SAMDaily.us | PRESOL | 48 | 48--VALVE,BALL

SAMDAILY.US - ISSUE OF JULY 24, 2021 SAM #7175
SOLICITATION NOTICE

48 -- 48--VALVE,BALL

Notice Date: 7/22/2021 6:31:03 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: N0010421QFC61
Response Due: 8/10/2021 12:00:00 AM
Archive Date: 08/25/2021
Point of Contact: Telephone: 7176053875
E-Mail Address: JILL.SABOL@NAVY.MIL
(JILL.SABOL@NAVY.MIL)
Description: CONTACT INFORMATION|4|N743.7|WVN|717-605-3875|jill.sabol@navy.mil| ITEM UNIQUE IDENTIFICATION AND VALUATION (MAR 2016)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP REVIEW FEB 1991)(FEB 1999)|1|See specification section C | INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2||| INSPECTION AND ACCEPTANCE - SHORT VERSION|8|x||x|||||| TIME OF DELIVERY (JUNE 1997)|20|0001AA|5|450|||||||||||||||||| GENERAL INFORMATION-FOB-DESTINATION|1|B| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)|16|Material - Invoice & Receiving Report (COMBO) Certifications - Stand-Alone Receiving Report|Material - Inspection & Acceptance at SOURCE Certifications - Inspection at DESTINATION & Acceptance at OTHER |TBD|N00 104|TBD|Certifications - N39040; Material -S4306A |N50286|TBD|133.2|NA|NA|Certifications - N39040|NA|NA|See DD Form 1423|PORT_PTNH_WAWF_Notification@navy.mil| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| EQUAL OPPORTUNITY (SEP 2016)|2||| WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUNE 2003)|6|one year from the date of delivery |one year from the date of delivery ||||| WARRANTY OF DATA--BASIC (MAR 2014)|2||| AUTHORIZED DEVIATIONS IN CLAUSES (NOV 2020)|2||| NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (OCT 2020)(DEVIATION 2020-O0008)|1|| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2020)|13|||||||||||||| BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (NOV 2014)|1|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAR 2020)|13|332919|750|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||x| EVALUATION CRITERIA AND BASIS FOR AWARD-|1|| 1. The resultant award of this solicitation will be issued bilaterally, requiring the contractor's written acceptance prior to execution. 2. Any contract/order awarded as a result of this solicitation will be a ""DO"" rated order certified for national defense use under the Defense Priorities and Allocations System (DPAS). See 52.211-14, Notice of Priority Rating for National Defense, Emergency Preparedness, and Energy Program Use. 3. DD 1423 Data Item A001 (Inspection and Test Plan) may be waived if already on file at NAVSUP WSS Mechanicsburg. See WSSTERMLZ02 for details. Quality Manuals shall be submitted to the NAVSUP WSS POC for this RFQ, currently Jill Sabol, at jill.sabol@navy.mil 4. Consistent with FAR 52.216-18, ""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. NAVSUP WSS Mech will be considering past performance in the evaluation of offers. See Clauses DFARS 252.213-7000 and WSSTERMMZ01. 6. Available drawings and additional documents can be accessed through SAM.gov. 7. This procurement has radiography/radiographic shooting sketch requirements. 8. The following delivery schedule will apply: RADIOGRAPHIC SHOOTING SKETCHES (RSS) 45 DAYS ADC APPROVAL OF RADIO RSS 30 DAYS AFTER RECEIPT PRODUCTION RADIOGRAPHY (PR) 135 DAYS AFTER APPROVAL OF RSS APPROVAL OF PR 30 DAYS AFTER RECEIPT Submission of all other form 1423 certification data (CDRLs) will be on or before 20 days prior to delivery. PNSY review/acceptance of CDRLs shall be 6 working days after receipt of CDRLs. Final delivery of material will be on or before 450 days after the effective date of the contract. \ 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. 2.3 Specification Revisions - The specification revisions listed under ""Docu ments 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. 