Loren Data's SAM Daily™

SAMDAILY.US - ISSUE OF JUNE 05, 2022 SAM #7492
SOLICITATION NOTICE

48 -- VALVE, HULL/BACKUP

Notice Date

6/3/2022 10:21:41 AM
 

Notice Type

Solicitation
 

NAICS

332919 — Other Metal Valve and Pipe Fitting Manufacturing
 

Contracting Office

NAVSUP WEAPON SYSTEMS SUPPORT MECH MECHANICSBURG PA 17050-0788 USA
 

ZIP Code

17050-0788
 

Solicitation Number

N0010422QFD98
 

Response Due

6/21/2022 9:00:00 PM
 

Archive Date

07/07/2022
 

Point of Contact

Telephone: 7176051234
 

E-Mail Address

SYLVIA.SENTZ@NAVY.MIL
(SYLVIA.SENTZ@NAVY.MIL)
 

Description

CONTACT INFORMATION|4|N743.45|WVN|717-605-3353|sylvia.sentz@navy.mil| ITEM UNIQUE IDENTIFICATION AND VALUATION (MAR 2022)|19|||||||||||||||||||| MARKINGS LEVEL I/SUBSAFE/DSS-SOC/TRIPER|5|x||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP REVIEW FEB 1991)(FEB 1999)|1|See specification sections C and E| INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2||| INSPECTION AND ACCEPTANCE - SHORT VERSION|8|x||x|||||| INSPECTION/ACCEPTANCE POINT|6||||||| TIME OF DELIVERY (JUNE 1997)|20|0001|4|365 days|||||||||||||||||| GENERAL INFORMATION-FOB-DESTINATION|1|B| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)|16|Stand-Alone Receiving Report - Certifications Combo-Receiving Report & Invoice - Material |n/a|tbd|N00104|tbd|N39040 - Certifications, S4306A - Material|N50286|tbd|133.2|n/a|n/a|S4306A - Material|n/a|n/a|See DD 1423|PORT_PTNH_WAWF_NOTIFICATION@NAVY.MIL| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| EQUAL OPPORTUNITY (SEP 2016)|2||| WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUNE 2003)|6|one year from 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(DEVIATION 2020-O0019) (MAR 2022))|3|||| NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (OCT 2020)(DEVIATION 2020-O0008)|1|| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2020)|13|||||||||||||| SMALL BUSINESS PROGRAM REPRESENTATIONS (SEP 2021)|4||||| 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 (JAN 2022)|13|332919|750|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||x| 1. Data Item A001 (inspection and Test Plan) may be waived if already on fileat NAVSUP WSS Mech. 2. Drawings associated with this solicitation will be made available on the SAM.gov website but will be restricted access, which needs to be approved.Once access has been requested, interested vendors should email the POC listed on the solicitation to inform them of the request. 3. NAVSUP WSS Mech will be considering past performance in the evaluation ofoffers. See Clause 252.213-7000. 4. All contractual documents (i.e. contracts, purchase orders, task orders,delivery orders, and modifications) related to the instant procurement areconsidered to be ""issued"" by the Government when copies are either depositedin 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. 5. The following proposed delivery schedule applies: RADIOGRAPHY SHOOTING SKETCHES (RSS) 45 DAYS ADC SD APPROVAL OF RADIO RSS 30 DAYS AFTER RECEIPT PRODUCTION RADIOGRAPHY (PR) 135 DAYS AFTER APPROVAL OF RSS SD APPROVAL OF PR 30 DAYS AFTER RECEIPT 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 (365 days) Delivery days and past performance will be evaluation factors in determining awardee. Early and incremental delivery is acceptable at no additional cost to the Government. 6. This requirement requires access to confidential drawings. These drawings are not required to provide a quotation for the RFQ/RFP. However, in the event of an award, a facility security clearance is/maybe required. 7. This item requires oxygen cleaning and requires Navy Joint Source Certification prior to O2 cleaning. See local text WSSTERMDZ01 and WSSTERMEZ01. 8. Radiography shooting sketches and production radiography can be submittedvia WAWF with acceptance by N39040. (The actual Radiography film cannot beattached in WAWF but should be mailed to Portsmouth NSY Attn: Code 135.3) 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. 1.1.1 LI-SOC ITEM - It has been determined that this item falls within both the Level I boundary and the Scope of Certification (SOC) boundary. 1.1.2 This ;2 Inch Combination Hull and Backup Ball Valve; contains non-metallic materials which must satisfy the toxicity and flammability requirements of NAVSEA SS800-AG-MAN-010/P-9290. Use of any material other than that specified requires special engineering approval and may require testing. 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 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. 2.3.2 Documents, drawings, and publications supplied are listed under ""Drawing Number"". These items should be retained until an award is made. 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=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=6404016 |53711| B| |F|0001 | B|00026|0000000 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 | | | |130701|A| | | DOCUMENT REF DATA=ASTM-B369 | | | |200401|A| | | DOCUMENT REF DATA=MIL-STD-792 | | |F |060519|A| | | DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | | DOCUMENT REF DATA=MIL-STD-1330 | | |D |070628|A| |01| 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=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-PRF-27617 | | |F |980217|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=SS800-AG-MAN-010/P-9290 | | |A |200324|A| |42| 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 must be in accordance with Naval Sea Systems Command drawing 6408529 assembly 97, Naval Ship Systems Command drawings 4385050, 4384678, and all liabilities provided with this Contract/Purchase Order (less hull fasteners - Find Numbers 69 and 70), except as amplified or modified herein.; 3.1.1 ;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.; 3.1.2 ;The thermocouple hole depicted on page 12 of NAVSEA drawing 6408529, Find Number 5, is not required.; 3.2 Oxygen Cleaning - This material must be cleaned, tested, packaged & labeled by trained personnel and procedures in accordance with MIL-STD-1330. 