Inactive
Notice ID:N0010426QZA28
CONTACT INFORMATION|4|N742.10|WV2BB|N/A|madison.m.gray4.civ@us.navy.mil| ITEM UNIQUE IDENTIFICATION AND VALUATION (JAN 2023)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP RE...
CONTACT INFORMATION|4|N742.10|WV2BB|N/A|madison.m.gray4.civ@us.navy.mil| ITEM UNIQUE IDENTIFICATION AND VALUATION (JAN 2023)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP REVIEW FEB 1991)(FEB 1999)|1|ISO9001| INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2||| INSPECTION/ACCEPTANCE POINT|6||||||| GENERAL INFORMATION-FOB-DESTINATION|1|N50286| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (JAN 2023)|16|Material - Invoice & Receiving Report (COMBO); Certifications - Stand-Alone Receiving Report|N/A|TBD|N00104|TBD|Material - S4306A; Certifications - N39040|N50286|TBD|133.2|N/A|N/A|Certifications - N39040|N/A|N/ A|See DD Form 1423|PORT_PTNH_WAWF_NOTIFICATION@NAVY.MIL| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|WSS| 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||| FIRST ARTICLE APPROVAL--CONTRACTOR TESTING (SEP 1989)|10||||||||||| NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (OCT 2020)(DEVIATION 2020-O0008)|1|| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (OCT 2025)|13|||||||||||||| BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024)|1|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAR 2025)(DEVIATION 2025-O0003 AND2025-O0004))|13|332911|750 (# of employees)|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||X| 1. NAVSUP WSS Mechanicsburg will be considering past performance in the evaluation of offers. See Clause 252.213-7000 and NAVSUP WSS term WSSTERMMZ01. 2. 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 in the mail, transmitted by facsimile, or sent by other electronic methods, such as email. The Government's acceptance of the contract proposal constitutes bilateral agreement to "issue" contractual documents as detailed herein. 3. The following proposed delivery schedule applies: WELD PROCEDURES 120 DAYS AFTER CONTRACT AWARD APPROVAL MUST BE OBTAINED PRIOR TO PERFORMING WELDING RADIOGRAPHIC SHOOTING SKETCHES (RSS) 45 DAYS ADC DD OF RSS DD APPROVAL OF RADIO RSS 30 DAYS AFTER RECEIPT PRODUCTION RADIOGRAPHY (PR) 135 DAYS AFTER APPROVAL OF RSS DD APPROVAL OF PR FORGING MANUFACTURING SKETCH 90 DAYS ADC FORGING MANUFACTURING SKETCH APPROVAL 120 DAYS AFTER FMS RECEIPT FORGING REPORT 330 DAYS AFTER FMS APPROVAL FORGING REPORT APPROVAL 90 DAYS AFTER RECEIPT Final delivery of material shall be on or before 362 days after the effective date of the contract. 4. Drawings associated with this solicitation will be made available on the individual solicitation page on Contract Opportunities on the SAM.gov website. Drawings have restricted access which needs to be approved. Once access has been requested, qualified Contractors shall email the POC listed on the solicitation to inform them of the request. 5. This requirement requires access to classified drawings. A facility clearance may be required in accordance with FAR 52.204-2. 6. 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 FAR Clause 52.211-14, Notice of Priority Rating for National Defense, Emergency Preparedness, and Energy Program Use. 7. The resultant award of this solicitation will be issued bilaterally, requiring the contractor's written acceptance prior to execution. \ 1. SCOPE 1.1 The material covered in this contract/purchase order will be used in a crucial shipboard system. The use of incorrect or defective material would create a high probability of failure resulting in serious personnel injury, loss of life, loss of vital shipboard systems, or loss of the ship itself. Therefore, the material has been designated as SPECIAL EMPHASIS material (Level I, Scope of Certification, or Quality Assured) and special control procedures are invoked to ensure receipt of correct material. 2. APPLICABLE DOCUMENTS 2.1 Order of Precedence - In the event of a conflict between the text of this contract/purchase order and the references and/or drawings cited herein, the text of this contract/purchase order must take precedence. Nothing in this contract/purchase order, however, must supersede applicable laws and regulations unless a specific exemption has been obtained. 