2.3.1 Documents, drawings, and publications supplied are listed under ""Drawing Number"". These items should be retained until an award is made. 2.3.2 ""Document References"" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. DRAWING DATA=DM124930 |96169| A|1N |D|0001 | A|49998|0069057 DRAWING DATA=DM124930 |96169| A|1N |D|0002 | A|49998|0023769 DRAWING DATA=EB-4147 |96169| A|PS |D|0001 | A|49998|1441793 DRAWING DATA=2641-405-01 |96169| C| |D|0001 | C|49998|0677137 DRAWING DATA=2641-405-01 |96169| C| |D|0002 | C|49998|0306486 DRAWING DATA=2641-405-01C03 |96169| A|ER |D|0001 | A|49998|0054739 DRAWING DATA=2641-405-01C03 |96169| A|ER |D|0001.1 | A|49998|0013034 DRAWING DATA=2641-405-01C03 |96169| A|ER |D|0002 | A|49998|0148533 DRAWING DATA=2641-405-01C1 |96169| |ER |D|0001 | |49998|1557359 DRAWING DATA=2641-405-01C2 |96169| |ER |D|0001 | |49998|1959053 DRAWING DATA=2641-405-01C4 |96169| B|ER |D|0001 | B|49998|1906271 DRAWING DATA=2641-809-40F1 |53711| A|ER |D|0001 | A|49998|0482072 DRAWING DATA=2641-809-40F2 |53711| A|ER |D|0001 | A|49998|1032221 DRAWING DATA=2641-809-40F3 |53711| A|ER |D|0001 | A|49998|1105420 DRAWING DATA=2641-809-41 |96169| F| |D|0001 | F|49998|0196377 DRAWING DATA=2641-809-41F02 |96169| A|ER |D|0001 | A|49998|0817284 DRAWING DATA=2641-809-41F03 |96169| A|ER |D|0001 | A|49998|3043683 DRAWING DATA=4384678 |80064| C| |D|0001 | C|49998|1136401 DRAWING DATA=4384678C01 |53711| C|DN |D|0001 | C|49998|0067532 DRAWING DATA=4384678C01 |53711| C|DN |D|0002 | C|49998|0045081 DRAWING DATA=4384678C01 |53711| C|DN |D|0003 | C|49998|0030946 DRAWING DATA=4384678C02 |53711| C|DN |D|0001 | C|49998|0041260 DRAWING DATA=4384678C03 |53711| C|DN |D|0001 | C|49998|0035403 DRAWING DATA=4384678C04 |53711| C|DN |D|0001 | C|49998|0040252 DRAWING DATA=4384678C05 |53711| C|DN |D|0001 | C|49998|0033942 DRAWING DATA=4384678C06 |53711| C|DN |D|0001 | C|49998|0033961 DRAWING DATA=7108936 |53711| F| |D|0001 | F|49998|0807371 DRAWING DATA=7108936 |53711| F| |D|0002 | F|49998|0292564 DRAWING DATA=7108936 |53711| F| |D|0003 | F|49998|0173351 DRAWING DATA=7108936 |53711| F| |D|0004 | F|49998|0213107 DRAWING DATA=7108936 |53711| F| |D|0005 | F|49998|0408672 DRAWING DATA=7108936 |53711| F| |D|0006 | F|49998|0266144 DRAWING DATA=7108936 |53711| F| |D|0007 | F|49998|0272454 DRAWING DATA=7108936 |53711| F| |D|0008 | F|49998|0376438 DRAWING DATA=7108936 |53711| F| |D|0009 | F|49998|0402428 DRAWING DATA=7108936 |53711| F| |D|0010 | F|49998|0407398 DRAWING DATA=7108936 |53711| F| |D|0011 | F|49998|0201710 DRAWING DATA=7108936 |53711| F| |D|0012 | F|49998|0373272 DRAWING DATA=7108936 |53711| F| |D|0013 | F|49998|0196952 DRAWING DATA=7108936 |53711| F| |D|0014 | F|49998|0219783 DRAWING DATA=7108936 |53711| F| |D|0015 | F|49998|0465991 DRAWING DATA=7108936 |53711| F| |D|0016 | F|49998|0255117 DRAWING DATA=7108936 |53711| F| |D|0017 | F|49998|0419296 DRAWING DATA=7108936 |53711| F| |D|0018 | F|49998|0425311 DRAWING DATA=7284884 |53711| F| |D|0001 | F|49998|0125575 DRAWING DATA=7284884 |53711| F| |D|0002 | F|49998|0133395 DRAWING DATA=7284886 |53711| E| |D|0001 | E|49998|1587181 DOCUMENT REF DATA=FED-STD-H28 | | |A |941228|A| | | DOCUMENT REF DATA=ANSI/ASQ Z1.4 | | | |080101|A| | | DOCUMENT REF DATA=ASTM-B150 | | | |190401|A| | | DOCUMENT REF DATA=ASTM-A351 | | | |060301|A| | | DOCUMENT REF DATA=ASTM-A574 | | | |120401|A| | | DOCUMENT REF DATA=ASTM-F606 | | | |160901|A| | | DOCUMENT REF DATA=MIL-STD-792 | | |F |060519|A| | | 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=ISO/IEC 17025 | | | |050515|A| | | DOCUMENT REF DATA=MIL-DTL-18240 | | |F |000313|A| 1| | DOCUMENT REF DATA=QPL 18240 | | |QPD|170619|A| | | DOCUMENT REF DATA=MIL-I-45208 | | |A |810724|A| 1| | DOCUMENT REF DATA=MIL-STD-45662 | | |A |880801|A| | | DOCUMENT REF DATA=A-A-59004 | | |A |950907|A| | | DOCUMENT REF DATA=SAE AMS-QQ-S-763 | | |D |150301|A| | | DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | | DOCUMENT REF DATA=S9074-AQ-GIB-010/248 | | | |950801|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 ;The 2 inch Ball Valve shall be in accordance with Electric Boat Drawing 2641-405-01, Assembly IRHY, along with all EB ERs provided with this Contract/Purchase Order, except as amplified or modified herein.; 3.2 ;Spring, item 51, of Drawing 2641-405-01 shall be modified to ER2641-809-41F2.; 3.3 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: Part - ;Body, item 104, on Drawing 2641-405-01; Material - ;ASTM-A351, Grade CF-3M; Part - ;Bonnet Cap, item 54, on Drawing 2641-405-01; Material - ;SAE AMS-QQ-S-763, Class 304, Condition A; Part - ;Stem, item 50 on Drawing 2641-405-01; Material - ;ASTM-B150, Alloy C63200, Temper TQ-50; Part - ;Self-Locking Socket Head Cap Screw, item 119, on Drawing 2641-405-01; Material - ;MIL-DTL-1222, Type II, ASTM-A574 and