Loren Data's SAM Daily™

SAMDAILY.US - ISSUE OF APRIL 15, 2021 SAM #7075
SOLICITATION NOTICE

48 -- 48--VALVE,BALL

Notice Date

4/13/2021 7:04:55 AM
 

Notice Type

Solicitation
 

NAICS

333999 — All Other Miscellaneous General Purpose Machinery Manufacturing
 

Contracting Office

NAVSUP WEAPON SYSTEMS SUPPORT MECH MECHANICSBURG PA 17050-0788 USA
 

ZIP Code

17050-0788
 

Solicitation Number

N0010421QFB00
 

Response Due

4/20/2021 12:00:00 AM
 

Archive Date

05/05/2021
 

Point of Contact

Telephone: 7176054237
 

E-Mail Address

WILLIAM.E.NORMAN2@NAVY.MIL
(WILLIAM.E.NORMAN2@NAVY.MIL)
 

Description

CONTACT INFORMATION|4|N743.43|WV1|717-605-4237|william.e.norman2@navy.mil| ITEM UNIQUE IDENTIFICATION AND VALUATION (MAR 2016)|19|||||||||||||||||||| INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT|6|x|||||| GENERAL INFORMATION-FOB-DESTINATION|1|B| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)|16|Combo (Invoice & Receiving)|N/A|TBD|N00104|TBD|TBD|N50286|TBD|N/A|N/A|TBD|||||| 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|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|x| This amendment is hereby incorporated to extend the offer due date to 20 APR 21. 1. Data Item A001 (Inspection and Test Plan) maybe waived if already on file at NAVSUP WSS Mech. 2. Submission of Certification Data CDRLs will be on or before 20 days prior toscheduled delivery. PNSYReview/acceptance of Certification CDRLs 6 working days after receipt of Certification DD 1423 CDRLs.Final delivery of material will be on or before 410 days after effective date of the resulting contract. 3. Consistent with FAR 52.216-18, all contractual documents (i.e. contracts, purchase orders, task orders ,delivery orders and modifications) related to the instant procurement are considered to be ""issued"" by the Government when copies are either deposited in the mail, transmitted by facsimile, or sent by other electronic commerce methods, such as email. The Government's acceptance of the contractor's proposal constitutes bilateral agreement to ""issue"" contractual documents as detailed herein. 4. NAVSUP WSS Mech will be considering past performance in the evaluation of offers iaw FAR 13.106. \ 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=4384678C01 |53711| C|DN |D| 0001 | |C4999|8006753 DRAWING DATA=4384678C01 |53711| C|DN |D| 0002 | |C4999|8004508 DRAWING DATA=4384678C01 |53711| C|DN |D| 0003 | |C4999|8003094 DRAWING DATA=4384678C02 |53711| C|DN |D| 0001 | |C4999|8004126 DRAWING DATA=4384678C03 |53711| C|DN |D| 0001 | |C4999|8003540 DRAWING DATA=4384678C04 |53711| C|DN |D| 0001 | |C4999|8004025 DRAWING DATA=4384678C05 |53711| C|DN |D| 0001 | |C4999|8003394 DRAWING DATA=4384678C06 |53711| C|DN |D| 0001 | |C4999|8003396 DRAWING DATA=4385050 |53711| C| |D| 0002 | |C4999|8030555 DRAWING DATA=4385050 |53711| C| |D| 0003 | |C4999|8040193 DRAWING DATA=4385050 |53711| C| |D| 0004 | |C4999|8033416 DRAWING DATA=4385050 |53711| C| |D| 0005 | |C4999|8035092 DRAWING DATA=4385050 |53711| C| |D| 0006 | |C4999|8025046 DRAWING DATA=4385050 |53711| C| |D| 0007 | |C4999|8019198 DRAWING DATA=4385050 |53711| C| |D| 0008 | |C4999|8031453 DRAWING DATA=4385050 |53711| C| |D| 0009 | |C4999|8026598 DRAWING DATA=4385050 |53711| C| |D| 0010 | |C4999|8021021 DRAWING DATA=4385050 |53711| C| |D| 0011 | |C4999|8025302 DRAWING DATA=4385050 |53711| C| |D| 0012 | |C4999|8025411 DRAWING DATA=4385050 |53711| C| |D| 0013 | |C4999|8019720 DRAWING DATA=4385050 |53711| C| |D| 0014 | |C4999|8025316 DRAWING DATA=4385050 |53711| C| |D| 0015 | |C4999|8020494 DRAWING DATA=4385050 |53711| C| |D| 0016 | |C4999|8023311 DRAWING DATA=4385050 |53711| C| |D| 0017 | |C4999|8023868 DRAWING DATA=4385050 |53711| C| |D| 0018 | |C4999|8009884 DRAWING DATA=4385050-C1 |53711| -|1N |D| 0001 | |-4999|8004094 DRAWING DATA=4385050-C2 |53711| -|1N |D| 0001 | |-4999|8004085 DRAWING DATA=4385050-C3 |53711| -|1N |D| 0001 | |-4999|8004108 DRAWING DATA=4385050-C4 |53711| -|1N |D| 0001 | |-4999|8004020 DRAWING DATA=4385050-C5 |53711| -|1N |D| 0001 | |-4999|8004569 DRAWING DATA=4385050-C5 |53711| -|1N |D| 0002 | |-4999|8001873 DRAWING DATA=4385050-C6 |53711| -|1N |D| 0001 | |-4999|8004549 DRAWING DATA=4385050-C6 |53711| -|1N |D| 0002 | |-4999|8001703 DRAWING DATA=6404016 |53711| B| |F| 0001 | |B0002|6000000 DRAWING DATA=6408529 |53711| C| |D| 0001 | |C4999|8047141 