2.2 Identification of Classified Documents - This contract/purchase order requires the Contractor to have authorized access to classified documents in accordance with the attached Contract Security Classification Specification (DD Form 254). The classified documents and security level are: ;4384676 - CONFIDENTIAL; 2.3 Applicable Documents - The document(s) listed below form a part of this contract/purchase order including modifications or exclusions. 2.3.1 "Document References" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. 2.3.2 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. 2.3.3 Documents, drawings, and publications supplied are listed under "Drawing Number". These items should be retained until an award is made. DRAWING DATA=EB-2937 |96169| B|SP |D|0001 | B|49998|0568465 DRAWING DATA=EB-2937 |96169| B|SP |D|0002 | B|49998|0262311 DRAWING DATA=EB-2937 |96169| B|SP |D|0003 | B|49998|0457001 DRAWING DATA=EB-2937 |96169| B|SP |D|0004 | B|49998|0494479 DRAWING DATA=EB-2937 |96169| B|SP |D|0005 | B|49998|0557624 DRAWING DATA=EB-2937 |96169| B|SP |D|0006 | B|49998|0572669 DRAWING DATA=EB-2937 |96169| B|SP |D|0007 | B|49998|0588302 DRAWING DATA=EB-2937 |96169| B|SP |D|0008 | B|49998|0487356 DRAWING DATA=EB-2937 |96169| B|SP |D|0009 | B|49998|0641401 DRAWING DATA=EB-2937 |96169| B|SP |D|0010 | B|49998|0609048 DRAWING DATA=EB-2937 |96169| B|SP |D|0011 | B|49998|0332061 DRAWING DATA=EB-3644 |96169| -|SP |D|0001 | -|49998|0303997 DRAWING DATA=EB-3644 |96169| -|SP |D|0002 | -|49998|0246508 DRAWING DATA=EB-3644 |96169| -|SP |D|0003 | -|49998|0249290 DRAWING DATA=EB-3644 |96169| -|SP |D|0004 | -|49998|0381855 DRAWING DATA=EB-3644 |96169| -|SP |D|0005 | -|49998|0334460 DRAWING DATA=EB-3644 |96169| -|SP |D|0006 | -|49998|0296015 DRAWING DATA=EB-3644 |96169| -|SP |D|0007 | -|49998|0364993 DRAWING DATA=EB-3644 |96169| -|SP |D|0008 | -|49998|0235376 DRAWING DATA=4384676 |53711| C| |D|0001 | C|00026|0000000 DRAWING DATA=5959302 |53711| B| |D|0001 | B|00026|0000000 DRAWING DATA=5959302 |53711|B1|1N |D|0001 |B1|00026|0000000 DRAWING DATA=5959302B2 |53711| A|ER |D|0001 | A|00026|0000000 DRAWING DATA=5959302B3 |53711| A|ER |D|0001 | A|00026|0000000 DRAWING DATA=5959302B5 |53711| B|ER |D|0001 | B|00026|0000000 DRAWING DATA=5959311 |53711| C| |D|0001 | C|00026|0000000 DRAWING DATA=5959311C3 |53711| B|ER |D|0001 | B|00026|0000000 DRAWING DATA=5959311C4 |53711| B|ER |D|0001 | B|00026|0000000 DRAWING DATA=5959311C5 |53711| A|ER |D|0001 | A|49998|0674623 DRAWING DATA=5959311C6 |53711| A|ER |D|0001 | A|49998|0236936 DRAWING DATA=5959311C7 |53711| A|ER |D|0001 | A|49998|0228015 DOCUMENT REF DATA=FED-STD-H28 | | |B |190424|A| | | DOCUMENT REF DATA=FED-STD-H28 |0020| |B |941221|A| |01| DOCUMENT REF DATA=ANSI/ASQ Z1.4 | | | |080101|A| | | DOCUMENT REF DATA=QQ-N-281 | | |D |851023|A|2 | | DOCUMENT REF DATA=QQ-N-286 | | |G |001207|A| | | DOCUMENT REF DATA=ASTM-B367 | | | |130701|A| | | DOCUMENT REF DATA=ASTM-B564 | | | |191101|A| | | DOCUMENT REF DATA=MIL-STD-792 | | |F |060519|A| | | DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | | DOCUMENT REF DATA=ASTM-E1417 | | | |160615|A| | | DOCUMENT REF DATA=ASTM-E1444 | | | |160601|A| | | DOCUMENT REF DATA=MIL-STD-2035 | | |A |950515|A| | | DOCUMENT REF DATA=MIL-STD-2132 | | |D |080310|F| |01| DOCUMENT REF DATA=MIL-STD-2197 | | | |890328|A| | | DOCUMENT REF DATA=ASTM-D4066 | | | |130701|A| | | DOCUMENT REF DATA=SAE AMS 6931 | | |D |171201|A| | | DOCUMENT REF DATA=ISO_9001 | | | |081115|A| | | DOCUMENT REF DATA=ISO10012 | | | |030415|A| | | DOCUMENT REF DATA=MIL-C-14550 | | |B |870320|A|3 | | DOCUMENT REF DATA=MIL-DTL-15024 | | |G |180303|A| | | DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | | DOCUMENT REF DATA=MIL-DTL-24252 | | |E |061108|F| | | DOCUMENT REF DATA=QPL 25027 | | |17 |000207|A| | | DOCUMENT REF DATA=MIL-DTL-32286 | | | |090408|A|2 | | 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 | | | |181118|A| | | DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | | DOCUMENT REF DATA=AIA/NAS NASM 17828 | | |1 |130430|A| | | DOCUMENT REF DATA=AIA/NAS NASM 25027 | | |1 |121221|A| | | DOCUMENT REF DATA=S9074-AQ-GIB-010/248 | | |1 |191112|A| | | DOCUMENT REF DATA=T9074-AS-GIB-010/271 | | |1 |140911|A| | | DOCUMENT REF DATA=S9074-AR-GIB-010A/278 (CHG A) | | | |130214|A| | | 3. REQUIREMENTS 3.1 ;Complete 1.5 Inch Non-Rated Seawater Flanged by Buttweld Combination Hull and Backup Ball Valve, must be in accordance with NAVSEA drawing 803-5959302 assembly A with General Notes on NAVSEA drawing 803-5959311 and provided liabilities, except as amplified or modified herein. Less Hydraulic Actuator (Item 54) and Hull Fasteners (Items 17 and 33).; 3.1.1 ;Bolt holes on mounting flanges and dowel pin holes for actuator locating must not be drilled.; 3.1.2 ;All actuator associated mounting parts must be supplied in a bag attached to the valve.; 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, Item 1 and Access Cover, Item 2; Material - ;UNS N06625 per E.B.Spec 2937 or ASTM B564, as modified by General Note 2.E; Part - ;Stems, Items 7 and 8; Material - ;MIL-DTL-24252, Composition 1, Condition CA-7; Part - ;Stem Sleeves, Items 11 and 12; Material - ;E.B.Spec 3644, to be electroplated in accordance with MIL-STD-2197, Class 1 with material in accordance with MIL-C-14550. Electroplating to be accomplished after Dye Penetrant Inspection of Sleeves in the area shown on drawing; Part - ;Studs, Item 34; Material - ;MIL-DTL-1222, Type IV, Grade 500 (QQ-N-286), Annealed and Age Hardened, and marked .K.; PART - ;Self-Locking Hex Nuts, Item 44; MATERIAL - QQ-N-281, class A annealed (hot finished or cold drawn) or class B cold drawn. All material must be from the same class. SELF-LOCKING ELEMENT- ASTM-D4066, Group 01, Class 1 or 2, Grade 1 Part - ;Balls, Items 4 and 5; Material - SAE-AMS-6931 OR Centrifugally cast 6AL-4V, ASTM-B367, Grade C-5, with mechanical properties as listed in supplementary Requirement S6. Note: Mechanical properties for bars, forgings and forging stock over 10" must be as specified in the applicable drawing. If the mechanical properties are not provided in the drawing, the mechanical properties specified in SAE-AMS-6931 Table 2 for material 6" to 10", must be applied. Part - ;Seats, Item 6 (Q3); Material - MD71-GG Mearthane (Graphite Filled Urethane). Material must be manufactured by Mearthane Products Inc. Cranston, RI. (Properties Specified Below Only) ITEM PROPERTY ASTM TEST METHOD VALUE (A) Hardness D2240 70 +/- 5 Shore D (B) Specific Gravity D792 1.18 +/- 0.02 (C) Tensile Strength D412 (DIEC) 5000 PSI MIN (D) Compression-Defl D575 700 PSI MIN @ 2% DEF. (E) Tensile Impact D1822 300 FT-LB/SQ IN (Note 1) (TYPE L SPECIMEN) (F) Water Absorption D570 1.5% MAX (1 Week at R.T.) Note 1: These values are minimum averages. Separate specimen values may not vary more than 25% under the specified minimum. 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 is still required, but certifications are only required as listed below. Test - ;Liquid Penetrant Inspection; Item - ;Studs, Item 34; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Test - Quality Conformance Tests Item - Self-Locking Nuts Performance - ;NASM25027; Acceptance - ;NASM25027; Attribute - Certificate of Completion Item - Self-Locking Nut Nonmetallic Insert Performance - ;ASTM-D4066, Group 01, Class 1, Grade 1; Attribute - Certificate of Compliance Item - Self-Locking Nuts Performance - This Certificate must state that self-locking nuts were manufactured by an approved source. Approved sources are those listed on QPL-25027 for the appropriate fastener. This QPL may also be considered as approved sources for Heavy Hex self-locking nuts. Attribute - Annealing and Age Hardening Item - ;Studs, Item 34; Performance - QQ-N-286 Test - ;Dye Penetrant Inspection for Non-Magnetic Grades; Item - ;Self-Locking Hex Nuts, Item 44; Performance - T9074-AS-GIB-010/271 or ASTM-E1417/ASTM-E1444 (Method C solvent removal techniques must not be used on thread) Acceptance - ;NASM25027; Test - ;Dye Penetrant Inspection per Supplementary Note S4.F(3); Item - ;Stem Sleeves, Items 11 and 12; Performance - T9074-AS-GIB-010/271 Acceptance - MIL-STD-2035 Test - ;Dye Penetrant Inspection; Item - ;All cladded surfaces after final machining per General Note 2.D.