COMB HULL&BP
CONTACT INFORMATION|4|N743.43|WV4|717-605-4237|william.e.norman2@navy.mil| ITEM UNIQUE IDENTIFICATION AND VALUATION (MAR 2016)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP ... CONTACT INFORMATION|4|N743.43|WV4|717-605-4237|william.e.norman2@navy.mil| ITEM UNIQUE IDENTIFICATION AND VALUATION (MAR 2016)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP REVIEW FEB 1991)(FEB 1999)|1|See Specifications Sections C & E| INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2||| TIME OF DELIVERY (JUNE 1997)|20|1|10|500 days or best offer|||||||||||||||||| GENERAL INFORMATION-FOB-DESTINATION|1|b| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)|16|Combo (Invoice & Receiving)|N/A|TBD|N00104|TBD|DCMA NSEO (S4306A)|N50286|TBD|||DCMA NSEO (S4306A)|||||| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUNE 2003)|6|365 days after acceptance|365 days after acceptance||||| WARRANTY OF DATA--BASIC (MAR 2014)|2||| BUY AMERICAN --FREE TRADE AGREEMENTS--BALANCE OF PAYMENTS PROGRAM - BASIC(DEVIATION 2020-O0019) (JUL 2020))|3|||| NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (OCT 2020)(DEVIATION 2020-O0008)|1|| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2020)|13|||||||||||||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM CERTIFICATE (DEVIATION 2020-O0019) (JUL 2020))|3|||| BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (NOV 2014)|1|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAR 2020)|13|332911|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.DD1423 Data Item A001 (Inspection and Test Plan) may be waived if already on file at NAVSUP WSS Mechanicsburg. 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 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 here in. 3.The following proposed delivery schedule applies: Submission of all certification data CDRLS 20 days prior to delivery. PNSY review/acceptance of certification CDRLS 6 working days after receipt Final delivery of material (500 days) 4.NAVSUP WSS Mech will be considering past performance in the evaluation of offers. See Clause 252.213-7000. 5.This requirement falls under the Special Emergency Procurement Authority(SEPA) in accordance with 41 U.S.C. 1903 and Class Deviation 2018-O0013. 6. This requirement requires access to confidential drawings. These drawings are not required to submit a quote. However, in the event of an award, a facility clearance may be required in accordance with FAR 52.204-2. \ 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. 2.3 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. DRAWING DATA=DM117384 |96169| A| |D|0001 | A|49998|0055082 DRAWING DATA=DM117384 |96169| A| |D|0001.A | A|49998|0042263 DRAWING DATA=DM117384 |96169| A| |D|0002 | A|49998|0053468 DRAWING DATA=DM117384 |96169| A| |D|0003 | A|49998|0059744 DRAWING DATA=DM117384 |96169| A| |D|0004 | A|49998|0012659 DRAWING DATA=DM117384 |96169| A| |D|0005 | A|49998|0028276 DRAWING DATA=DM117384 |96169| A| |D|0006 | A|49998|0025657 DRAWING DATA=DM117384 |96169| A| |D|0007 | A|49998|0028768 DRAWING DATA=DM117384 |96169| A| |D|0008 | A|49998|0029722 DRAWING DATA=DM117384 |96169| A| |D|0009 | A|49998|0251337 DRAWING DATA=DM117384 |96169| A| |D|0010 | A|49998|0024477 DRAWING DATA=DM117384 |96169| A| |D|0011 | A|49998|0023361 DRAWING DATA=DM117384 |96169| A| |D|0012 | A|49998|0023810 DRAWING DATA=DM117384 |96169| A| |D|0013 | A|49998|0018527 DRAWING DATA=256172 |43689| J| |D|0001 | J|49998|0450942 DRAWING DATA=4384676 |53711| C| |D|0001 | C|00026|0000000 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=4385050 |53711| C| |D|0001 | C|49998|0227949 DRAWING DATA=4385050 |53711| C| |D|0002 | C|49998|0305552 DRAWING DATA=4385050 |53711| C| |D|0003 | C|49998|0401935 DRAWING DATA=4385050 |53711| C| |D|0004 | C|49998|0334168 DRAWING DATA=4385050 |53711| C| |D|0005 | C|49998|0350929 DRAWING DATA=4385050 |53711| C| |D|0006 | C|49998|0250462 DRAWING DATA=4385050 |53711| C| |D|0007 | C|49998|0191986 DRAWING DATA=4385050 |53711| C| |D|0008 | C|49998|0314531 DRAWING DATA=4385050 |53711| C| |D|0009 | C|49998|0265988 DRAWING DATA=4385050 |53711| C| |D|0010 | C|49998|0210216 DRAWING DATA=4385050 |53711| C| |D|0011 | C|49998|0253021 DRAWING DATA=4385050 |53711| C| |D|0012 | C|49998|0254114 DRAWING DATA=4385050 |53711| C| |D|0013 | C|49998|0197208 DRAWING DATA=4385050 |53711| C| |D|0014 | C|49998|0253167 DRAWING DATA=4385050 |53711| C| |D|0015 | C|49998|0204941 DRAWING DATA=4385050 |53711| C| |D|0016 | C|49998|0233116 DRAWING DATA=4385050 |53711| C| |D|0017 | C|49998|0238680 DRAWING DATA=4385050 |53711| C| |D|0018 | C|49998|0098849 DRAWING DATA=4385050-C1 |53711| -|1N |D|0001 | -|49998|0040946 DRAWING DATA=4385050-C2 |53711| -|1N |D|0001 | -|49998|0040858 DRAWING DATA=4385050-C3 |53711| -|1N |D|0001 | -|49998|0041083 DRAWING DATA=4385050-C4 |53711| -|1N |D|0001 | -|49998|0040208 DRAWING DATA=4385050-C5 |53711| -|1N |D|0001 | -|49998|0045691 DRAWING DATA=4385050-C5 |53711| -|1N |D|0002 | -|49998|0018735 DRAWING DATA=4385050-C6 |53711| -|1N |D|0001 | -|49998|0045492 DRAWING DATA=4385050-C6 |53711| -|1N |D|0002 | -|49998|0017033 DOCUMENT REF DATA=FED-STD-H28 | | |A |941228|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-B369 | | | |090401|A| | | DOCUMENT REF DATA=ASTM-B505 | | | |140401|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=ASTM-E1417 | | | |130601|A| | | DOCUMENT REF DATA=ASTM-E1444 | | | |160616|A| | | DOCUMENT REF DATA=MIL-STD-2035 | | |A |950515|A| | | DOCUMENT REF DATA=SAE AMS 2631 | | |E |171201|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-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-N-25027 |0001| |A |990331|A| 1| | 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=ANSI/NCSL Z540.3 | | | |130326|A| | | DOCUMENT REF DATA=AIA/NAS NASM 25027 | | |1 |121221|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 complete 1 1/2 Inch Hull and Backup Ball Valve to be in accordance with Newport News Drawing 256172 Assembly "AF-3", NAVSHIPs Drawing 803-4385050, and NAVSHIPs Drawing 803-4384678 along with attached DRNs C1 thru C6, except as amplified or modified herein. (Less operators and hull fasteners). NOTE: Line end is to be undrilled.; 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 on Drawing 256172 (Piece 72-S1 on Drawing 803-4385050) and Tailpiece, Piece 75-S1 on Drawing 803-4385050; Material - ;ASTM-B369, Alloy UNS C96400; Part - ;Stems, Piece 2 on Drawing 256172 and Piece 14 on Drawing 803-4385050; Material - ;QQ-N-286, Form 2, Annealed and Age Hardened or Form 7, Annealed and Age Hardened; Part - ;Stem Retaining Nut, Piece 10 and Stem Retaining Nut, Piece 12 on Drawing 803-4385050; Material - ;ASTM-B505, Alloy UNS C90300; Part - ;Studs, Piece 62 on Drawing 803-4385050; Material - ;MIL-DTL-1222, QQ-N-286, Annealed and Age Hardened, and Marked .K.; Part - ;Body Insert (Q3), Piece 68-S1 on Drawing 803-4385050; Material - ;QQ-N-281, Class A, Hot Finished; PART - ;Self-Locking Heavy Hex Nuts, Piece 76 on Drawing 803-4385050, Part Number M25027/1-20C; MATERIAL - QQ-N-281, Class A or B, in accordance with MIL-N-25027/1. All material shall be the same Class. SELF-LOCKING ELEMENT - ASTM-D4066, Group 01, Class 1 or 2, Grade 1. Part - ;Self-Locking Socket Head Cap Screws (Q3), Piece 36 on Drawing 803-4385050; Material - ;MIL-DTL-1222, TYPE II, QQ-N-286, Annealed and Age Hardened, and marked .K. . Self- Locking Elements in accordance with MIL-DTL-18240.; For Boilerplate R00375, Part - ;Ball, Piece 7 and Ball, Piece 8 on Drawing 803-4385050; 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 (Q3), Piece 9 on Drawing 803-4385050; 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 - Quality Conformance Tests Item - Self-Locking Nuts Performance - ;NASM25027 and MIL-N-25027/1; Acceptance - ;NASM25027 and MIL-N-25027/1; Attribute - Certificate of Completion Item - Self-Locking Nut Nonmetallic Insert Performance - ASTM-D4066, Group 01, Class 1 or 2, Grade 1 Attribute - Certificate of Compliance Item - Self-Locking Nuts Performance - This Certificate shall 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, Piece 62, Self-Locking Socket Head Cap Screws, Piece 36 on Drawing 803-4385050 and Stems, Piece 2 on Drawing 256172 and Piece 14 on Drawing 803-4385050; Performance - QQ-N-286 Test - ;Liquid Penetrant Inspection; Item - ;Studs, Piece 62 and Self-Locking Socket Head Cap Screws, Piece 36 on Drawing 803-4385050; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Test - ;Dye Penetrant Inspection for Non-Magnetic Grades; Item - ;Self-Locking Heavy Hex Nuts, Piece 76 on Drawing 803-4385050; Performance - T9074-AS-GIB-010/271 or ASTM-E1417/ASTM-E1444 (Method C solvent removal techniques shall not be used on thread) Acceptance - ;NASM25027 with sampling in accordance with MIL-N-25027/1; Test - ;Dye Penetrant Inspection; Item - ;Stem, Piece 2 on Drawing 256172 and Stems, Piece 14 and Body Insert, Piece 68-S1 on Drawing 803-4385050; Performance - T9074-AS-GIB-010/271 Acceptance - MIL-STD-2035 Test - Weldability Test of ASTM-B369 material Item - ;Body, Piece 1 on Drawing 256172 (Piece 72-S1 on Drawing 803-4385050) and Tailpiece, Piece 75-S1 on Drawing 803-4385050; Performance - ASTM-B369 Acceptance - ASTM-B369 Test - Pressure Tests Item - Each Assembly Performance - ;General Note 18 on Drawing 256172; Acceptance - ;General Note 18 on Drawing 256172; 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/-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. 3.5 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; . 3.6 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/ 3.6.1 CSD099 provides guidance for acceptance/rejection of teflon-coated valve balls after valve assembly production testing. 3.7 A visual inspection shall be performed on the finished seat with acceptance criteria on critical surfaces per CSD167 in the ECDS (Electronic Contractor Data Submission) system at: https://register.nslc.navy.mil/. 3.8 K-MONEL Fasteners - Material must be heat treated per QQ-N-286. 3.8.1 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. 3.8.2 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. 3.9 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.) 3.9.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222. 3.9.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order. 3.10 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. 3.10.1 Testing for Socket Head Cap Screws shall be in accordance MIL-DTL-1222, paragraphs 4.5.2.3 and 4.5.2.3.1. 3.10.2 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. 3.10.3 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. 3.11 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. 3.12 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.13 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. 3.13.1 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. 3.13.2 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. 3.13.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.14 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. 3.15 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. 3.16 O-ring grooves and mating sealing surfaces shall 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 shall 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/ 3.17 ;Radiography is required on Body, Piece 1 on Drawing 256172 (Piece 72-S1 on Drawing 803-4385050) and Tailpiece, Piece 75-S1 on Drawing 803-4385050; 3.18 ;Shim material for Piece 68-S2 to be in accordance with DM117384. NOTE: Quantitative chemical and mechanical analysis is not required.; 3.19 ;Thrust Washers (Pieces 18, 19, and 20) to be made from either Nylatron GSVQ II or Delrin-AF-DE588.; 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 884305664; ) 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 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 ;UNS C90300 material; . Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing. 3.22 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: Frank Veltry huntington, WV 25705 Phone: (304) 526-5759 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 3.23 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. 3.24 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. 3.24.1 Marking of material with a Material Designator per the Drawing is also prohibited, with the exception of Fasteners. Fasteners must be marked with a Material Symbol/Designator as specified elsewhere in this contract. 3.25 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. 3.25.1 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. 3.25.2 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/ 3.25.3 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. 3.26 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. 3.27 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. ^ QUALITY ASSURANCE REQUIREMENTS ^ 3.28 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. 3.29 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. 3.29.1 Approval of the Contractor's qualification data shall be obtained prior to performing any welding (production or repair). 3.29.2 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 ...
Data sourced from SAM.gov.
View Official Posting »