48--VALVE,BALL
CONTACT INFORMATION|4|N742.10|WV2|(717) 605-4056|madison.m.gray4.civ@us.navy.mil| ITEM UNIQUE IDENTIFICATION AND VALUATION (JAN 2023)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (... CONTACT INFORMATION|4|N742.10|WV2|(717) 605-4056|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 and Receiving Report (COMBO) Certifications - Stand-alone Receiving Report |N/A|TBD|N00104|TBD|Material - S4306A; Certifications - N64498|N50286|TBD|TBD|N/A|N/A|Certifications - N64498|N/A|N/ A|See DD Form 1423|N/A| 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 date of delivery|one year from date of delivery||||| WARRANTY OF DATA--BASIC (MAR 2014)|2||| BUY AMERICAN --FREE TRADE AGREEMENTS--BALANCE OF PAYMENTS PROGRAM - BASIC (FEB2024))|11|||||||||||| NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (OCT 2020)(DEVIATION 2020-O0008)|1|| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2023)|13|||||||||||||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024))|5|||||| BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024)|1|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (FEB 2024)|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 sent 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 delivery schedule applies: RADIOGRAPHIC SHOOTING SKETCHES (RSS) 45 DAYS ADC DD APPROVAL OF RADIO RSS 30 DAYS AFTER RECEIPT PRODUCTION RADIOGRAPHY (PR) 135 DAYS AFTER APPROVAL OF RSS DDAPPROVAL OF PR WELD PROCEDURES 120 DAYS AFTER CONTRACT AWARD APPROVAL MUST BE OBTAINED PRIOR TO PERFORMING WELDING Submission of Certification Data CDRLs will be on or before 20 days prior to scheduled delivery. PNSY review/acceptance of Certification CDRLs 6 working days after receipt of Certification DD 1423 CDRLs. Final delivery of material shall be on or before 450 days after the effective date of the contract. 4. 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. 5. The resultant award of this solicitation will be issued bilaterally, requiring the contractor's written acceptance prior to execution. 6. Drawings associated with this solicitation will be made available on the individual solicitation page on Contracts 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. 7. This requirement requires access to classified 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. 8. 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: ;6404016 - 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 Documents, drawings, and publications supplied are listed under "Drawing Number". These items should be retained until an award is made. 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 "Document References" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. DRAWING DATA=DF330613C10 |53711| A|ER |D|0001 | A|49998|0178040 DRAWING DATA=DF330613C11 |53711| B|ER |D|0001 | B|49998|0307832 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 |80064| C| |D|0001 | C|49998|0451442 DRAWING DATA=4385050 |80064| C| |D|0002 | C|49998|0678090 DRAWING DATA=4385050 |80064| C| |D|0003 | C|49998|0767802 DRAWING DATA=4385050 |80064| C| |D|0004 | C|49998|0647579 DRAWING DATA=4385050 |80064| C| |D|0005 | C|49998|0676019 DRAWING DATA=4385050 |80064| C| |D|0006 | C|49998|0560045 DRAWING DATA=4385050 |80064| C| |D|0007 | C|49998|0427112 DRAWING DATA=4385050 |80064| C| |D|0008 | C|49998|0680510 DRAWING DATA=4385050 |80064| C| |D|0009 | C|49998|0574591 DRAWING DATA=4385050 |80064| C| |D|0010 | C|49998|0463459 DRAWING DATA=4385050 |80064| C| |D|0011 | C|49998|0562323 DRAWING DATA=4385050 |80064| C| |D|0012 | C|49998|0533163 DRAWING DATA=4385050 |80064| C| |D|0013 | C|49998|0430211 DRAWING DATA=4385050 |80064| C| |D|0014 | C|49998|0553678 DRAWING DATA=4385050 |80064| C| |D|0015 | C|49998|0424546 DRAWING DATA=4385050 |80064| C| |D|0016 | C|49998|0511681 DRAWING DATA=4385050 |80064| C| |D|0017 | C|49998|0490597 DRAWING DATA=4385050 |80064| C| |D|0018 | C|49998|0161231 DRAWING DATA=4385050-C4 |53711| -|1N |D|0001 | -|49998|0040208 DRAWING DATA=6404016 |53711| B| |F|0001 | B|00026|0000000 DRAWING DATA=6405351 |53711| A| |D|0001 | A|49998|0068528 DRAWING DATA=6405351 |53711| A| |D|0001.A | A|49998|0043345 DRAWING DATA=6405351 |53711| A| |D|0002 | A|49998|0024372 DRAWING DATA=6405351 |53711| A| |D|0003 | A|49998|0048337 DRAWING DATA=6405351 |53711| A| |D|0004 | A|49998|0099367 DRAWING DATA=6405351 |53711| A| |D|0004.A | A|49998|0066936 DRAWING DATA=6405351 |53711| A| |D|0005 | A|49998|0052935 DRAWING DATA=6405351 |53711| A| |D|0005.A | A|49998|0045852 DRAWING DATA=6405351 |53711| A| |D|0006 | A|49998|0069025 DRAWING DATA=6405351 |53711| A| |D|0006.A | A|49998|0074653 DRAWING DATA=6405351 |53711| A| |D|0006.B | A|49998|0067651 DRAWING DATA=6405351 |53711| A| |D|0006.C | A|49998|0068861 DRAWING DATA=6405351 |53711| A| |D|0006.D | A|49998|0066196 DRAWING DATA=6405351 |53711| A| |D|0006.E | A|49998|0068551 DRAWING DATA=6405351 |53711| A| |D|0006.F | A|49998|0071144 DRAWING DATA=6405351 |53711| A| |D|0006.G | A|49998|0072373 DRAWING DATA=6405351 |53711| A| |D|0006.H | A|49998|0069052 DRAWING DATA=6405351 |53711| A| |D|0006.J | A|49998|0053342 DRAWING DATA=6405351 |53711| A| |D|0007 | A|49998|0036178 DRAWING DATA=6405351 |53711| A| |D|0008 | A|49998|0047650 DRAWING DATA=6405351 |53711| A| |D|0008.A | A|49998|0046214 DRAWING DATA=6405351 |53711| A| |D|0009 | A|49998|0033667 DRAWING DATA=6405351 |53711| A| |D|0010 | A|49998|0033949 DRAWING DATA=6405351 |53711| A| |D|0011 | A|49998|0038121 DRAWING DATA=6405351 |53711| A| |D|0012 | A|49998|0034092 DRAWING DATA=6405351 |53711| A| |D|0013 | A|49998|0061596 DRAWING DATA=6405351 |53711| A| |D|0013.A | A|49998|0047323 DRAWING DATA=6405351 |53711| A| |D|0013.B | A|49998|0042959 DRAWING DATA=6405351 |53711| A| |D|0013.C | A|49998|0034536 DRAWING DATA=6405351 |53711| A| |D|0013.D | A|49998|0041758 DRAWING DATA=6405351 |53711| A| |D|0014 | A|49998|0028916 DRAWING DATA=6405351 |53711| A| |D|0015 | A|49998|0033225 DRAWING DATA=6405351 |53711| A| |D|0016 | A|49998|0032954 DRAWING DATA=6405351 |53711| A| |D|0017 | A|49998|0032993 DRAWING DATA=6405351 |53711| A| |D|0017.A | A|49998|0028430 DRAWING DATA=6405351 |53711| A| |D|0018 | A|49998|0041883 DRAWING DATA=6405351 |53711| A| |D|0019 | A|49998|0018102 DRAWING DATA=6405351 |53711| A| |D|0020 | A|49998|0040978 DRAWING DATA=6405351 |53711| A| |D|0021 | A|49998|0024729 DRAWING DATA=6405351 |53711| A| |D|0022 | A|49998|0022918 DRAWING DATA=6405351 |53711| A| |D|0023 | A|49998|0022338 DRAWING DATA=6405351 |53711| A| |D|0024 | A|49998|0025996 DRAWING DATA=6405351 |53711| A| |D|0025 | A|49998|0020041 DRAWING DATA=6405351 |53711| A| |D|0026 | A|49998|0022424 DRAWING DATA=6405351 |53711| A| |D|0027 | A|49998|0025693 DRAWING DATA=6405351 |53711| A| |D|0028 | A|49998|0025617 DRAWING DATA=6405351 |53711| A| |D|0029 | A|49998|0054176 DRAWING DATA=6405351 |53711| A| |D|0030 | A|49998|0035399 DRAWING DATA=6405351 |53711| A| |D|0031 | A|49998|0020856 DRAWING DATA=6405351 |53711| A| |D|0032 | A|49998|0023935 DRAWING DATA=6405351 |53711| A| |D|0033 | A|49998|0022020 DRAWING DATA=6405351 |53711| A| |D|0034 | A|49998|0031023 DRAWING DATA=6405351 |53711| A| |D|0035 | A|49998|0022084 DRAWING DATA=6405351 |53711| A| |D|0036 | A|49998|0023967 DRAWING DATA=6408529 |53711| C| |D|0001 | C|49998|0471414 DRAWING DATA=6408529 |53711| C| |D|0001.A | C|49998|0332904 DRAWING DATA=6408529 |53711| C| |D|0001.B | C|49998|0345072 DRAWING DATA=6408529 |53711| C| |D|0002 | C|49998|0298556 DRAWING DATA=6408529 |53711| C| |D|0002.A | C|49998|0303003 DRAWING DATA=6408529 |53711| C| |D|0002.B | C|49998|0319148 DRAWING DATA=6408529 |53711| C| |D|0002.C | C|49998|0235527 DRAWING DATA=6408529 |53711| C| |D|0002.D | B|49998|0276389 DRAWING DATA=6408529 |53711| C| |D|0002.E | B|49998|0260935 DRAWING DATA=6408529 |53711| C| |D|0002.F | B|49998|0243303 DRAWING DATA=6408529 |53711| C| |D|0003 | C|49998|0270451 DRAWING DATA=6408529 |53711| C| |D|0003.A | C|49998|0288663 