3.3 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: Part - ;Body, Find Number 72-S1 and Tailpiece, Find Number 77-S1; Material - ;ASTM-B369, Alloy UNS 96400; Part - ;Stems, Find Number 14 and Find Number 81; Material - ;QQ-N-286, Alloy UNS N05500, Form 2, Annealed (Hot Finished or Cold Drawn) and Age Hardened; Part - ;Continuous Threaded Stud, Find Number 62; Material - ;MIL-DTL-1222, Type IV, QQ-N-286, Alloy UNS N05500, Annealed and Age Hardened; PART - ;Self-locking Heavy Hex Nut, Find Number 43; 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 Number 10 and Find Number 12; 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; Material - ;QQ-N-281, Class A, Form 1, Annealed (Hot Finished or Cold Drawn); Part - ;Straight Ball, Find Number 5 and Angle Ball, Find Number 6; 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; 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. 3.4 Testing Certification - Certifications are required for the following tests on the items listed below. Additional testing on other piece parts (if any) per applicable drawings is still required, but certifications are only required as listed below. Test - ;Liquid Penetrant Inspection; Item - ;Continuous Threaded Stud, Find Number 62; 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; 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 - ;Ultrasonic Testing is required for SAE AMS 6931 starting material per Note 16 on Drawing 801-6408529; Item - ;Straight Ball, Find Number 5 and Angle Ball, Find Number 6; Performance - ;In Accordance with 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 77-S1; Performance - ASTM-B369 Acceptance - ASTM-B369 Test - ;Dye Penetrant Inspection; Item - ;Body Insert, Find Number 68-S1; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;MIL-STD-2035; Test - ;Production Test; Item - ;Each Assembly; Performance - ;General Note 18 of Drawing 6408529; Acceptance - ;General Note 18 of Drawing 6408529; Test - ;Dye Penetrant Inspection; Item - ;Tailpiece weld ends in final machined condition including 1/2"" of base material; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;S9074-AR-GIB-010A/278; 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 - Annealing and Age Hardening Item - ;Stems, Find Number 14 and Find Number 81 and Continuous Threaded Stud, Find Number 62; Performance - QQ-N-286 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. 3.5 Radiography is required on ;Body, Find Number 72-S1 and Tailpiece, Find Number 77-S1; . 3.6 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/. 3.7 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. 3.7.1 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. 3.7.2 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. 3.7.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.8 Confidential Hydrostatic Test Pressures - When test pressures are confidential, certification must reference ;Drawing 830-6404016, Rev 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 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. 3.10 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; . 3.10.1 ;Naval Ordinance Systems Command OD 10362 First Revision dated 15 Aug 1961 is provided by Contract Support Library Reference Number CSD018.; 3.10.2 CSD099 provides guidance for acceptance/rejection of teflon-coated valve balls after valve assembly production testing. 3.11 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number ;CSD018, CSD099; in ECDS at https://register.nslc.navy.mil/ 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 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. 3.14 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/ 3.15 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 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 ;Grease must be MIL-PRF-27617 Type III (Krytox 240AC).; 3.21 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 887306381Y; ) 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. 3.22 Welding or Brazing - When welding, brazing, and allied processes are required, as invoked by Section C paragraph 3 requirements, they must be in accordance with S9074-AR-GIB-010A/278, 0900-LP-001-7000 for brazing of piping and pressure vessel applications, or S9074-AQ-GIB-010/248 for brazing of other applications. For all production and repair welding and brazing, personnel and procedures must be qualified under S9074-AQ-GIB-010/248 or 0900-LP-001-7000, as applicable. Repair welding is not permitted on ;on alloy C90300 material; . Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing. 3.23 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. 3.24 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. 3.24.1 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. 3.24.2 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/ 3.24.3 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. 3.25 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. 3.26 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...
 

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