meeting the mechanical properties of note 22 of drawing 2641-405-01, with Self-Locking element in accordance with MIL-DTL-18240.; Part - ;Ball (Q3), item 42, on Drawing 2641-405-01; Material - ;SAE AMS-QQ-S-763, Class 304, Condition A; Part - ;Seats (Q3), piece 65, on Drawing 2641-405-01 (Note: This is piece 46 on Drawing 7284884); Material - Torlon 4503, 4203, or 4203L (unfilled polyamide-imide) per Electric Boat Specification 4147. (Certificate of Compliance only is required) 3.4 Testing Certification - Certifications are required for the following tests on the items listed below. Additional testing on other piece parts (if any) per applicable drawings is still required, but certifications are only required as listed below. Test - ;Liquid Penetrant Inspection or Magnetic Particle Inspection (Wet Method) (Either inspection is acceptable); Item - ;Self-Locking Socket Head Cap Screw, item 119, on Drawing 2641-405-01; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Test - ;Dye Penetrant Inspection; Item - ;Body, item 104, on Drawing 2641-405-01; Performance - T9074-AS-GIB-010/271 Acceptance - S9074-AR-GIB-010A/278 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 - ;Bonnet Cap, item 54 and Ball, item 42 on Drawing 2641-405-01; Performance - SAE-AMS-QQ-S-763 Acceptance - SAE-AMS-QQ-S-763 Test - Pressure Tests Item - Each Assembly Performance - ;General Note 6 on Drawing 2641-405-01; Acceptance - ;General Note 6 on Drawing 2641-405-01; 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/-0PSIG. 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 thesmallest graduation on an analog test pressure gauge, not to exceed 50 PSIG. 30 minutes / - 0 minutes. 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 ;Radiography is required on Body, item 104, on Drawing 2641-405-01; 3.7 Wedge Tensile Test Specimens (Headed fasteners) - A wedge tensile test shall be conducted on a Full Size Fastener for each production lot and reported aspart of the Mechanical Properties. The required specimens for the Wedge TensileTest shall be separate fasteners from those required for the Yield Test. 3.7.1 Testing for Socket Head Cap Screws shall 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 shall be in accordance with ASTM-F606 for grades 5, 8, B7, and B16.For all other grades, the following wedge angles shall be used. a. Except as specified in item c below, fasteners with a nominal diameter of 1/4-inch through 1-inch (inclusive) shall be tested with a ten degree wedge. b. Except as specified in item c below, fasteners with a nominal diameter over 1-inch shall 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 shall 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"" shall be manufactured from each lot of fasteners and tested to represent that lot. The length of these test specimen fasteners shall meet the minimum specified in table 1 of ASTM-F606 but shall not exceed it by more than 1/4 inch. Test specimen fasteners shall be the same type, style, and diameter as the production lot and shall be manufactured from the same starting material, using the same manufacturing techniques as the production lot, and shall be heat treated (if required) along with the production lot. 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 Thread Lubricant - Thread lubricants containing molybdenum disulfide shall not be used on this material. Bacteria in water, especially seawater, causes molybdenum disulfide to break down. The by-products of the breakdown form compounds which attack the fasteners. Anti-galling compound A-A-59004 (or copper or nickel based anti-seize compounds if A-A-59004 is not available) shall be used as a replacement when thread lubricant is required for assembly. 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 Dupont Teflon Coating 850G-204 and 852G-201. Use of Dupont Teflon Coating 851N-204 and 852N-201 is acceptable until exhausted - Teflon coating of ball(s) must be in accordance with general note ;4. F.; of drawing ;803-4384678; . 3.12 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/ 3.12.1 CSD099 provides guidance for acceptance/rejection of teflon-coated valve balls after valve assembly production testing. 