and/or Production Weld (as applicable); Performance - Per applicable fabrication specification Acceptance - Per applicable fabrication specification 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 - ;Body on drawing 233985-0002; Plug and bleeder assembly item 81 on drawing 236001-1005; Retainer item 17 and body item 18 on drawing 281015-0001; Retainer screw item 13 and stem item 15 on drawing 283538; screw item 12 on drawing 233029; Adapter item 106 on drawing 236463-1005; Cover item 28 and plug and bleeder item 85 on drawing 236461-0002.; Performance - SAE-AMS-QQ-S-763 Acceptance - SAE-AMS-QQ-S-763 Test - Intergranular Corrosion Testing Item - ;Adapter, Item 106 on drawing 236463-1005 (required only if material for Adapter is ASTM-A240); Performance - ASTM-A262, Practice E Acceptance - ASTM-A262 Test - ;Liquid Penetrant Inspection or Magnetic Particle Inspection (Wet Method) (Either inspection is acceptable); Item - ;Socket Head Cap Screws item 86 and 87 on drawing 280912-1005; item 100 on drawing 236001-1005; Item 82 of drawing 236461-0002 and Item 60 of drawing 235445-0003; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Test - ;All test required by ATP280912-1005; Item - ;Each Assembly; Performance - ;ATP280912-1005; Acceptance - ;ATP280912-1005; 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 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. 3.5.1 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. 3.5.2 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. 3.5.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.6 Thread Forming - The following provides the official interpretation of paragraph 4.5.2.7 of MIL-DTL-1222. 3.6.1 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. 3.6.2 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. 3.6.3 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. 3.7 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 887905309; ) 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. 3.8 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. 3.8.1 Testing for Socket Head Cap Screws must be in accordance MIL-DTL-1222, paragraphs 4.5.2.3 and 4.5.2.3.1. 3.8.2 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. 3.8.3 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. 3.9 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.10 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. 3.11 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/ 3.12 Specification Change - For QQ-N-281, Class B material: 1 - Footnote 9 to Table II of QQ-N-281 does not apply. 2 - When starting material is Round Bar greater than 3" dia, the mechanical properties of Hex Bar apply. 3.13 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. 3.14 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. 3.14.1 Waivers/Deviations - All waivers and deviations, regardless of significance or require review and approval by the