DRAWING DATA=6408529 |53711| C| |D|0003.B | C|49998|0307445 DRAWING DATA=6408529 |53711| C| |D|0003.C | C|49998|0292708 DRAWING DATA=6408529 |53711| C| |D|0003.D | C|49998|0299361 DRAWING DATA=6408529 |53711| C| |D|0003.E | C|49998|0281233 DRAWING DATA=6408529 |53711| C| |D|0003.F | C|49998|0334124 DRAWING DATA=6408529 |53711| C| |D|0003.G | C|49998|0313284 DRAWING DATA=6408529 |53711| C| |D|0003.H | C|49998|0300646 DRAWING DATA=6408529 |53711| C| |D|0003.J | C|49998|0279814 DRAWING DATA=6408529 |53711| C| |D|0003.K | C|49998|0297569 DRAWING DATA=6408529 |53711| C| |D|0003.L | C|49998|0289795 DRAWING DATA=6408529 |53711| C| |D|0004 | C|49998|0238167 DRAWING DATA=6408529 |53711| C| |D|0005 | A|49998|0142890 DRAWING DATA=6408529 |53711| C| |D|0006 | B|49998|0198379 DRAWING DATA=6408529 |53711| C| |D|0007 | A|49998|0157342 DRAWING DATA=6408529 |53711| C| |D|0008 | A|49998|0166003 DRAWING DATA=6408529 |53711| C| |D|0009 | B|49998|0203178 DRAWING DATA=6408529 |53711| C| |D|0010 | A|49998|0107019 DRAWING DATA=6408529 |53711| C| |D|0011 | C|49998|0192483 DRAWING DATA=6408529 |53711| C| |D|0012 | A|49998|0104270 DRAWING DATA=6408529 |53711| C| |D|0013 | A|49998|0099090 DRAWING DATA=6408529 |53711| C| |D|0014 | A|49998|0107926 DRAWING DATA=6408529 |53711| C| |D|0015 | C|49998|0204749 DRAWING DATA=6408529 |53711| C| |D|0016 | C|49998|0152364 DOCUMENT REF DATA=FED-STD-H28 | | |B |190424|A| | | DOCUMENT REF DATA=FED-STD-H28 |0020| |B |941221|A| |01| DOCUMENT REF DATA=ANSI/ASQ Z1.4 | | | |080101|A| | | DOCUMENT REF DATA=ASTM-B139 | | | |121001|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 | | | |220401|A| | | DOCUMENT REF DATA=ASTM-B369 | | | |200401|A| | | DOCUMENT REF DATA=ASTM-B505 | | | |180301|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=SAE AMS 2631 | | |E |171201|A| | | DOCUMENT REF DATA=ASTM-D4066 | | | |130701|A| | | DOCUMENT REF DATA=ASTM-D6456 | | | |100801|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=QPL 25027 | | |17 |000207|A| | | DOCUMENT REF DATA=MIL-DTL-32258 | | | |210601|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 | | |B |181118|A| | | DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | | DOCUMENT REF DATA=0900-LP-001-7000 | | | |810101|C| |01| 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 ;The complete 2 Inch Combination Hull and Backup Ball Valve required to be in accordance with Naval Sea Systems Command drawing 6408529 Assembly 94 and all DNs, DRNs and ERs provided with this Contract/Purchase Order (less actuator Find Number 42 of NAVSEA drawing 6408529 and hull fasteners Find Numbers 69, 70 of NAVSEA drawing 6408529), except as amplified or modified herein.; 3.1.1 ;Bolt and dowel pin holes on mounting flange(s) and dowel pin holes for actuator locating must not be drilled.; 3.1.2 ;Find Numbers 47, 50, 55, 56, and 57 of drawing 6408529 must be supplied in a bag attached to the valve.; 3.1.3 ;All actuator associated mounting parts must be supplied in bag attached to the valve.; 3.1.4 ;Dimension for Find Number 14 on NAVSEA Drawing 6408529 Sheet 10 from Datum B to the end of the 1.0 inch radius is 1.688 inches.; 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, Find Number 72-S1 and Tailpiece, Find Number 80-S1 of Drawing 6408529; Material - ;ASTM-B369, Alloy UNS 96400; Part - ;Continuous Threaded Studs, Find Number 62 of Drawing 6408529; Material - ;MIL-DTL-1222, Type IV, QQ-N-286, Alloy UNS N05500, Annealed and Age Hardened; PART - ;Self-locking Heavy Hex Nuts, Find Number 43 of Drawing 6408529; MATERIAL - QQ-N-281, Class A or B, with chemical composition in accordance with MIL-DTL-32258. NOTE: All material must be the same Class. SELF-LOCKING ELEMENT - For 250 degree nuts use ASTM-D6456, Type 1 or ASTM-D4066, Group 01, Class 1 or 2, Grade 1, 2, 3, 4, 5,or 6. For 450 degree nuts use ASTM-D6456, Type 1. Part - ;Stem Retaining Nuts, Find Numbers 10 and 12 of Drawing 6408529; Material - ;ASTM-B505, Alloy C90300 or, as an alternate