3.13 ;Naval Ordnance Systems Command OD 10362 First Revision dated 15 Aug 1961 is provided by Contract Support Library Reference Number CSD018.; 3.14 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 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 T887306005; ) 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 ;Plastic color coding of the Handwheel is not required.; 3.17 Welding or Brazing - When welding, brazing, and allied processes are required, they must be in accordance with S9074-AR-GIB-010A/278, (S9074-AQ-GIB-010/248 for brazing) by personnel and procedures qualified under S9074-AQ-GIB-010/248 for all production and repair welding and brazing. Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing. 3.18 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. 3.18.1 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. 3.18.2 All requests for Waivers/Deviations on NAVSUP-WSS Contracts must be submitted using the ECDS (Electronic Contractor Data Submission) system at https://register.nslc.navy.mil/ 3.18.3 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. 3.19 Certificate of Compliance - (SPECIAL EMPHASIS MATERIAL) The Contractor shall 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. 3.20 Mercury Free - Mercury and mercury containing compounds shall 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. 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. ^ QUALITY ASSURANCE REQUIREMENTS ^ 3.22 See CDRL DI-MISC-80678 (Test Certification) - A statement of tests performed, listing the pieces tested shall be furnished along with a copy of the test results. Certification shall 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 shall be identified to weld joint and layer. 3.23 Welding Requirements - When production or repair welding is required, the applicable welding procedure(s) and qualification data shall be submitted for review and approval. In addition, the CONSUMED WELD METAL C of C as defined below shall be submitted as part of the certification OQE package submitted by the Contractor. Note: These requirements do not apply to tack/spot welds. 3.23.1 Approval of the Contractor's qualification data shall be obtained prior to performing any welding (production or repair). 3.23.2 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 shall be submitted at the same time. Welding procedures and qualification data shall be submitted in a commercially available electronic format such as Adobe Acrobat PDF. The contractor shall state the applicability of each weld procedure and qualification data submitted, citing the drawing number and pieces to be welded. (i.e. ""WP-123 and QD-123 are submitted for the weld joint between pieces 1 and 2 on drawing ABC."" "" WP-456 and QD-456 are submitted for the hardfacing of piece 3 on drawing XYZ.""). Authority for the repair of Special Repairs in castings and authority for the repair of wrought or forged material material shall be obtained from the Procurement Contracting Officer. This request shall describe the defect; including size, depth, location, and a description of the proposed repair. This request for NAVSUP-WSS Contracts shall be submitted via the Electronic Contractor Data Submission (ECDS) application. 3.23.3 Any new procedure qualification performed under this Contract will require the vendor to provide a minimum 48 hour notification to DCMA with an offer to observe the welding of the test assemblies. The 48 hour time limit may be modified upon mutual agreement between the vendor and DCMA. 3.23.4 When drawings require hard facing surface Iron content (Nickel for Monel valves) not to exceed 5%, the contractor shall verify surface Iron or Nickel content by performing chemical testing as defined by the applicable drawing. The chemical test results shall be submitted as part of the qualification data. 3.23.5 Qualification requirements for production hardfacing: The maximum qualified thickness for hardfacing shall be twice the weld deposit thickness measured in the as-welded condition that is subjected to initial NDT (Non-Destructive Testing) and any additional drawing requirements. The minimum qualified thickness is the final machined thickness at which hardness testing, NDT, macro-etch, and any additional drawing requirements are satisfactorily performed. 