Globe Valve

|4|N744.1|WVR|771-229-3917|[email protected]| ITEM UNIQUE IDENTIFICATION AND VALUATION (JAN 2023)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (DEC 2014)|1|See specifications C and E| INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2||| INSPECTION/ACCEPTANCE POINT|6|TBD|DCMA NSEO S4306A|||TBD|DCMA NSEO S4306A| 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|[email protected]| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|WSS| MANDATORY USE OF WORKFLOW PRO (WFP) MOD ASSIST MODULE|1|| 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||||| FIRST ARTICLE APPROVAL--CONTRACTOR TESTING (DEV 2026-O0042)(FEB 2026)|10|One (1)|0001AA|30|TBD||||||| 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-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024)|1|| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (DEVIATION 2026-O0043)(FEB 2026))|13||||||||||||||

INSTRUCTIONS TO OFFERORS -- COMPETITIVE ACQUISITION (DEV 2026-O0048)(MAR 2026)|2||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||X| EVALUATION OF FIRST ARTICLE TESTING|3|||X| 1. This requirement is pursuant to Emergency Acquistion Flexibilities (EAF). 2. The resultant award of this solicitation will be issued bilaterally, requiring the contractor's written acceptance prior to execution. 3. 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. 4. Any contract awarded as a result of this solicitation will be DO certified for national defense use under the Defense Priorities and Allocations System (DPAS). Provision 52.211-14, Notice of Priority Rating for National Defense, Emergency Preparedness, and Energy Program Use, shall be inserted in solicitations when the contract to be awarded shall be a rated order. 5. If drawings are included in the solicitation, access needs to be requested on the individual solicitation page under Contract Opportunities on SAM.gov website. After requesting access, send an email to the POC listed on the solicitation. 6. NAVSUP WSS Mechanicsburg will be considering past performance in the evaluation of offers IAW FAR 13.106(a)(2). 7. Data Item A001 (Inspection and Test Plan) may be waived if already on file at NAVSUP WSS Mechanicsburg. 8. This solicitation requires First Article Testing (FAT). See FAR 52.209-3 First Article Approval - Contractgor Testing for more 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 "Document References" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. 2.2.2 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. 2.2.3 Documents, drawings, and publications supplied are listed under "Drawing Number". These items should be retained until an award is made. DRAWING DATA=1385620 |80064| M| |D| | | | DRAWING DATA=2177525 |80064|AA|DW |D| | | | DOCUMENT REF DATA=ASTM-E18 | | | |200201|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-A105 | | | |210101|A| | | DOCUMENT REF DATA=ASTM-E140 | | | |121201|A| | | DOCUMENT REF DATA=ASTM-A182 | | | |240301|A| | | DOCUMENT REF DATA=ASTM-A193 | | |A |241015|A| | | DOCUMENT REF DATA=ASTM-A194 | | | |240501|A| | | DOCUMENT REF DATA=ASTM-B633 | | | |151201|A| | | DOCUMENT REF DATA=MIL-STD-792 | | |F |230223|A| |01| DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | | DOCUMENT REF DATA=MIL-STD-2035 | | |A |950515|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=MIL-DTL-16232 | | |H |200915|A| | | DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | | DOCUMENT REF DATA=MIL-S-24093 | | |A |911105|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 1/2 INCH SOCKET WELD IN-LINE STOP VALVE WITH BACKSEAT TO BE IN ACCORDANCE WITH NAVSHIPS DRAWING 803-2177525, ASSEMBLY 803-2177525-C3A1AF, 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, PIECE 1, AND BONNET, PIECE 86; Material - ;FORGED ASTM-A105 or MIL-S-24093, TYPE V, CLASS H. (PHOSPHATE COATING TO BE IN ACCORDANCE WITH GENERAL NOTE 4.H); Part - ;STEM, PIECE 79; Material - ;ASTM-A182 GRADE F6A or SAE-AMS-QQ-S-763 CLASS 410 CONDITION T. MECHANICAL PROPERTIES FOR ASTM-A182 MATERIAL MODIFIED PER GENERAL NOTE 4.B.1 of DRAWING. MECHANICAL PROPERTIES FOR SAE-AMS-QQ-S-763 MATERIAL MUST BE AS SPECIFIED IN SAE-AMS-QQ-S-763 AND MODIFIED TO GENERAL NOTE 4.B.2 OF DRAWING 2177525.; Part - ;BODY STUDS, PIECE 11; Material - ;MIL-DTL-1222 GRADE B7 (ASTM-A193) WITH COATING/PLATING IN ACCORDANCE WITH GENERAL NOTE 4.F OF DRAWING 2177525.; Part - ;BODY STUD NUTS, PIECE 12; Material - ;MIL-DTL-1222 GRADE 2H or 7 (ASTM-A194) WITH COATING/PLATING IN ACCORDANCE WITH GENERAL NOTE 4.F OF DRAWING 2177525.; 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 (as applicable); Performance - Per applicable fabrication specification Acceptance - Per applicable fabrication specification Test - ;Liquid Penetrant Inspection or Magnetic Particle Inspection (Wet Method) (Either inspection is acceptable); Item - ;Body Studs, Piece 11, and Body Stud Nuts, Piece 12; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Test - Pressure Tests Item - Each Assembly Performance - ;General Note 1 of Drawing 2177525; Acceptance - ;General Note 1 of Drawing 2177525; Test - ;Dye Penetrant Inspection; Item - ;All hardfacing after final machining; Performance - T9074-AS-GIB-010/271 Acceptance - MIL-STD-2035 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 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. 3.6 Stem Hardness - Additional Inspection