material, ASTM-B139, Alloy C51000, Temper H04 with the following minimum mechanical properties: 55 ksi tensile strength, 22 ksi yield strength, 18% elongation; Part - ;Insert (Q3), Find Number 68-S1 of Drawing 6408529; Material - ;QQ-N-281, Class A, Form 1, Hot finished or Cold drawn, Annealed; Part - ;Straight Ball, Find Number 7 and Angle Ball, Find Number 8 of Drawing 6408529; 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), Find Number 9 of Drawing 6408529; 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 and specifications is still required, but certifications are only required as listed below. Test - Quality Conformance Tests Item - Self-Locking Nuts Performance - ;MIL-DTL-32258; Acceptance - ;MIL-DTL-32258; Attribute - Certificate of Completion Item - Self-Locking Nut Nonmetallic Insert Performance - ;ASTM D6456, Type 1 or ASTM D4066, Group 01, Class 1 or 2, Grade 1, 2, 3, 4, 5, or 6; 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 - ;Stems Find Number 14 and Find Number 15 and Continuous Threaded Studs Find Number 62 of Drawing 6408529; Performance - QQ-N-286 Test - Ultrasonic Inspection on Starting Material Item - ;All Items requiring certification made from QQ-N-286 with a diameter or minimum distance between parallel surfaces of 4 inches or greater of the starting material, or when required by a drawing or specification invoked elsewhere in this contract; Performance - T9074-AS-GIB-010/271 or MIL-STD-2132, and QQ-N-286 Acceptance - QQ-N-286 Test - ;Liquid Penetrant Inspection; Item - ;Continuous Threaded Studs, Find Number 62 on Drawing 6408529; 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 Find Number 43 on drawing 6408529; Performance - T9074-AS-GIB-010/271 or ASTM-E1417/ASTM-E1444 (Method C solvent removal techniques must not be used on thread) Acceptance - ;NASM25027 with sampling in accordance with MIL-DTL-32258; Test - ;Dye Penetrant Inspection; Item - ;Stem, Find Number 15; and Insert (Q3), Find Number 68-S1 of Drawing 6408529; Performance - T9074-AS-GIB-010/271 Acceptance - MIL-STD-2035 Test - ;Ultrasonic Testing is required for SAE AMS 6931 starting material per Note 16 on Drawing 801-6408529; Item - ;Straight Ball, Find Number 7 and Angle Ball, Find Number 8 of Drawing 6408529; Performance - ;SAE-AMS-6931 and SAE-AMS-2631; Acceptance - ;SAE-AMS-2631; Test - Weldability Test of ASTM-B369 material Item - ;Body, Find Number 72-S1 and Tailpiece, Find Number 80-S1 of Drawing 6408529; Performance - ASTM-B369 Acceptance - ASTM-B369 Test - ;Production Test; Item - ;Each Assembly; Performance - ;General Note 18 of Drawing 6408529; Acceptance - ;General Note 18 of Drawing 6408529; Test - Non-Destructive Tests Item - ;Weld Repair (as applicable); Performance - Per applicable fabrication specification Acceptance - Per applicable fabrication specification 3.4 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/. 3.5 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 / -0 PSIG. For pressure tests at or above 100 PSIG up to and including 2500 PSIG, the pressure tolerance must be +2% / -0 PSIG rounded off to the nearest multiple of the smallest graduation on an analog test pressure gauge, not to exceed 50 PSIG. For pressure tests above 2500 PSIG, the pressure tolerance must be +2% / -0 PSIG, rounded off to the nearest multiple of the smallest graduation on an analog test pressure gauge, not to exceed 200 PSIG. The pressure test time tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure test time tolerances are not provided by drawings, specifications or specified elsewhere in this contract, the following must be used: For a test duration up to and including 1 hour, the tolerance must be +5 minutes / - 0 minutes. For a test duration of more than 1 hour up to and including 24 hours, the tolerance must be +30 minutes / - 0 minutes. For a test duration of more than 24 hours, the tolerance must be +60 minutes / - 0 minutes. 