3.23.6 Additional qualification requirements for production hardfacing thickness less than 1/8-inch: Macro-etch (or legible photomacrographs) shall be submitted for review and show consistent, minimized dilution. All essential elements and any elements not listed in S9074-AQ-GIB-010/248 that influence dilution shall be in the qualification data and weld procedure, with strict limits placed on each essential element. 3.23.7 Qualification requirements for production cladding: The maximum qualified thickness for cladding shall be twice the weld deposit thickness measured in the as-welded condition that is subjected to initial NDT and any additional drawing requirements. The minimum qualified thickness is the final machined thickness at which NDT, side bends, macro-etch testing, and any additional drawing requirements are satisfactorily performed. 3.23.8 When weld repair is required on titanium material, the applicable fabrication plan, facilities procedure, training plan, and active welder qualification shall be submitted for review and approval. 3.23.9 If the contractor's fabrication plan, facilities procedure, training plan, or active welder qualification has previously been approved by the Navy for other contracts, a copy of the original approval letter may be submitted along with the applicable documentation to expedite the approval process. The approval letter must reference the applicable documentation. Prior approval does not guarantee acceptance for this or any future contracts. The contractor's fabrication plan, facilities procedure, training plan, and active welder qualification shall be submitted at the same time as the applicable welding procedure(s) and weld procedure qualification data. All documentation shall be submitted in a commercially available electronic formation, such as Adobe Acrobat PDF. 3.23.10 Preparation and retention of weld records is required, as specified by paragraph 4.1.3 of S9074-AR-GIB-010A/278. 3.23.11 A Certificate of Compliance is required for all weld filler metals used for production or repair welding, and shall include the following: a) Filler Metal LOT number(s) b) Specification and Type c) A positive statement that the vendor has obtained OQE and verified that each LOT of weld filler material conforms to specification requirements. d) Apositive statement verifying that the weld filler metals were the correct material type or grade prior to consumption. 3.23.12 When production welds or repair welds are performed by a subcontractor, the requirement for submission of all certification documentation required herein shall be passed down to the subcontractor. 3.24 Radiography (RT) - Radiography shall be performed in accordance with T9074-AS-GIB-010/271. RT acceptable criteria for castings to be criticality level Iper the applicable table of S9074-AR-GIB-010A/278. RT acceptance criteria for weldments to be per the applicable table of S9074-AR-GIB-010A/278 (P-1 piping) or MIL-STD-2035, class 1, as applicable. 3.24.1 See CDRL DI-MISC-80678 (RSS) - The Contractor or activity performing theradiography shall be responsible for preparing the radiographic shooting sketches (RSS) in accordance with T9074-AS-GIB-010/271. Shooting sketches are not required for radiography of weldments. The radiographic standard shooting sketches (RSSS) referenced on the applicable drawing may be used, however, since T9074-AS-GIB-010/271 permits a variety of processes, the RSSS may not be applicable as they will not necessarily depend only on the coverage requirements, but also on the equipment and procedures of the particular radiographic facility. Approval of these shooting sketches or radiographic standard shooting sketches is required per S9074-AR-GIB-010A/278. If this datahas been previously approved by a Navy activity, the original approval letter shall be submitted at the same time as RT film and reader sheet submittal. 3.24.2 All pieces radiographed shall be permanently marked with ""RT"" and a unique RT serial number. (The unique RT serial number must be directly traceable tothe RT film.) 3.24.3 See CDRL DI-MISC-80678 (Production Radiography) - Production Radiographyrequires final acceptance by the Navy. The items listed below shall be submitted for final acceptance, cataloging, file, and retention. They must be submitted and approved prior to shipment of the...
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