DRAWING DATA=6408529 |53711| C| |D| 0001.A | |C4999|8033290 DRAWING DATA=6408529 |53711| C| |D| 0001.B | |C4999|8034507 DRAWING DATA=6408529 |53711| C| |D| 0002 | |C4999|8029855 DRAWING DATA=6408529 |53711| C| |D| 0002.A | |C4999|8030300 DRAWING DATA=6408529 |53711| C| |D| 0002.B | |C4999|8031914 DRAWING DATA=6408529 |53711| C| |D| 0002.C | |C4999|8023552 DRAWING DATA=6408529 |53711| C| |D| 0002.D | |B4999|8027638 DRAWING DATA=6408529 |53711| C| |D| 0002.E | |B4999|8026093 DRAWING DATA=6408529 |53711| C| |D| 0002.F | |B4999|8024330 DRAWING DATA=6408529 |53711| C| |D| 0003 | |C4999|8027045 DRAWING DATA=6408529 |53711| C| |D| 0003.A | |C4999|8028866 DRAWING DATA=6408529 |53711| C| |D| 0003.B | |C4999|8030744 DRAWING DATA=6408529 |53711| C| |D| 0003.C | |C4999|8029270 DRAWING DATA=6408529 |53711| C| |D| 0003.D | |C4999|8029936 DRAWING DATA=6408529 |53711| C| |D| 0003.E | |C4999|8028123 DRAWING DATA=6408529 |53711| C| |D| 0003.F | |C4999|8033412 DRAWING DATA=6408529 |53711| C| |D| 0003.G | |C4999|8031328 DRAWING DATA=6408529 |53711| C| |D| 0003.H | |C4999|8030064 DRAWING DATA=6408529 |53711| C| |D| 0003.J | |C4999|8027981 DRAWING DATA=6408529 |53711| C| |D| 0003.K | |C4999|8029756 DRAWING DATA=6408529 |53711| C| |D| 0003.L | |C4999|8028979 DRAWING DATA=6408529 |53711| C| |D| 0004 | |C4999|8023816 DRAWING DATA=6408529 |53711| C| |D| 0005 | |A4999|8014289 DRAWING DATA=6408529 |53711| C| |D| 0006 | |B4999|8019837 DRAWING DATA=6408529 |53711| C| |D| 0007 | |A4999|8015734 DRAWING DATA=6408529 |53711| C| |D| 0008 | |A4999|8016600 DRAWING DATA=6408529 |53711| C| |D| 0009 | |B4999|8020317 DRAWING DATA=6408529 |53711| C| |D| 0010 | |A4999|8010701 DRAWING DATA=6408529 |53711| C| |D| 0011 | |C4999|8019248 DRAWING DATA=6408529 |53711| C| |D| 0012 | |A4999|8010427 DRAWING DATA=6408529 |53711| C| |D| 0013 | |A4999|8009909 DRAWING DATA=6408529 |53711| C| |D| 0014 | |A4999|8010792 DRAWING DATA=6408529 |53711| C| |D| 0015 | |C4999|8020474 DRAWING DATA=6408529 |53711| C| |D| 0016 | |C4999|8015236 DRAWING DATA=6408529C01 |53711| A|DN |D| 0001 | |A4999|8004040 DRAWING DATA=6408529C01 |53711| A|DN |D| 0002 | |A4999|8002646 DRAWING DATA=6408529C01 |53711| A|DN |D| 0003 | |A4999|8005321 DRAWING DATA=6408529C01 |53711| A|DN |D| 0003.A | |A4999|8005354 DRAWING DATA=6408529C01 |53711| A|DN |D| 0003.B | |A4999|8005379 DRAWING DATA=6408529C01 |53711| A|DN |D| 0003.C | |A4999|8005279 DRAWING DATA=6408529C01 |53711| A|DN |D| 0003.D | |A4999|8004439 DRAWING DATA=6408529C01 |53711| A|DN |D| 0004 | |A4999|8003101 DRAWING DATA=6408529C01 |53711| A|DN |D| 0005 | |A4999|8004559 DRAWING DATA=6408529C01 |53711| A|DN |D| 0006 | |A4999|8004637 DRAWING DATA=6408529C01 |53711| A|DN |D| 0007 | |A4999|8003229 DRAWING DATA=6408529C01 |53711| A|DN |D| 0008 | |A4999|8001987 DRAWING DATA=6408529C01 |53711| A|DN |D| 0009 | |A4999|8002067 DRAWING DATA=6408529C01 |53711| A|DN |D| 0010 | |A4999|8002038 DRAWING DATA=6408529C01 |53711| A|DN |D| 0011 | |A4999|8001948 DRAWING DATA=6408529C01 |53711| A|DN |D| 0012 | |A4999|8002566 DRAWING DATA=6408529C02 |53711| A|DN |D| 0001 | |A4999|8003747 DRAWING DATA=6408529C02 |53711| A|DN |D| 0002 | |A4999|8003002 DRAWING DATA=6408529C02 |53711| A|DN |D| 0003 | |A4999|8003721 DRAWING DATA=6408529C02 |53711| A|DN |D| 0004 | |A4999|8001187 DRAWING DATA=6408529C02 |53711| A|DN |D| 0005 | |A4999|8003208 DRAWING DATA=6408529C02 |53711| A|DN |D| 0006 | |A4999|8001108 DOCUMENT REF DATA=FED-STD-H28 | | |B |190424|A| | | 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 | | | |090401|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-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 2 Inch Combination Hull and Backup Ball Valve shall be in accordance with Naval Sea Systems Command drawing 6408529 Assembly 95, Naval Ship Systems Command drawings 4385050 and 4384678 and DRNS 4384678-C1 through 4384678-C6 (less hull fasteners pieces 69 and 70), except as amplified or modified herein.; 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 72-S1 and Tailpiece, Piece 79-S1; Material - ;ASTM-B369, Alloy UNS 96400; Part - ;Stems, Piece 14 and Piece 81; Material - ;QQ-N-286, Alloy UNS N05500, Form 2, Hot Finished or Cold Drawn Annealed and Age Hardened; Part - ;Continuous Threaded Studs, Piece 62; Material - ;MIL-DTL-1222, Type IV, QQ-N-286, Alloy UNS N05500, Annealed and Age Hardened and Marked .K.; PART - ;Self-locking