(2)(D); Performance - T9074-AS-GIB-010/271 Acceptance - MIL-STD-2035 Test - ;Dye Penetrant Inspection of Final External Surface per General Note 3.T; Item - ;Body, Item 1; Access Cover, Item 2; Stems, Items 7 and 8; and Stem Sleeves, Items 11 and 12; Performance - T9074-AS-GIB-010/271 Acceptance - MIL-STD-2035 Test - Pressure Tests Item - Each Assembly Performance - ;General Note 6.C.(1) Group II; Acceptance - ;Hydrostatic Test - No Weeping, No Porosity and No Permanent Deformation. Seat Tightness - No Leakage Allowed; Test - Ultrasonic Inspection Item - ;Stems, Items 7 and 8; Performance - MIL-STD-2132 and MIL-DTL-24252 Acceptance - MIL-DTL-24252 Test - ;Ultrasonic Inspection; Item - ;Body, Item 1 and Access Cover, Item 2; Performance - ;T9074-AS-GIB-010/271 as modified by E.B. Spec 2937; Acceptance - ;E.B. Spec 2937; 3.4 Radiography is required on ;Stem sleeves, item 11 and item 12 in accordance with drawing 803-5959302 Supplementary Note S4.F(2); . 3.5 Confidential Hydrostatic Test Pressures - When test pressures are confidential, certification must reference ;803-4384676 REV C; and the item number to which the item was tested in lieu of the actual pressures. Any drawing requirement to mark the working pressure on the item does not apply and is strictly prohibited. 3.6 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. 3.7 ;Thrust washers, Items 15 and 16 to be Nylatron GSVQ-II (Nylon 66 with molybdenum disulfide) in accordance with MIL-DTL-32286, as manufactured by Quadrant Engineering Plastic Products (EPP) or Delrin AF DE588.; 3.8 ;The original melter/converter and converter of MIL-DTL-24252 material must be qualified in accordance with paragraph 3.2.6 of MIL-DTL-24252.; 3.9 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. 3.10 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number ;CSD018 and CSD099; in ECDS at https://register.nslc.navy.mil/ 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 ;2.C.; of drawing ;803-5959311; . 3.11.1 ;Naval Ordnance Systems Command OD 10362 First Revision dated 15 Aug 1961 is provided by Contract Support Library Reference Number CSD018.; 3.11.2 CSD099 provides guidance for acceptance/rejection of teflon-coated valve balls after valve assembly production testing. 3.12 Slow Strain Rate Tensile Test Laboratories - The Slow Strain Rate Tensile Test of QQ-N-286 must be performed by one of the following laboratories: Huntington Alloys, a Special Metals Company Attn: Bill Bolenr 3200 Riverside Drive Huntington, WV 257059 Phone: (304) 526-5889 FAX: (304) 526-5973 Metallurgical Consultants, Inc. Attn: W. M. Buehler 4820 Caroline PO Box 88046 Houston, TX 77288-0046 Phone: (713) 526-6351 FAX: (713) 526-2964 Naval Surface Warfare Center, Carderock Division Attn: Eric Focht Code 614 9500 Macarthur Blvd West Bethesda, MD 20817-5700 Phone: (301) 227-5032 FAX: (301) 227-5576 Teledyne Allvac Attn: Dr. W. D. Cao 2020 Ashcraft Ave. Monroe, NC 28110 Phone: (704) 289-4511 FAX: (704) 289-4269 Westmoreland Mechanical Testing and Research Inc. Attn: Andrew Wisniewski P.O. Box 388 Youngstown, PA 15696-0388 Mannesmann Rohrenwerke Mannesmann Forschungsinstitut (MFI) Attn: Dr. Weiss Postfach 251160 47251 Duisburg Germany Phone: 011-49-0203-9993194 FAX: 011-49-0203-9994415 ThyssenKrupp VDM USA, Inc. Attn: D. C. Agarwal 11210 Steeplecrest Drive, Suite 120 Houston, TX 77065-4939 Phone: (281) 955-6683 3.13 K-MONEL Fasteners - Material must be heat treated per QQ-N-286. 3.13.1 Fasteners that have been hot or cold headed or roll threaded must be solution annealed followed by age hardening subsequent to all heading and thread rolling operations. The mechanical properties on certifications must be actual properties of the annealed and age hardened material and must meet the requirements of QQ-N-286. 