3.6 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/ 3.7 Radiography is required on ;Body, Find Number 72-S1 and Tailpiece, Find Number 80-S1 of Drawing 6408529; . 3.8 Confidential Hydrostatic Test Pressures - When test pressures are confidential, certification must reference ;Drawing 830-6404016, Revision B; 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. 3.9 Chemours Company (formerly DuPont) Teflon Coating 850G-204 and 852G-201. Use of Chemours Company (formerly 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; . 3.9.1 Naval Ordnance Systems Command OD 10362 First Revision dated 15 Aug 1961 is provided by Contract Support Library Reference Number CSD018 in ECDS at https://register.nslc.navy.mil/ 3.9.2 CSD099 provides guidance for acceptance/rejection of teflon-coated valve balls after valve assembly production testing. 3.10 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/ 3.11 Ball Spherical Surface Waviness - Unless otherwise specified on drawing, all sealing area surfaces must have a spherical surface waviness which does not exceed 0.0005 inches of height per inch of spherical surface. Roughness and waviness ratings must apply in a direction which yields the maximum rating, normally perpendicular to the lay. 3.12 ;Surface waviness must be verified prior to Teflon coating.; 3.13 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 3.14 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. 3.15 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 K-MONEL Fasteners - Material must be heat treated per QQ-N-286. 3.16.1 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. 3.16.2 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. 3.17 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.) 3.17.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222. 3.17.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order. 3.18 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.19 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. 3.19.1 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. 3.19.2 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. 3.19.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.20 Installation of titanium shims must be performed using section 6.1.3 of the procedure provided in CSD158 in the ECDS (Electronic Contractor Data Submission) system at: https://register.nslc.navy.mil/. Paragraph 6.1.3.9 is not applicable. 3.20.1 Use of alternative epoxies, other than the epoxies listed in EQUIPMENT/MATERIAL section of CSD158, must be requested as stated elsewhere in the Contract/Purchase Order. 3.21 Thread Forming - The following provides the official interpretation of paragraph 4.5.2.7 of MIL-DTL-1222. 3.21.1 In order to qualify for "Alternate Mechanical Testing" found in MIL-DTL-1222J paragraph 4.5.2.7 and utilize the mechanical properties for the starting bar stock in lieu of performing yield strength or proof stress testing on finished fasteners, all of the subsequent provisions found in MIL-DTL-1222J paragraphs 4.5.2.7 a through e must be met. If any single provision is not met, all required mechanical testing must be performed on the finished full sized fasteners. These provisions are explained as follows: a. Proper product lot control and traceability must be in place. b. No heat treatment (including hot heading and hot forming), cold forming, drawing, rolling and thread rolling may be performed on the starting bar, fastener blanks or finished fasteners after the completion of the mechanical testing on the starting bar. c. and d. The proper size starting bar must be selected to ensure mechanical properties of finished fasteners are represented by the mechanical properties of the starting bar. e. The mandatory testing, axial tensile (studs) and wedge tensile (screws and bolts) must be performed on full sized fasteners. Note that there is a typographical error in paragraph 4.5.2.7 and that the ...
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