Heavy Hex Nuts, Piece 43; MATERIAL - QQ-N-281, Class A or B, in accordance with MIL-N-25027/1. All material must be the same Class. SELF-LOCKING ELEMENT - ASTM-D4066, Group 01, Class 1 or 2, Grade 1. Part - ;Nuts, Stem Retaining Pieces 10 and 12; Material - ;ASTM-B139 UNS C51000 Temper Hard; Part - ;Insert, Piece 68-S1; Material - ;QQ-N-281, Class A, Form 1, Hot finished or Cold drawn, Annealed; For Boilerplate R00375, Part - ;Straight Ball, Piece 7 and Angle Ball, Piece 8; 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; Material - MD71-GG Mearthane (Graphite Filled Urethane). Material must be manufactured by Mearthane Products Inc. Cranston, RI. (Properties Specified Below Only) ITEM PROPERTY ASTM TEST METHOD VALUE (A) Hardness D2240 70 +/- 5 Shore D (B) Specific Gravity D792 1.18 +/- 0.02 (C) Tensile Strength D412 (DIEC) 5000 PSI MIN (D) Compression-Defl D575 700 PSI MIN @ 2% DEF. (E) Tensile Impact D1822 300 FT-LB/SQ IN (Note 1) (TYPE L SPECIMEN) (F) Water Absorption D570 1.5% MAX (1 Week at R.T.) Note 1: These values are minimum averages. Separate specimen values may not vary more than 25% under the specified minimum. 3.3 Testing Certification - Certifications are required for the following tests on the items listed below. Additional testing on other piece parts (if any) per applicable drawings is still required, but certifications are only required as listed below. Test - ;Liquid Penetrant Inspection; Item - ;Continuous Threaded Studs, Piece 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 Piece 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-N-25027/1; Test - ;Ultrasonic Testing is required for SAE AMS 6931 starting material per Note 16 on Drawing 801-6408529; Item - ;Straight Ball, Piece 7 and Angle Ball, Piece 8; Performance - ;In Accordance with SAE-AMS-6931 and SAE-AMS-2631; Acceptance - ;SAE-AMS-2631; Test - Weldability Test of ASTM-B369 material Item - ;Body, Piece 72-S1 and Tailpiece, Piece 79-S1; Performance - ASTM-B369 Acceptance - ASTM-B369 Test - Pressure Tests Item - Each Assembly Performance - ;Production Test 18 A,B,C,D,E And F of drawing 6408529; Acceptance - ;Production Test 18 A,B,C,D,E And F of drawing 6408529; 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 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 Piece 14 and Piece 81 and Continuous Threaded Studs Piece 62; Performance - QQ-N-286 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 Radiography is required on ;Body, Piece 72-S1 and Tailpiece, Piece 79-S1; . 3.6 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. 3.6.1 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. 3.6.2 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. 3.6.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.7 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. 3.8 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; . 3.9 ;Naval Ordnance Systems Command OD 10362 First Revision dated 15 Aug 1961 is provided by Contract Support Library Reference Number CSD018.; 3.10 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number ;CSD 099; in ECDS at https://register.nslc.navy.mil/ 3.10.1 CSD099 provides guidance for acceptance/rejection of teflon-coated valve balls after valve assembly production testing. 3.11 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/. 3.12 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 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. 3.15 K-MONEL Fasteners - Material must be heat treated per QQ-N-286. 3.15.1 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. 3.15.2 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. 3.16 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.) 3.16.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222. 3.16.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order. 3.17 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.18 ;During assembly, liberally coat the following surfaces with grease per CID A-A-50433 (Termalene No. 2): ball cavity (including body insert), stem cavity (excluding threads), ball outer surface, ball seats, O-rings and O-ring mating sealing surfaces, and all stem surfaces (excluding any splines). Lubricate valve threads and threaded fasteners with lubricant per CID A-A-59004 (Molykote P-37 paste).; 3.19 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 884245639; ) 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. 