3.13.2 QQ-N-286 fasteners that have been headed and/or roll threaded must not beage hardened unless the material has been solution annealed subsequent to the heading and threading operations. Threads formed after the final age hardening heat treatment must be cut or ground only. 3.14 K-MONEL Fasteners - K-MONEL externally threaded fasteners must have mechanical properties determined in accordance with MIL-DTL-1222. Test results must include Tensile, Yield, Elongation and Hardness as required by MIL-DTL-1222. (The Hardness tests must be performed on a full size fastener.) 3.14.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222. 3.14.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order. 3.15 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. 3.15.1 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. 3.15.2 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. 3.15.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.16 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. 3.17 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.18 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/ 3.19 Thread Lubricant - Thread lubricants containing molybdenum disulfide must 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 must be used as a replacement when thread lubricant is required for assembly. 3.20 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 884245655X; ) 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. 3.21 Forging Sketches and FAT for Forgings - Forging Sketches and First Article Testing for forgings are required for ;Body, Item 1 and Access Cover, Item 2; per ;General Note 2.N; . 3.22 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 welding and brazing. Repair welding is not permitted ;on MIL-DTL-24252 material; . Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing. 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 using the ECDS (Electronic Contractor Data Submission) system at https://register.nslc.navy.mil/ 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. 3.25 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. 3.26 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. 3.26.1 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 ^ 3.27 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. 3.28 Radiography (RT) - Radiography must be performed in accordance with T9074-AS-GIB-010/271. RT acceptable criteria for castings to be criticality level I per 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. 3.28.1 See CDRL DI-MISC-80678 (RSS) - The Contractor or activity performing the radiography must be responsible for preparing the radiographic shooting sketches (RSS) in accordance with T9074-AS-GIB-010/271. Shooting sketch approval is 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 data has been previously approved by a Navy activity, the original approval letter must be submitted at the same time as RT film and reader sheet submittal. 3.28.2 All pieces radiographed must be permanently marked with "RT" and a unique RT serial number. (The unique RT serial number must be directly traceable to the RT film.) 3.28.3 See CDRL DI-MISC-80678 (Production Radiography) - Production Radiography requires final acceptance by the Navy. The items listed below must be submitted for final acceptance, cataloging, file, and retention. They must be submitted and approved prior to shipment of the applicable hardware. However, when the source certification clause is invoked, they must be submitted a minimum of forty-five (45) working days prior to the date of source certification inspection. (a) Film (b) RSS/RSSS (c) RS (Reader Sheets) (d) Documentation record listing the part number, heat/lot traceability, and theunique RT serial number (which is traceable to the RT film and reader sheet) 3.29 See CDRL DI-FORG-80412 (Forging Manufacturing Sketches) and DI-FORG-80962 (First Article Forging Report) - The Forging Sketch must include additional First Article requirements as follows: 1 - 100% Ultrasonic Testing must be performed. 2 - A minimum of two longitudinal and two transverse tensile tests must be taken. One of each must be taken near the geometric center of the forging. Other longitudinal and transverse tensile tests must be taken from areas representing all section thicknesses. (section thickness is based upon final machined dimensions) 3.30 See CDRLs DI-MISC-80875 (welding procedures) and DI-MISC-80...