Requirements: 3.6.1 Perform stem hardness testing in accordance with General Note 5.W of NAVSHIPS Standard Drawing 803-2177525. The results must be in accordance with General Note 4.B of Drawing 803-2177525. 3.6.2 ASTM-E18 requires correction factors to be applied to readings taken on convex cylindrical surfaces. Uncorrected readings (i.e. Hardness readings taken on convex cylindrical surfaces without the correction factor applied OR hardnessreadings taken on flat surfaces) must not be above 100 HRB or below 20 HRC. Readings that exceed 100 HRB due to the application of correction factors are acceptable for stems in accordance with Drawing 803-2177525 and General Note 4.B(1) or 4.B(2). NOTE: Uncorrected readings below 20 HRC and above 100 HRB are beyond their respective ranges recommended for accuracy. Stems with uncorrected hardness readings beyond such recommended ranges must be retested using the appropriate Rockwell hardness scale or another hardness test method, where valid conversions are provided in ASTM E140, and in accordance with instruction provided in General Note 5.W of NAVSHIPS Standard Drawing 803-2177525. 3.7 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.8 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. 3.8.1 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. 3.8.2 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. 3.8.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.9 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/ 3.10 Thread Forming - The following provides the official interpretation of paragraph 4.5.2.7 of MIL-DTL-1222. 3.10.1 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. 3.10.2 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. 3.10.3 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. 3.11 Heat Treat

Requirements - Mechanical properties (via tension testing and hardness testing if hardness is required by the applicable material specification) are required for each heat in each heat treat charge for ASTM-A234, ASTM-A403, ASTM-A182, and ASTM-A105 material. 3.11.1 If heat treatment is performed in continuous-type furnaces with suitable temperature control and equipped with recording pyrometers so that complete heat-treatment records are available, a heat-treatment charge must be considered as any continuous run not exceeding an 8-hr duration. One tension test must be taken from one forging per heat in each heat treatment charge at a minimum of every 8 hours. 3.11.2 Certification of Mechanical Properties (Mechanical Analysis, Tension Testing) must include the condition furnished. The contractor must maintain a complete record on file of the heat treatment given each piece, including stress relief. The contractor must provide either the record of the final heat treatment or a heat treatment certification statement. The certification statement must be signed by the heat-treater and include the date of heat treatment, duration and temperature of heat treatment operations and quenching medium (if required). 3.12 First Article Approval (Contractor Testing) - First Article Test (FAT) and approval is required. 3.13 Welding or Brazing - When welding, brazing, and allied processes are required, as invoked by Section C paragraph 3