3.20 Welding or Brazing - When welding, brazing, and allied processes are required, they must be in accordance with S9074-AR-GIB-010A/278, (S9074-AQ-GIB-010/248 for brazing) by personnel and procedures qualified under S9074-AQ-GIB-010/248 for all production and repair welding and brazing. Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing. 3.21 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. 3.21.1 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. 3.21.2 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/ 3.21.3 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. 3.22 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. 3.23 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. 3.24 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. ^ QUALITY ASSURANCE REQUIREMENTS ^ 3.25 See CDRL DI-MISC-80678 (Test Certification) - A statement of tests performed, listing the pieces tested must be furnished along with a copy of the test results. Certification must include the contractor's name, address and date, quantity inspected, identified to the contract/purchase order and item number, and the Contractor's or authorized personnel's signature. Test certifications must reference the standard/specification, including the revision, to which the testing was performed and the acceptance criteria used. Test procedure numbers may also be referenced on test reports. Test reports on weldments must be identified to weld joint and layer. 3.26 Welding Requirements - When production or repair welding is required, the applicable welding procedure(s) and qualification data must be submitted for review and approval. In addition, the CONSUMED WELD METAL C of C as defined below must be submitted as part of the certification OQE package submitted by the Contractor. Note: These requirements do not apply to tack/spot welds. 3.26.1 Approval of the Contractor's qualification data must be obtained prior to performing any welding (production or repair). 3.26.2 If the Contractors qualification data has previously been approved by the Navy for other contracts, a copy of the original approval letter may be submitted along with the procedures and qualification data report to expedite the approval process.The approval letter must reference the applicable welding procedure and qualification data report identification/number. Prior approval does not guarantee acceptance for this or any future contracts. As far as practical, all procedures for the contract must be submitted at the same time. Welding procedures and qualification data must be submitted in a commercially available electronic format such as Adobe Acrobat PDF. The contractor must state the applicability of each weld procedure and qualification data submitted, citing the drawing number and pieces to be welded. (i.e. ""WP-123 and QD-123 are submitted for the weld joint between pieces 1 and 2 on drawing ABC."" "" WP-456 and QD-456 are submitted for the hardfacing of piece 3 on drawing XYZ.""). Authority for the repair of Special Repairs in castings and authority for the repair of wrought or forged material material must be obtained from the Procurement Contracting Officer. This request must describe the defect; including size, depth, location, and a description of the proposed repair. This request for NAVSUP-WSS Contracts must be submitted via the Electronic Contractor Data Submission (ECDS) application. 3.26.3 Any new procedure qualification performed under this Contract will require the vendor to provide a minimum 48 hour notification to DCMA with an offer to observe the welding of the test assemblies. The 48 hour time limit may be modified upon mutual agreement between the vendor and DCMA. 3.26.4 When drawings require hard facing surface Iron content (Nickel for Monel valves) not to exceed 5%, the contractor must verify surface Iron or Nickel content by performing chemical testing as defined by the applicable drawing. The chemical test results must be submitted as part of the qualification data. 3.26.5 Qualification requirements for production hardfacing: The maximum qualified thickness for hardfacing must be twice the weld deposit thickness measured in the as-welded condition that is subjected to initial NDT (Non-Destructive Testing...
 

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